EASA/JAA QUICK REFERENCE HANDBOOK

EMERGENCY EVACUATION

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In connection with the use of this document, Embraer does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose.

Copyright © 2007 by Embraer S.A.. All rights reserved.

EASA/JAA

QUICK REFERENCE HANDBOOK THIS PUBLICATION CANCELS AND SUPERSEDES THE QRH–135/1569 DATED JUNE 25, 2002; REVISION 6 DATED MARCH 31, 2005.

QRH–135/1569-02 JULY 16, 2007

REVISION 10 – FEBRUARY 10, 2014

LIST OF EFFECTIVE PAGES

THE PORTION OF THE TEXT AFFECTED BY THE CHANGE IS INDICATED BY A VERTICAL LINE IN THE OUTER MARGIN OF THE PAGE.

ORIGINAL...................... 0.................. JUL 16, 2007 REVISION...................... 1.................AUG 31, 2007 REVISION...................... 2.................MAR 28, 2008 REVISION...................... 3.................AUG 29, 2008 REVISION...................... 4..................JUN 30, 2009 REVISION...................... 5................. DEC 23, 2009 REVISION...................... 6.................MAR 29, 2010 REVISION...................... 7................. OCT 10, 2010 REVISION...................... 8................. DEC 23, 2010 REVISION...................... 9..................JUN 10, 2011 REVISION..................... 10.................FEB 10, 2014

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 244 CONSISTING OF THE FOLLOWING:

PAGE N° CHANGE N° PAGE N° CHANGE N°

* Asterisk indicates pages changed, added, or deleted by the current revision.

REVISION 10 A

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* Title ..................................10 * A ......................................10 * B ......................................10 * C ......................................10 I ........................................7 EAP INTRO-1 ....................0 EAP INTRO-2 ....................1 EAP INTRO-3 ....................9 EAP INTRO-4 ....................9 S-1 ...................................0 S-2 ...................................0 S-3 ...................................7 S-4 ...................................4 S-4A ..................................4 S-4B ..................................4 S-5 ...................................0 S-6 ...................................0 S-7 ...................................0 S-8 ...................................0 S-9 ...................................0 S-10 ..................................0 S-11 ..................................0 S-12 ..................................0 NAP-1 ...............................8 NAP-2 ...............................8 * NAP-3 ..............................10 NAP-4 ...............................0 * NAP-5 ..............................10 NAP-6 ...............................8 NAP-7 ...............................4 * NAP-8 ..............................10 NAP-9 ...............................7 NAP-10 ..............................3 NAP-11 ..............................4 * NAP-12 .............................10 NAP-13 ..............................9 NAP-14 ..............................0 * NAP-15 .............................10

NAP-16 ..............................0 NAP-17 ..............................0 NAP-18 ..............................4 NAP-19 ..............................0 NAP-20 ..............................8 NAP-21 ..............................8 NAP-22 ..............................8 NAP-23 ..............................4 NAP-24 ..............................4 NAP-25 ..............................4 NAP-26 ..............................8 NAP-26A ............................5 NAP-26B ............................5 NAP-27 ..............................0 NAP-28 ..............................0 NAP-29 ..............................0 NAP-30 ..............................0 NAP-31 ..............................0 NAP-32 ..............................0 NAP-33 ..............................0 NAP-34 ..............................0 NAP-35 ..............................0 NAP-36 ..............................8 NAP-37 ..............................0 * NAP-38 .............................10 NAP-39 ..............................7 NAP-40 ..............................0 NAP-41 ..............................0 NAP-42 ..............................3 NAP-43 ..............................3 NAP-44 ..............................8 EAP0-1 ..............................9 EAP0-2 ..............................9 EAP0-3 ..............................9 EAP0-4 ..............................9 EAP0-5 ..............................9 EAP0-6 ..............................9 * EAP0-7 .............................10 * EAP0-8 .............................10 EAP1-1 ..............................0 EAP1-2 ..............................0


THE PORTION OF THE TEXT AFFECTED BY THE CHANGE IS INDICATED BY A VERTICAL LINE IN THE OUTER MARGIN OF THE PAGE. PAGE N° CHANGE N° PAGE N° CHANGE N°


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EAP1-3 .............................. 0 EAP1-4 .............................. 0 EAP1-5 .............................. 0 EAP1-6 .............................. 9 EAP1-7 .............................. 0 EAP1-8 .............................. 0 * EAP1-9 ............................. 10 * EAP1-10........................... 10 EAP1-11............................ 5 EAP1-12............................ 5 EAP1-13............................ 5 EAP1-14............................ 4 EAP2-1 .............................. 0 EAP2-2 .............................. 0 EAP2-3 .............................. 8 EAP2-4 .............................. 0 EAP2-5 .............................. 0 EAP2-6 .............................. 0 EAP2-7 .............................. 4 * EAP2-8 ............................. 10 * EAP2-9 ............................. 10 EAP2-10............................ 0 EAP2-11............................ 0 EAP2-12............................ 0 EAP2-13............................ 2 EAP2-14............................ 0 EAP3-1 .............................. 0 EAP3-2 .............................. 0 EAP3-3 .............................. 0 EAP3-4 .............................. 0 EAP3-5 .............................. 0 EAP3-6 .............................. 0 EAP4-1 .............................. 0 EAP4-2 .............................. 0 * EAP4-3 ............................. 10 EAP4-4 .............................. 0 EAP4-5 .............................. 0 EAP4-6 .............................. 0 EAP5-1 .............................. 0 EAP5-2 .............................. 0 EAP5-3 .............................. 9 EAP5-4 .............................. 0 EAP5-5 .............................. 8 EAP5-6 .............................. 0 EAP5-7 .............................. 4 * EAP5-8 ............................. 10 * EAP5-9 ............................. 10 EAP5-10............................ 4 EAP5-11............................ 4 EAP5-12............................ 0 EAP5-13............................ 9 EAP5-14............................ 9 EAP5-15............................ 9 EAP5-16............................ 9 EAP6-1 .............................. 9 EAP6-2 .............................. 9 EAP6-3 .............................. 9 EAP6-4 .............................. 9

* EAP6-5 ............................. 10 EAP6-6 .............................. 9 * EAP6-7 ............................. 10 * EAP6-8 ............................. 10 EAP6-9 .............................. 9 EAP6-10 ............................ 9 EAP6-11 ............................ 9 EAP6-12 ............................ 9 EAP6-13 ............................ 9 EAP6-14 ............................ 9 EAP7-1 .............................. 0 EAP7-2 .............................. 0 EAP7-3 .............................. 0 EAP7-4 .............................. 0 EAP7-5 .............................. 0 EAP7-6 .............................. 0 EAP8-1 .............................. 0 EAP8-2 .............................. 0 EAP8-3 .............................. 0 EAP8-4 .............................. 0 EAP8-5 .............................. 0 EAP8-6 .............................. 8 * EAP8-7 ............................. 10 EAP8-8 .............................. 0 EAP8-9 .............................. 0 EAP8-10 ............................ 0 EAP8-11 ............................ 0 EAP8-12 ............................ 0 EAP9-1 .............................. 9 EAP9-2 .............................. 9 EAP9-3 .............................. 9 EAP9-4 .............................. 9 EAP9-5 .............................. 9 * EAP9-6 ............................. 10 EAP9-7 .............................. 9 EAP9-8 .............................. 9 EAP9-9 .............................. 9 EAP9-10 ............................ 9 EAP9-11 ............................ 9 EAP9-12 ............................ 9 EAP9-13 ............................ 9 EAP9-14 ............................ 9 EAP9-15 ............................ 9 EAP9-16 ............................ 9 EAP10-1 ............................ 0 EAP10-2 ............................ 0 * EAP10-3 ........................... 10 EAP10-4 ............................ 4 EAP10-5 ............................ 0 EAP10-6 ............................ 0 EAP10-7 ............................ 0 EAP10-8 ............................ 9 EAP10-9 ............................ 0 EAP10-10 .......................... 0 EAP11-1 ............................ 0 EAP11-2 ............................ 0 EAP11-3 ............................ 0 EAP11-4 ............................ 4


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EAP11-5.............................0 EAP11-6.............................0 * EAP11-7............................10 EAP11-8.............................4 EAP12-1.............................0 EAP12-2.............................0 EAP12-3.............................4 EAP12-4.............................0 EAP12-5.............................0 EAP12-6.............................0 EAP12-7.............................0 EAP12-8.............................4 * EAP12-9............................10 EAP12-10...........................0 EAP13-1.............................0 EAP13-2.............................0 EAP13-3.............................0 EAP13-4.............................0 EAP14-1.............................9 EAP14-2.............................4 EAP14-3.............................4 * EAP14-4............................10 EAP14-5.............................4 * EAP14-6............................10 EAP14-7.............................4 EAP14-8.............................4 PD-1 .................................5 PD-2 .................................7 PD-2A ................................5 PD-2B ................................5 PD-3 .................................0 PD-4 .................................0 PD-5 .................................0 PD-6 .................................0 PD-7 .................................0 PD-8 .................................0 PD-9 .................................0 PD-10 ...............................0 PD-11 ...............................7 PD-12 ...............................7 PD-13 ...............................7 PD-14 ...............................7 PD-15 ...............................7 PD-16 ...............................7 APP-1 ...............................0 APP-2 ...............................4

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APPLICABILITY

This handbook is applicable to the Legacy 600 model.

NOTE: The Legacy 600 model has the certification designation of EMB-135 BJ.

The procedures contained in this handbook have been developed by the manufacturer for use during the operation of the Legacy 600. These procedures are provided as guidance and should not be construed as prohibiting the development of equivalent procedures.

The use of the on board checklist is based on the assumption that both pilots have been properly trained on the type of airplane and, therefore, have a thorough knowledge of the airplane’s systems and procedures.

It further assumes that they know the consequences of not performing the right actions at the right time.

In case of conflicting information between this handbook and the AFM-135/1541, the AFM must prevail.

EMERGENCY/ABNORMAL PROCEDURES

ORIGINAL EAP INTRO-1

INTRODUCTION The Emergency/Abnormal Procedures published in the Quick Reference Handbook (QRH) are provided to pilots as quick guide to minimize the consequences of emergency and abnormal situations that might occur during the airplane operation.

In case a discrepancy is found between the QRH and the approved Airplane Flight Manual (AFM), the AFM shall prevail.

Using the QRH requires proper training on the execution of all operational, emergency and abnormal procedures set forth in the AFM and a thorough knowledge of airplane systems.

The procedures set forth herein also require situational awareness for identification of emergency or abnormal situations and pilot skills to guarantee safety. The Emergency Evacuation procedure accomplishment may be necessary in many situations and its need is at pilot’s discretion.

It is EMBRAER recommendation that any unusual situation encountered should be reported as quickly as possible to Flight Operations and Maintenance Personnel.

Three blocks of procedures are contained in this manual:

Smoke Procedures: address all annunciated and non annunciated smoke related procedures.

Non Annunciated Procedures: procedures that are not related to an EICAS message but rather to a condition present in the airplane. The Checklists are arranged in alphabetical order with Emergency Checklists (black label) first, followed by Abnormal Checklists (gray label).

Annunciated Procedures: procedures related to an EICAS message. These procedures are grouped by system and the system tabs are in alphabetical order. Each title procedure is followed by the corresponding EICAS message identification. The message provided for each procedure represents the root cause of the failure. The Checklists for each System Tab are first arranged with the Procedures that are related to Warning messages (red label) followed by the Procedures related to Caution messages (amber label) and then followed by the Procedures related to Advisory messages (blue label), therefore arranged in Procedure’s title alphabetical order.


EAP INTRO-2 REVISION 1

The emergency evacuation procedure is repeated in the last page of QRH, after Performance Data helping pilots to quickly get to this procedure.

Some procedures can either be annunciated or non annunciated. In this case, the procedures are presented in the Annunciated block but are referenced in the Non Annunciated index.

In each Annunciated System Tab Index, the related non annunciated procedures are presented with a cross-reference to the Non Annunciated Tab page. The Non Annunciated procedures index is classified into Emergency and Abnormal procedures, while both the Annunciated procedures index and EICAS Messages List are classified into Warning, Caution and Advisory.

Some EICAS messages do not have an associated QRH procedure. In these cases, “Crew Awareness” identifies the EICAS message as noted in the Index Table. If a Crew Awareness message is displayed on the EICAS, takeoff is prohibited, unless at least one of the following conditions is met:

- The message is an expected result of an intentional operation;

- Flight crew action is taken to clear the message; - Maintenance personnel take action to clear the

message; - The airplane is dispatched in accordance with

all approved company MEL provisions.

If one of the following Crew Awareness messages is presented after gate departure, the flight may continue only to the intended destination without further action:

- AHRS BASIC MODE, - DU 1 (2, 3, 4) FAN FAIL, - E1 (2) OIL IMP BYP, - ENG A/ICEOVERPRES, - IC 1 (2) FAN FAIL or - GEN 1 (2, 3, 4) BRG FAIL.

Some procedures include a characterization below the title if a relevant emergency/abnormal condition is present. Aural warnings, lights, EICAS indications, flight instrument flags or airplane condition can, itself or associated among themselves, characterize an emergency/abnormal situation.

The actions inside bold rectangular borderlines are recall items. They must be performed expeditiously, by memory.


REVISION 9 EAP INTRO-3

Flying the airplane is always the priority in any emergency/abnormal situation. Checklists should be called after the flight path is under control, critical phases of flight (such as takeoff and landing) have ended and all recall items have been accomplished.

Some emergency and abnormal situations require landing at the nearest suitable airport. This statement will be listed at the beginning of a task checklist to give the crew proper time to plan the landing. Also, as an aid for planning the diversion airport, the landing distance correction factor will be presented together with the “Land at nearest suitable airport” statement.

Some procedures contain “Lists of Relevant Inoperative Items” for that particular condition. Those lists presents only the most relevant items and for the full list, the AOM should be consulted. As SMOKE events are very time critical, on those procedures the lists contain only items that significantly affect airplane performance and/or controllability. For the entire list of relevant inoperative items on those conditions, the pilot can refer to the procedures associated with the electrical busses off.

Throughout this manual, a text followed by “()” means that either condition applies. A text followed by “-” means that both conditions apply simultaneously.

Some procedures require cabin depressurization. This will require either dumping the cabin air or the using manual control to accomplish this task. In this situation, manual control depressurization is the recommended method to be used for passenger comfort and should be done by setting the pressurization mode selector to MAN position and smoothly setting the controller to FULL UP position. When a specific method for cabin depressurization is required, the procedure will clearly state it.

The procedures contained herein assume that:

Airplane systems were operating normally prior to the failure.

All emergency/abnormal actions are performed in the order they are listed in the procedure.

Normal procedures have been properly performed.

Aural warnings are silenced as necessary. Master Warning/Caution lights are reset as soon as the failure is recognized.


EAP INTRO-4 REVISION 9

All procedures are self-contained. All other messages that may be generated by a single failure do not require that the procedures associated to those messages are accomplished in addition to the procedure addressing the root cause.

Circuit breakers must not be pushed in if they pop up.

All assigned tasks in the procedures have the indication END at the completion of each assigned task. No task is over until ……… has been reached. Upon completion of the checklist the reading pilot should state: “(Procedure Title) Checklist Complete”. In the event of multiple failures (excluding cascade failures) with different landing configuration and/or landing distance correction factors, the crew should use good judgment to determine the safest action.

According to the QRH philosophy, Rejected Takeoff (at or below V1) procedure is not considered in this manual. Indeed, should the flight crew decide to reject the takeoff; they will do it by memory, not by referring to the QRH. Consequently, Rejected Takeoff (at or below V1) procedure is a matter of flight crew training and is considered within the Standard Operating Procedures Manual, which contains the complete guidance to accomplish it.

END


Smoke

ORIGINAL S-1

TABLE OF CONTENTS

BAGGAGE SMOKE................... S-3

LAVATORY SMOKE.................. S-3

AIR CONDITIONING SMOKE.... S-4

CABIN FIRE OR SMOKE .......... S-5

ELECTRICAL SYSTEM FIRE OR SMOKE....................... S-6

SMOKE EVACUATION.............. S-11


Smoke

S-2 ORIGINAL

LIST OF EICAS MESSAGES

BAGG SMOKE...........................S-3

LAV SMOKE ..............................S-3


Smoke

REVISION 7 S-3

BAGGAGE SMOKE

EICAS Warning: BAGG SMOKE

EICAS Caution BAGG ACCESS OPN......NOT DISPLAYED

Fire Extg Bagg Button (if installed) .........PUSH IN

LAND AT THE NEAREST SUITABLE AIRPORT. Altitude ..............................MAINTAIN

Delay the descent as long as possible.

NOTE: Advise Ground Crew of possible Halon vapors approximately 75 minutes after discharging fire extinguishing bottle.

LAVATORY SMOKE

EICAS Warning: LAV SMOKE (may be presented).

Lavatory Light CB (Located in Line E) ........... PULL

Lavatory Flush CB's (Located in Line E or Cabin Entertainment Panel)... PULL

CABIN FIRE OR SMOKE Procedure (S-5)......... AS REQUIRED

END

END


Smoke

S-4 REVISION 4

AIR CONDITIONING SMOKE Condition: Smoke or odor inside the

cabin and/or cockpit.

Crew Oxygen Masks ....DON, 100% Smoke Goggles............DON Recirculation Fan.........PUSH OUT Crew Communication ..ESTABLISH

LAND AT THE NEAREST SUITABLE AIRPORT. XBleed...........................OPEN Suspected Bleed(s)......PUSH OUT Altitude..........................MAX 25’000 FT

MIN MEA No

Yes Suspected Pack .......... PUSH OUT Suspected Bleed ......... PUSH IN No

Yes Suspected Pack .......... PUSH IN Opposite Bleed............ PUSH OUT

No

Yes Opposite Bleed............ PUSH IN Opposite Pack ............. PUSH OUT

CONTINUES ON NEXT PAGE

SMOKE PERSISTS?

SMOKE PERSISTS?

SMOKE PERSISTS?


Smoke

REVISION 4 S-4A

CONTINUED FROM PREVIOUS PAGE

No

Yes Altitude ........................ MEA OR

15’000 FT, WHICHEVER IS HIGHER

If it is not possible to descend below 15’000 ft, anti-ice system failure messages may be presented. In this case, exit icing conditions.

SMOKE EVACUATION Procedure (S-11) ........AS REQUIRED

ICING CONDITIONS?

END


Smoke

S-4B REVISION 4

INTENTIONALLY BLANK


Smoke

ORIGINAL S-5

CABIN FIRE OR SMOKE

Condition: Smoke or odor inside the cabin and/or cockpit.

Crew Oxygen Masks......DON, 100% Smoke Goggles

or PBE..........................DON Recirculation Fan...........PUSH OUT Crew Communication....ESTABLISH

LAND AT THE NEAREST SUITABLE AIRPORT.

No

Yes

AIR CONDITIONING SMOKE (S-4) and/or ELECTRICAL SYSTEM FIRE OR SMOKE (S-6) Procedures................ AS REQUIRED

SMOKE EVACUATION Procedure (S-11)....... AS REQUIRED

END

END

TROUBLESHOOTING CONSIDERED?


Smoke

S-6 ORIGINAL

ELECTRICAL SYSTEM FIRE OR SMOKE

Condition: Smoke confirmed from electrical source.

Crew Oxygen Masks .....DON, 100% Smoke Goggles.............DON Crew Communication ...ESTABLISH Recirculation Fan..........PUSH OUT


No

Yes Electrical Power to

Affected Equipment..OFF SMOKE EVACUATION

Procedure (S-11) ........ AS REQUIRED

Shed Buses ..................OFF No

Yes Relevant Inoperative Items: TAXI AND NOSE LANDING LIGHTS FLASHLIGHT RECHARGE SYSTEM SELCAL SYSTEM WINDSHIELD HEATING 2

SMOKE EVACUATION Procedure (S-11) ...... AS REQUIRED

Bus Ties ...................... OFF APU Generator ........... PUSH OUT


SMOKE ORIGIN IDENTIFIED?

END

SMOKE DISSIPATES?

END


Smoke

ORIGINAL S-7

CONTINUED FROM PREVIOUS PAGE Battery 2 ......................OFF

Central Bus deenergized. No

Yes Relevant Inoperative Items: TAXI AND NOSE LANDING LIGHTS FLASHLIGHT RECHARGE SYSTEM SELCAL SYSTEM WINDSHIELD HEATING 2

SMOKE EVACUATION Procedure (S-11) ......AS REQUIRED

Fuel Pumps .................1B AND

2A OR 2C Battery 2 ......................AUTO Battery 1 ......................OFF Generators 1 and 3 .....PUSH OUT

DC Bus 1 and Essential Bus 1 deenergized.

No

Yes Icing Conditions..........EXIT/AVOID Altitude ........................MAX 25’000 FT,

MIN MEA At pilot’s discretion, on Reversionary Panel:

SG1............................PUSH IN MFD 1 control is possible through MFD 2 Bezel.

Brake effectiveness will be reduced. Monitor fuel quantity indication 1 through RMU 2.


SMOKE DISSIPATES?

SMOKE DISSIPATES?

END


Smoke

S-8 ORIGINAL

CONTINUED FROM PREVIOUS PAGE COM 2 on Digital

Audio Panel 1 .......PUSH IN Relevant Inoperative Items:

Autopilot Audio System 1 GPWS FMS 1 Transponder 1 RA 1 DME 1 Main Pitch Trim TCAS Pack 1 Speed Brake RMU 1 ADF/VHF/VOR/ILS/MB 1 Landing Gear Control (Down Override) W/S 1 Heating and Wiper

Do not set Thrust Lever 1 below idle in flight. Anticipate flap actuation. Do not actuate Thrust Reverser 1. Landing configuration:

Flaps........................22° VREF..........................VREF 45° + 10 KIAS

CAUTION: MULTIPLY BY 1.42 THE FLAPS 45° UNFACTORED LANDING DISTANCE.

SMOKE EVACUATION Procedure (S-11) .....AS REQUIRED

Generators 1 and 3 ...PUSH IN Battery 1.....................AUTO Fuel Pumps................1A OR 1C AND

2B Battery 2.....................OFF Generators 2 and 4 ...PUSH OUT

DC Bus 2 and Essential Bus 2 deenergized.


END


Smoke

ORIGINAL S-9

CONTINUED FROM PREVIOUS PAGE No

Yes Icing Conditions..........EXIT/AVOID Altitude ........................MAX 25’000 FT,

MIN MEA Airspeed ......................MAX 250 KIAS At pilot’s discretion, on Reversionary Panel:

SG 2 ..........................PUSH IN MFD 2 control is possible through MFD 1 Bezel.

Monitor fuel quantity indication 2 through RMU 1. COM 1 on Digital

Audio Panel 2...........PUSH IN Relevant Inoperative Items:

Transponder 2 Stick Pusher

Audio System 2 RMU 2

ISIS/Standby Altimeter FMS 2

Standby Attitude Indicator Pack 2

W/S 2 Heating and Wiper Steering

Landing Gear Control Landing lights

ADF 2/VOR 2/DME 2/VHF 2/ ILS 2/MB 2

Do not set Thrust Lever 2 below idle in flight. Do not actuate Thrust Reverser 2. Brake effectiveness will be reduced. When necessary to extend landing gear:

Gear Electrical Override.................DOORS

..............................WAIT 3 SECS CONTINUES ON NEXT PAGE

SMOKE DISSIPATES?


Smoke

S-10 ORIGINAL

CONTINUED FROM PREVIOUS PAGE Gear Electrical

Override................ GEAR/DOORS

Anticipate flap actuation. Landing configuration:

Flaps......................... 22° VREF........................... VREF 45° + 10 KIAS

CAUTION: MULTIPLY BY 1.42 THE FLAPS 45° UNFACTORED LANDING DISTANCE.

SMOKE EVACUATION Procedure (S-11) ...... AS REQUIRED

Generators 2 and 4 .... PUSH IN Battery 2...................... AUTO APU Generator ........... PUSH IN Bus Ties ...................... AUTO Shed Buses ................ AUTO Backup Battery........... PUSH OUT

SMOKE EVACUATION Procedure (S-11)...... AS REQUIRED

END

END


Smoke

ORIGINAL S-11

SMOKE EVACUATION

Condition: Smoke or odor inside the cabin and/or cockpit requiring removal.

Cockpit Door ...............CLOSE Recirculation Fan........PUSH OUT Gasper Fan ..................PUSH OUT Pressurization

Manual Controller ....1 O'CLOCK POSITION

................................WAIT 15 SECS Pressurization Mode

Selector ....................PUSH IN (MAN) Passenger Oxygen .....AS REQUIRED

Fast

Normal Pressurization Manual

Controller .................AS REQUIRED Turn the controller clockwise towards UP to adjust desired evacuation rate.

Pressurization Manual Controller .................UP

Packs 1 and 2 ..............PUSH OUT


END

DESIRED EVACUATION RATE?


Smoke

S-12 ORIGINAL

CONTINUED FROM PREVIOUS PAGE Bleeds (at least one) ....PUSH IN

Altitude..........................10’000 FT OR MEA, WHICHEVER IS HIGHER

Recover cabin pressure as soon as smoke has been cleared. EMERGENCY DESCENT

Procedure (NAP-6)....AS REQUIRED

END

EMERGENCY/ABNORMAL PROCEDURES Non Annunciated

REVISION 8 NAP-1 Q

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TABLE OF CONTENTS AIR CONDITIONING SMOKE ............................refer to S-4

AILERON RUNAWAY................................................NAP-3

AIRPLANE OVERSPEED..........................................NAP-4

APU OVERTEMPERATURE .....................................NAP-4

CABIN FIRE OR SMOKE ...................................refer to S-5

DITCHING .................................................................NAP-5

DUAL ENGINE FAILURE ...........................refer to EAP 6-3

ELECTRICAL SYSTEM FIRE OR SMOKE....................................................refer to S-6

EMERGENCY DESCENT..........................................NAP-6

EMERGENCY EVACUATION ...................................NAP-7

ENGINE FIRE, SEVERE DAMAGE OR SEPARATION ........................................refer to EAP 6-6

ENGINE OIL LOW PRESSURE .................refer to EAP 6-7

FORCED LANDING...................................................NAP-8

INADVERTENT SPOILER OPEN................refer to EAP 8-7

JAMMED AILERON...................................................NAP-10

JAMMED ELEVATOR ...............................................NAP-10

JAMMED RUDDER ...................................................NAP-11

PITCH TRIM INOPERATIVE .......................refer to EAP 8-3

PITCH TRIM RUNAWAY...........................................NAP-13

RAPID CABIN DEPRESSURIZATION ......................NAP-14

ROLL TRIM RUNAWAY ............................................NAP-3

SMOKE EVACUATION ......................................refer to S-11

ABNORMAL ENGINE START ...................................NAP-15

ABNORMAL LANDING GEAR EXTENSION.............NAP-16

AILERON ARTIFICIAL FEEL INOPERATIVE............NAP-17

ASYMMETRIC RUDDER OPERATION ....................NAP-17

CABIN DEPRESSURIZATION ...................refer to EAP 1-12

CAS MESSAGE MISCOMPARISON.........................NAP-17

CRACKED WINDSHIELD......................................... NAP-28

DISPLAY FAILURE .....................................refer to EAP 2-6

CDU DATA BUS FAIL FMS ANNUNCIATION...........NAP-18

EMERGENCY/PARKING BRAKE HANDLE DISAGREE ............................................NAP-18

ENGINE ABNORMAL VIBRATION............................NAP-18

ENGINE AIRSTART ..................................................NAP-19

ENGINE CONTROL FAILURE ....................refer to EAP 6-9

ENGINE FAILURE/SHUTDOWN...............................NAP-23

ENGINE OIL HIGH PRESSURE ...............................NAP-24



NAP-2 REVISION 8

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ENGINE OIL HIGH TEMPERATURE ...................... NAP-24

ENGINE OIL LOW LEVEL ....................................... NAP-24

ENGINE OIL LOW PRESSURE .............................. NAP-25

ENGINE OVERTEMPERATURE............................. NAP-25

ENGINE TAILPIPE FIRE ......................................... NAP-26

ERRONEOUS STALL PROTECTION ACTUATION.............................NAP-26A

GEAR LEVER CANNOT MOVE UP AFTER TAKEOFF ......................................... NAP-27

GUST LOCK FAILURE ............................................ NAP-27

IC BUS FAILURE....................................refer to EAP 2-8

IC FAILURE ............................................refer to EAP 2-8

IMPAIRED OR CRACKED WINDSHIELD ............... NAP-28

IRS/MSU FAILURE ANNUNCIATION ..................... NAP-29

LOSS OF ENGINE INDICATIONS .......................... NAP-30

LOSS OF PRESSURIZATION INDICATION ........... NAP-31

MAIN DOOR BLOCKED.......................................... NAP-33

NAV/FLIGHT INSTRUMENTS FAILURE................. NAP-33

ONE ENGINE INOPERATIVE APPROACH AND LANDING............................... NAP-35

OVERWEIGHT LANDING ....................................... NAP-36

OXYGEN LEAKAGE................................................ NAP-37

PARTIAL OR GEAR UP LANDING ......................... NAP-38

PRESSURIZATION AUTOMATIC SYSTEM FAILURE ............................refer to EAP 1-12

RADIO ALTIMETER FAIL.......................refer to EAP 2-14

RUDDER ARTIFICIAL FEEL INOPERATIVE .......... NAP-39

RUDDER RUNAWAY .............................................. NAP-40

SINGLE ENGINE BLEED OPERATION IN ICING CONDITIONS ...................................... NAP-41

STEERING SYSTEM INOPERATIVE.....refer to EAP 12-9

STIFFENED ELEVATOR......................................... NAP-41

STRUCTURAL DAMAGE ........................................ NAP-42

SUSPECTED FUEL LEAK....................................... NAP-42

UNCOMMANDED AILERON DISCONNECTION.... NAP-43

UNCOMMANDED ELEVATOR DISCONNECTION.......................... NAP-43

UNCOMMANDED SWERVING ON GROUND.....................................refer to EAP 12-9

UNRELIABLE AIRPEED.......................................... NAP-44

VOLCANIC ASH ...................................................... NAP-44

YAW TRIM RUNAWAY............................................ NAP-40


REVISION 10 NAP-3 Q

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RUNAWAY PERSISTS?

AILERON RUNAWAY/ ROLL TRIM RUNAWAY

Condition: Sudden roll.

Quick Disconnect Button.......................PRESS AND HOLD

Aileron Shutoff Sys 1 and 2...................PUSH OUT

Roll Trim CB (F22 or F23) ......................PULL Quick Disconnect Button.......................RELEASE Airspeed ..................................................MAX 250 KIAS Roll Trim Position...................................CHECK

No Yes

Roll Trim CB (F22) ..................................PUSH Prepare to overcome uncommanded roll. Aileron Shutoff Sys 1 .............................PUSH IN

No

Yes

Aileron Shutoff Sys 1 .............................PUSH OUT Prepare to overcome uncommanded roll. Aileron Shutoff Sys 2 .............................PUSH IN

No

Yes

Aileron Shutoff Sys 2 .............................PUSH OUT Expect greater aileron control force. If required both pilots should act together to control the airplane.

Avoid airports with anticipated turbulence or crosswind. Perform a long final approach. Landing configuration:

Landing Gear .....................................DOWN Flaps ...................................................22° VREF......................................................VREF45 + 10 KIAS

CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.45.

Aileron Shutoff Sys 1 and 2...................PUSH IN Roll trim is inoperative. Use aileron and rudder to control the airplane.

END

RUNAWAY STILL PERSISTS?

ROLL TRIM IN NEUTRAL POSITION?

END


NAP-4 ORIGINAL Q

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EGT REMAINS HIGH?

AIRPLANE OVERSPEED

Aural Warning: Voice Message HIGH SPEED.

INDICATION: Airspeed and Mach indications in red range.

Airspeed...................................................MAX VMO/MMO

APU OVERTEMPERATURE

EICAS Indication: EGT enter amber or red range. EICAS Caution: APU FAIL may be presented.

APU Bleed ...............................................PUSH OUT

.............................................................WAIT 10 SECONDS

No

Yes

APU Fuel Shutoff Valve ..........................PUSH IN

APU Master Knob....................................OFF

CAUTION: DO NOT ATTEMPT TO RESTART APU.

Consider the APU shutdown if it is not necessary.

END

END

END


REVISION 10 NAP-5 Q

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ICING CONDITIONS?

DITCHING

ATC ..........................................................NOTIFY

Transponder............................................7700 ELT ...........................................................ON Emerg Lts ................................................ON

FSTN Belts...............................................ON Cabin Crew (if applicable)......................NOTIFY Passengers (and Crew)..........................PREPARE FOR

DITCHING Below 10’000 ft:

Pressurization Dump Button............PUSH IN (ON)

EGPWS CB (D2 or J8) .......................PULL Aural Warn CB’s (B4 and E29

or B4 and E30) ..............................PULL At 1’000 ft:

Fuselage Tank Transfer Knob..........TURN OFF Packs 1 and 2.....................................PUSH OUT Engine Bleeds 1 and 2 ......................PUSH OUT

Plan ditching parallel to the line of the wave crests. On final, level the wings and avoid skidding. Touchdown with 4o nose up attitude, and rate of descent less than 180 ft/min. Use only overwing emergency exits for passenger evacuation. Do not open remaining doors.

Ditching configuration: No

Yes

Landing Gear...........................................UP Flaps ........................................................22° If it is not possible to achieve the selected flap position, maintain airspeed according to the following:

FLAPS POSITION MIN AIRSPEED

0 to 8° VREF45 + 30 KIAS

9° to 21° VREF45 + 10 KIAS

22° VREF45 + 5 KIAS

Upon water contact: Thrust Levers 1 and 2 ....................... IDLE Start/Stop Selectors 1 and 2.............STOP APU .....................................................SHUTDOWN Fire Extinguishing Handles ..............PULL APU Fuel Shutoff ...............................PUSH IN Engine and APU Fire Extinguishing

Bottles (if necessary) ...................DISCHARGE Fuel Pumps Pwr.................................OFF Hydraulic Elec Pumps.......................OFF Evacuation ......................................... INITIATE

CONTINUES ON NEXT PAGE END


NAP-6 REVISION 8 Q

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Landing Gear......................................UP

Flaps....................................................45° If it is not possible to achieve the selected flap position, maintain airspeed according to the following:

FLAPS POSITION MINIMUM AIRSPEED


9° to 21° VREF45 + 10 KIAS

22° to 44° VREF45 + 5 KIAS

45° VREF45

Upon water contact: Thrust Levers 1 and 2........................IDLE Start/Stop Selectors 1 and 2 .............STOP APU .....................................................SHUTDOWN Fire Extinguishing Handles ..............PULL APU Fuel Shutoff ...............................PUSH IN Engine and APU Fire Extinguishing

Bottles (if necessary) ...................DISCHARGE Fuel Pumps Pwr.................................OFF Hydraulic Elec Pumps .......................OFF Evacuation..........................................INITIATE

EMERGENCY DESCENT

Cabin Crew ...........................................NOTIFY

FSTN Belts............................................ON

Thrust Levers .......................................IDLE

Speed Brakes .......................................OPEN

Airspeed ...............................................MAX 250 KIAS

Landing Gear........................................DOWN

Speed Brakes .......................................CHECK OPEN

Landing Gear........................................CHECK DOWN

Descent.................................................INITIATE

Transponder.........................................7700

Altitude .................................................MEA OR 10’000 FT, WHICHEVER IS HIGHER

CAUTION: IF STRUCTURAL DAMAGE IS SUSPECTED, USE THE FLIGHT CONTROLS WITH CAUTION AVOIDING HIGH MANEUVERING LOADS AND REDUCING AIRSPEED AS APPROPRIATE.

END

END


REVISION 4 NAP-7 Q

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Parking Brake ......................................APPLY

Cabin.....................................................DEPRESSURIZE

Fire Extinguishing Handles................PULL

APU Fuel Shutoff Valve ......................PUSH IN

Fuel Pumps Pwr 1 and 2.....................OFF

Hydraulic Elec Pumps 1 and 2 ..........OFF

Engines and APU Fire Extinguishing Bottles (if necessary) ...................DISCHARGE

Cabin Crew...........................................NOTIFY

Emerg Lts.............................................ON

Evacuation ........................................... INITIATE

ATC........................................................NOTIFY Before leaving the airplane: Batteries 1 and 2 .............................OFF

END


NAP-8 REVISION 10 Q

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ICING CONDITIONS?

FORCED LANDING

ATC...........................................................NOTIFY Transponder ............................................7700

ELT ...........................................................ON Emerg Lts.................................................ON FSTN Belts...............................................ON

Cabin Crew (if applicable) ......................NOTIFY Passengers (and Crew) ..........................PREPARE FOR

FORCED LANDING Below 10’000 ft:

Pressurization Dump Button ............PUSH IN (ON) EGPWS CB (D2 or J8)........................PULL Aural Warn CB’s (B4 and E29

or B4 and E30)...............................PULL When committed to land:

No

Yes

Landing Gear...........................................AS REQUIRED The decision to land with all gear up or with any gear extended is left to pilots. The choice of configuration is based on the number of gear available, airplane load distribution, controllability and conditions of the landing field. Ground spoilers and thrust reversers will not operate if any main gear is up.

Flaps.........................................................22° If it is not possible to achieve the selected flap position, maintain airspeed according to the following:


0 to 8° VREF45 + 30 KIAS 9° to 21° VREF45 + 10 KIAS

22° VREF45 + 5 KIAS

Just before touchdown:

Fuselage Tank Transfer Knob ..........TURN OFF

Fire Extinguishing Handles ..............PULL

APU Fuel Shutoff Valve.....................PUSH IN When the airplane stops:


Fuel Pumps Pwr 1 and 2 ...................OFF

Hydraulic Elec Pumps 1 and 2 .........OFF

Evacuation..........................................INITIATE


END


REVISION 7 NAP-9 Q

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Landing Gear...........................................AS REQUIRED

The decision to land with all gear up or with any gear extended is left to pilots. The choice of configuration is based on the number of gear available, airplane load distribution, controllability and conditions of the landing field. Ground spoilers and thrust reversers will not operate if any main gear is up.

Flaps ........................................................45°

If it is not possible to achieve the selected flap position, maintain airspeed according to the following:


0 to 8° VREF45 + 30 KIAS 9° to 21° VREF45 + 10 KIAS 22° to 44° VREF45 + 5 KIAS

45° VREF45

Just before touchdown:

Fuselage Tank Transfer Knob..........TURN OFF

Fire Extinguishing Handles ..............PULL

APU Fuel Shutoff Valve ....................PUSH IN

When the airplane stops:


Fuel Pumps Pwr 1 and 2 ...................OFF

Hydraulic Elec Pumps 1 and 2 ........OFF

Evacuation ......................................... INITIATE

END


NAP-10 REVISION 3 Q

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ICING CONDITIONS?

JAMMED AILERON Condition: Both control wheels can not be moved to

either side.

Aileron Disconnection Handle .............PRESS AND PULL

Autopilot ..................................................DISENGAGE

Airspeed...................................................MAX 200 KIAS

If the right control wheel is jammed, roll trim and artificial feel are not available.

Maintain bank angle below 20°. If both ailerons are jammed, use rudder to control the airplane.

Avoid abrupt and large aileron inputs.

Avoid airports with anticipated turbulence or crosswind.

No

Yes

Landing configuration: Landing Gear......................................DOWN Flaps....................................................22° VREF ......................................................VREF45 + 15 KIAS




JAMMED ELEVATOR

Condition: Both control columns can not be moved either forward or backward.

EICAS Warning: SPS 1-2 INOP may be presented.

EICAS Caution: STICK PUSHER FAIL may be presented.

Elevator Disconnection Handle ...........PRESS AND PULL

Autopilot ..................................................DISENGAGE

Airspeed...................................................MAX 200 KIAS If left elevator is jammed, Stick Pusher will not be available. Avoid airports with anticipated turbulence or crosswind.


END

END


REVISION 4 NAP-11 Q

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RUDDER FREE?

ICING CONDITIONS?

RUDDER FREE?


Pitch Trim ................................................AS REQUIRED Elevator authority to flare during landing may be reduced. If both elevators are jammed, pitch trim may be used to land the airplane.

Landing configuration: Landing Gear .....................................DOWN Flaps ...................................................22° VREF......................................................VREF45 + 10 KIAS


JAMMED RUDDER

Condition: Pedals can not be moved.

Command rudder through yaw trim. If required, use asymmetric thrust to control the airplane. Rudder Shutoff Sys 2 .............................PUSH OUT

No

Yes

Rudder Shutoff Sys 2 .............................PUSH IN

Rudder Shutoff Sys 1 .............................PUSH OUT

No

Yes

Airspeed ..................................................MAX 200 KIAS Avoid airports with anticipated turbulence or crosswind. Do not reduce engine thrust during flare.

No

Yes

Landing configuration:

Landing Gear .....................................DOWN

Flaps ...................................................22°

VREF......................................................VREF45 + 15 KIAS



END

END

END


NAP-12 REVISION 10 Q

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During final approach and landing run:

Pilot not flying: Steering Disengage Button .........PRESS AND HOLD

Steering Handle.......................................AS REQUIRED Use Steering Handle still keeping the Steering Disengage Button pressed.

After the touchdown:

Thrust Levers .....................................IDLE If necessary, use differential braking to steer the airplane.


Landing Gear......................................DOWN

Flaps....................................................45°

VREF ......................................................VREF45 + 5 KIAS


During final approach and landing run:

Pilot not flying: Steering Disengage Button .........PRESS AND HOLD

Steering Handle.......................................AS REQUIRED Use Steering Handle still keeping the Steering Disengage Button pressed.

CAUTION: DO NOT RELEASE THE NOSEWHEEL STEERING HANDLE UNTIL THE AIRPLANE IS COMPLETELY STOPPED.

After the touchdown:

Thrust Levers .....................................IDLE If necessary, use differential braking to steer the airplane.

END

END


REVISION 9 NAP-13 Q

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RUNAWAY PERSISTS?

PITCH TRIM RUNAWAY

Condition: Uncommanded pitch and trim indication changes.

EICAS Warning: AUTOPILOT FAIL may be presented.

EICAS Caution: AUTO TRIM FAIL may be presented.

Quick Disconnect Button .....................PRESS AND HOLD

NOTE: Do not change flap setting.

At safe altitude:

Pitch Trim Main Sys Cutout..............PUSH OUT

Pitch Trim Backup Sys Cutout.........PUSH OUT

Quick Disconnect Button .................RELEASE

WARNING: DO NOT OPEN SPEED BRAKE.

Prepare to overcome unwanted pitch change.

Pitch Trim Backup Sys Cutout ..............PUSH IN

Pitch Trim ................................................ACTUATE No Yes

Pitch Trim Backup Sys Cutout ..............PUSH OUT

Prepare to overcome unwanted pitch change.

Pitch Trim Main Sys Cutout...................PUSH IN No Yes Pitch Trim Main Sys Cutout...................PUSH OUT

PITCH TRIM INOPERATIVE Procedure (EAP 8-3)..........................ACCOMPLISH

Autopilot can be used. Autopilot ..................................................DISENGAGE

END

END

END



NAP-14 ORIGINAL Q

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APU ABNORMAL INDICATION PRESENTS?

RAPID CABIN DEPRESSURIZATION

Aural Warning: Voice Message CABIN. EICAS Indication: CAB ALT Value in red.

Condition: Cabin altitude has exceeded 10’000 ft.

Crew Oxygen Masks ...............................DON

Crew Communication .............................ESTABLISH

EICAS Pressurization Indication ...........CHECK

Passenger Oxygen..................................AS REQUIRED

If Emergency Descent is necessary:

FSTN Belts..........................................ON

Cabin Crew .........................................NOTIFY

Thrust Levers .....................................IDLE

Speed Brakes .....................................OPEN

Airspeed..............................................MAX 250 KIAS

Landing Gear......................................DOWN

Descent ...............................................INITIATE

Altitude................................................MEA OR 10’000 FT, WHICHEVER IS HIGHER

CAUTION: IF STRUCTURAL DAMAGE IS SUSPECTED, USE THE FLIGHT CONTROLS WITH CAUTION AVOIDING HIGH MANEUVERING LOADS AND REDUCING AIRSPEED AS APPROPRIATE.

Altitude................................................MEA OR 10’000 FT, WHICHEVER IS HIGHER

APU Parameters.................................CHECK

No

Yes

APU .....................................................OFF

END

END


REVISION 10 NAP-15 Q

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ABNORMAL ENGINE START

Condition: Any abnormal engine indication during engine start.

To abort start:

Associated Thrust Lever .................. IDLE

Associated Start/Stop Selector........STOP

No

Yes

Fire Extinguishing Handle .....................PULL

ENGINE FIRE, SEVERE DAMAGE OR SEPARATION Procedure (EAP 6-6) or ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)...........................ACCOMPLISH

No

Yes

FADEC in Command ..............................CHECK

FADEC Control Knob .............................ALTN No

Yes

Ignition.....................................................OFF Associated Start/Stop Selector.............START, THEN RUN

.............................................................WAIT 10 SECONDS N2 Indication ...........................................CHECK

No Yes

.............................................................WAIT 30 SECONDS Associated Start/Stop Selector.............STOP Ignition Selector .....................................AUTO Engine......................................................START

Do not attempt another start. ENGINE FAILURE/SHUTDOWN

Procedure (NAP-23)...........................ACCOMPLISH

END

FIRE OCCURS OR ENGINE STILL RUNNING?

END

ANOTHER START CONSIDERED?

FADEC ALTERNATES?

END

N2 INDICATES ROTATION?


NAP-16 ORIGINAL Q

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ABNORMAL LANDING GEAR EXTENSION

Condition: Landing gear has not extended by normal means.

Free Fall Electrical Override

NOTE: Hydraulic System 1 must be operative.


Landing Gear Lever ................................DOWN

Gear Electrical Override .........................DOORS

..............................................................WAIT 3 SECONDS

Gear Electrical Override .........................GEAR/DOORS

Landing Gear Indication.........................CHECK No Yes


Landing Gear Lever ................................UP

Gear Electrical Override .........................NORMAL

..............................................................WAIT 10 SECONDS

Free Fall Lever.........................................ACTUATE

Landing Gear Lever ................................DOWN

Landing Gear Indication.........................CHECK No Yes

Free Fall Lever.........................................CYCLE Cycle the free fall lever as necessary, limited to 10 times, leaving it at the latched position for 20 seconds between each cycle.

No

Yes

PARTIAL OR GEAR UP LANDING Procedure (NAP-38)...........................ACCOMPLISH

WHICH EXTENSION CONSIDERED?

THREE LEGS DOWN?

ANY LEG STILL UP?

END

END

ANY LEG STILL UP?


ORIGINAL NAP-17 Q

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AILERON ARTIFICIAL FEEL INOPERATIVE

Condition: Control Wheel excessively light and oversensitive.

Airspeed. .................................................MAX 200 KIAS Do not make abrupt and large aileron inputs.

ASYMMETRIC RUDDER OPERATION

Condition: Rudder pedals heavier to be moved to one side than the other.


No

Yes


CAS MESSAGE MISCOMPARISON

PFD Indication: CAS MSG in amber.

Reversionary Panel:

MFD 1 Knob........................................EICAS

MFD 2 Knob........................................EICAS

Pilot’s/Copilot’s EICAS messages........COMPARE

Discrepant message...............................CHECK Analyze the situation to check whether the discrepant message is spurious or not, and take the appropriate corrective action.

END

END

END

FAILURE PERSISTS?

END


NAP-18 REVISION 4 Q

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CDU DATA BUS FAIL FMS ANNUNCIATION

Condition: Affected FMS is not updating CDU. CDU DATA BUS FAIL message presented on FMS.

Affected FMS .................................... OFF, then ON Power down the FMS using the ON-OFF DIM key. DO NOT use the circuit breaker to cycle power to the FMS.

No

Yes

Affected FMS .................................... OFF

EMERGENCY/PARKING BRAKE HANDLE DISAGREE

Light: BRAKE ON with Emergency/Parking Brake Handle not actuated for more than 10 seconds.

Do not takeoff.

ENGINE ABNORMAL VIBRATION

EICAS Indication: Engine vibration enters amber range.

Associated Thrust Lever ........................REDUCE TO KEEP VIBRATION WITHIN LIMITS

No Yes

Monitor engine vibration.

Affected ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)...........................ACCOMPLISH

VIBRATION WHITIN GREEN LIMITS?

END

END

END

CDU DATA BUS FAIL MESSAGE PERSISTS?

END


ORIGINAL NAP-19

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ENGINE AIRSTART

Inoperative engine:

Fuel Pump Selector...........................A or B

Fuel Pump Pwr...................................ON

Ignition................................................AUTO

Start/Stop Selector ............................STOP

Engine Bleed......................................PUSH OUT

Thrust Lever....................................... IDLE

Engine Airstart Envelope.......................CHECK

ENGINE AIRSTART ENVELOPE

0

5000

10000

15000

20000

25000

30000

50 100 150 200 250 300 350

AL

TIT

UD

E -

ft

INDICATED AIRSPEED - KIAS

ASSISTED START

ASSISTED AND

WINDMILLING START

145J

AA

057A

- 1

6MA

Y20

06

AE 3007A ENGINES

NOTE: Shaded area may be below 1.23 VSR.



NAP-20 REVISION 8 Q

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Windmilling APU Assisted Crossbleed Assisted

CAUTION: ANTI-ICING SYSTEM WILL BE INOPERATIVE TEMPORARILY.

APU...........................................................START APU Bleed................................................PUSH IN XBleed......................................................AUTO OR OPEN Operative engine: Engine Bleed ......................................PUSH OUT Inoperative engine: Start/Stop Selector ............................START, THEN RUN Engine Indication ....................................MONITOR

No Yes

Engine Bleeds 1 and 2............................AS REQUIRED XBleed......................................................AUTO APU Bleed................................................AS REQUIRED

Consider another start procedure attempt.

Do not alternate FADEC.

NOTE: For AE3007A1E engines only, reset the FADEC of the inoperative engine if another airstart attempt is considered.

Operative Engine Bleed..........................AS REQUIRED Affected ENGINE FAILURE/SHUTDOWN

Procedure (NAP-23)...........................AS REQUIRED

Operative engine: N2 ........................................................MIN 80% XBleed.................................................AUTO OR OPEN

Engine Bleed ......................................PUSH IN Inoperative engine: Start/Stop Selector ............................START, THEN RUN Engine Indication ....................................MONITOR


START PROCEDURE CONSIDERED?

END

NORMAL START?

END


REVISION 8 NAP-21

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No

Yes

Engine Bleeds 1 and 2 ...........................AS REQUIRED XBleed......................................................AUTO APU Bleed ...............................................AS REQUIRED

Consider another start attempt.

NOTE: For AE3007A1E engines only, reset the FADEC of the inoperative engine if another airstart reattempt is considered.

Operative Engine Bleed .........................AS REQUIRED Affected ENGINE FAILURE/SHUTDOWN


NOTE: - Due to the characteristics listed below, the windmilling start should be accomplished only if an assisted start is not an option.

- For AE3007A1E engines only, reset the FADEC of the inoperative engine if another airstart reattempt is considered.

- Initiate windmilling start with N2 as high as possible. Windmilling starts are not possible with N2 below 10%. Once N2 is below 10%, it may not be recovered.

- Windmilling start is slower than an assisted start. - During a Windmilling start, if N2 reaches 30% and

keeps increasing, the loss of altitude may be minimized by reducing airspeed.

- ITT peaks may occur during windmilling starts above 10000 ft with airspeed below 290 knots. In this case, the engine may operate above the ITT limit, up to 850°C, for a maximum 5 seconds. Abort the start if the engine remains operating above the ITT limit for more than 5 seconds.

Airspeed: Above 10000 ft ...................................MIN 250 KIAS Below 10000 ft....................................220 TO 250 KIAS

N2 .............................................................MIN 10% Inoperative engine: Start/Stop Selector ............................START, THEN RUN

ITT and N2 ...............................................MONITOR


END

END

NORMAL START?


NAP-22 REVISION 8 Q

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No Yes

Engine Bleeds 1 and 2............................AS REQUIRED XBleed......................................................AUTO APU Bleed................................................AS REQUIRED

Consider another start attempt.

NOTE: For AE3007A1E engines only, reset the FADEC of the inoperative engine if another airstart reattempt is considered.

Operative Engine Bleed..........................AS REQUIRED Affected ENGINE FAILURE/SHUTDOWN


END

NORMAL START?

END


REVISION 4 NAP-23

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ENGINE FAILURE/SHUTDOWN

Condition: Loss of thrust on an engine or abnormal engine indication or precautionary shutdown.

Associated Thrust Lever........................ IDLE

Associated Start/Stop Selector.............STOP

NOTE: If engine shutdown does not occur, pull the associated fire extinguishing handle.

Engine Thrust Rating .............................CON

APU (if available) ....................................START

APU Bleed ...............................................AS REQUIRED

XBleed......................................................AS REQUIRED

Fuel ..........................................................BALANCE

Altitude ....................................................MAX 25’000 FT, MIN MEA

No Yes

Affected ENGINE AIRSTART Procedure (NAP-19)...........................ACCOMPLISH

TCAS........................................................TA ONLY



No Yes XBleed......................................................OPEN Altitude ....................................................MAX 15’000 FT,

MIN MEA If it is not possible to descend below 15’000 ft:

Icing Conditions ................................EXIT

ONE ENGINE INOPERATIVE

APPROACH AND LANDING Procedure (NAP-35)...........................AS REQUIRED

ENGINE RESTART CONSIDERED?

END

END

ICING CONDITIONS?


NAP-24 REVISION 4 Q

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ENGINE OIL HIGH PRESSURE

EICAS Indication: Oil pressure pointer in amber range.

No

Yes

Associated Procedure............................ACCOMPLISH

ENGINE OIL HIGH TEMPERATURE

EICAS Indication: Oil temperature pointer and digits become red.

Associated Thrust Lever ........................REDUCE No Yes No Yes

Altitude.....................................................MAX 25’000 FT, MINIMUM MEA

No

Yes


ENGINE OIL LOW LEVEL

MFD Indication: Oil level digits become amber.

Oil Pressure, Oil Temperature ........ MONITOR

Affected ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)..................... AS REQUIRED Consider shutting the engine down to preserve oil quantity, and if required restart it prior to landing.

END

FAILURE PERSISTS?

FAILURE PERSISTS?

ABOVE 25’000 FT?

END

OIL TEMPERATURE, OIL LEVEL OR ENGINE VIBRATION OUT OF LIMITS?

END


REVISION 4 NAP-25 Q

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ENGINE OIL LOW PRESSURE

EICAS Indication: Oil pressure in amber range.

Associated Thrust Lever........................REDUCE Reduce N2 below 88%.

ENGINE OVERTEMPERATURE

Condition: ITT pointer and digits flashing amber or red.

Associated Thrust Lever........................REDUCE No Yes

Operate at reduced thrust to keep ITT within limits.

Associated Bleed....................................PUSH OUT

Altitude ....................................................MAX 25’000 FT, MIN MEA

No Yes


Operate at reduced thrust to keep ITT within limits.

ITT INDICATION WITHIN LIMITS?

END

END

ITT INDICATION STILL OUT OF LIMITS?

END

END


NAP-26 REVISION 8 Q

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ENGINE TAILPIPE FIRE

Condition: Tailpipe fire was detected visually by crew or ground personnel. No EICAS message displayed.

Affected engine:

Thrust Lever .......................................IDLE Start/Stop Selector ............................STOP Ignition ................................................OFF Fuel Pump...........................................OFF XFEED Selector Knob .......................OFF Start/Stop Selector ............................START, THEN RUN

ITT.............................................................MONITOR ATC...........................................................NOTIFY

..............................................................WAIT 90 SECONDS Associated Start/Stop Selector .............STOP Associated Fire

Extinguishing Handle ........................PULL (DO NOT ROTATE)

If fire is not extinguished while the engine is motored, ground personnel support must be requested.

END


REVISION 5 NAP-26A Q

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ERRONEOUS STALL PROTECTION ACTUATION

Condition: Inadvertent shaker and/or pusher actuation.

Quick Disconnect Button.......................PRESS AND HOLD

Stall Protection Cutout 1 and 2 .............PUSH OUT

Quick Disconnect Button.......................RELEASE

Minimum Airspeed .................................FLAP MANEUVERING SPEED (PD-2)

Avoid skidding the airplane. No

Yes

Add 15 KIAS to go-around speed to prevent stall protection from being actuated. Landing configuration:


Flaps ...................................................22°

VREF......................................................VREF45 + 15 KIAS


Add 5 KIAS to go-around speed to prevent stall protection from being actuated. Landing configuration:


Flaps ...................................................45°

VREF......................................................VREF45 + 5 KIAS


ICING CONDITIONS?

END

END


NAP-26B REVISION 5 Q

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01

INTENTIONALLY BLANK


ORIGINAL NAP-27 Q

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GEAR LEVER CANNOT MOVE UP AFTER TAKEOFF

Condition: Landing gear cannot be moved to up position after takeoff in the normal manner.

.............................................................WAIT 10 SECONDS No Yes

Landing Gear Lever................................DO NOT MOVE LANDING GEAR AIR/GROUND SYSTEM

FAILURE Procedure (EAP 12-8) .......ACCOMPLISH

Downlock Release Button (DN LOCK REL).....................PRESS

Landing Gear Lever................................UP

GUST LOCK FAILURE

Light: GUST LOCK (amber).

On Ground In Flight

Consider diversion. Do not push control column full Nose Down. Avoid flying in turbulence conditions. Avoid airports with anticipated turbulence or crosswind.

Do not takeoff.

CONDITION?

END

END

LG AIR/GND FAIL MESSAGE DISPLAYED?

END

END


NAP-28 ORIGINAL Q

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FORWARD VISIBILITY GOOD IN ONE SIDE?

IMPAIRED OR CRACKED WINDSHIELD

Associated Ice Protection Windshield..........................................PUSH OUT

No Yes

Cockpit Door ...........................................CLOSE Oxygen Masks.........................................AS REQUIRED

Altitude.....................................................MEA OR 10’000 FT, WHICHEVER IS HIGHER

Pressurization Manual Controller .........1 O'CLOCK POSITION

.............................................................WAIT 15 SECONDS

Pressurization Mode Selector ...............PUSH IN (MAN)

Pressurization Manual Controller .........CAB MAX P = 1 PSI


Smoke Goggle.........................................DON

No

Yes

Pilot flying must be on non impaired side.

When reaching 10’000 ft:

Pressurization Mode Selector ..........PUSH OUT

Pressurization Dump Button ............PUSH IN

During approach and landing, when visibility is required:

Airspeed..............................................MAX 140 KIAS, MIN VREF45

Check no loose objects in the cockpit.

Direct Vision Window ........................REMOVE Landing must be made by looking through Direct Vision Window. Intercommunication will be impossible with window removed.

ONLY OUTER LAYER CRACKED?

END

END

END


ORIGINAL NAP-29 Q

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IRS/MSU FAILURE ANNUNCIATION

OPERATION PHASE LIGHT POWER ON ALIGNMENT IN FLIGHT

ALIGN

No light: Check IRS

CB’s. Set mode

select switch to ALIGN or NAV.

Press MSU Test switch. Annunciator bulb must be replaced if the other MSU annunciators do light.

Accomplish associated IRS ALIGNMENT FAULT Procedure (EAP 2-9).

Flashes: IRS data is not

normal. Accomplish

associated IRS OVERHEAT Procedure (EAP 2-11).

FAULT

Set mode select switch to OFF for at least 3 sec. Then set mode select switch back to ALIGN or NAV.

If the annunciator remains lighted, do not takeoff.

Associated with ALIGN annunciation: Check and

reenter latitude. Allow additional

time for alignment.

Try new alignment. Set mode select switch to OFF for at least 3 sec, then to ALIGN, and enter present position.

If on ground, do not takeoff.

Select the remaining IRU by pressing the IRS Button on the associated reversionary panel.

If necessary set mode select switch to ATT.

NO AIR

Do not takeoff.

*******

Operate IRU until flight completion.

If fault annunciator is ON or inertial data ceases to be transmitted by IRU, accomplish associated IRS OVERHEAT Procedure (EAP 2-11). IRS data is not normal.

BATT FAIL

Do not takeoff. ******* *******

ON BATT

Check IRS CB’s. If the annunciator

remains lighted, do not takeoff.

*******

The IRU operates on backup DC power and will operate for 30 minutes.

END


NAP-30 ORIGINAL Q

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LOSS OF ENGINE INDICATIONS

Condition: Loss of Thrust Mode, ITT, N1 and N2 indications.

No Yes

Associated FADEC .................................RESET No Yes

Associated FADEC .................................ALTN No

Yes

Associated ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)...........................AS REQUIRED

Associated ENGINE FAILURE/SHUTDOWN

Procedure (NAP-23)...........................ACCOMPLISH

END

ASSOCIATED ENGINE OPERATING?

FAILURE PERSISTS?

FAILURE PERSISTS?

END


ORIGINAL NAP-31 Q

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LOSS OF PRESSURIZATION INDICATION

Condition: Cabin altitude or cabin P is not being presented or during use of the pressurization manual control.

Use the remaining indications to maintain cabin altitude below 10’000 ft, according to the table below: 41000 FT

39000 FT

AIRPLANE/CABIN ALTITUDE CONVERSION TABLE FOR AIRPLANES WITH MAXIMUM ALTITUDE CEILING OF 39000 FT

AIRPLANE ALTITUDE

(ft)

CABIN ALTITUDE

(ft)

DIFFERENTIAL PRESSURE

(psi) 10000 800 4.211000 1100 4.412000 1300 4.713000 1500 4.914000 1700 5.215000 2000 5.416000 2200 5.617000 2400 5.818000 2600 6.019000 2800 6.220000 3100 6.421000 3300 6.622000 3500 6.723000 3800 6.824000 4000 7.025000 4200 7.126000 4500 7.227000 4700 7.428000 4900 7.529000 5200 7.630000 5400 7.731000 5600 7.832000 5900 7.833000 6200 7.934000 6400 8.035000 6700 8.036000 7000 8.037000 7300 8.138000 7700 8.139000 8000 8.1

If pressurization can not be maintained, refer to PRESSURIZATION AUTOMATIC SYSTEM FAILURE/CABIN DEPRESSURIZATION Procedure (EAP 1-12).

CONTINUES ON THE NEXT PAGE

END

AIRPLANE MAXIMUM ALTITUDE CEILING?


NAP-32 ORIGINAL Q

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AIRPLANE/CABIN ALTITUDE CONVERSION TABLE FOR AIRPLANES WITH MAXIMUM ALTITUDE CEILING OF 41000 FT

AIRPLANE ALTITUDE

(ft)

CABIN ALTITUDE

(ft)

DIFFERENTIAL PRESSURE

(psi) 10000 600 4.311000 900 4.512000 1100 4.813000 1300 5.014000 1500 5.315000 1700 5.516000 1900 5.717000 2100 6.018000 2300 6.219000 2500 6.420000 2700 6.621000 3000 6.722000 3200 6.923000 3400 7.024000 3600 7.225000 3800 7.326000 4000 7.527000 4200 7.628000 4500 7.729000 4700 7.830000 4900 7.931000 5100 8.032000 5400 8.133000 5600 8.134000 5800 8.235000 6100 8.236000 6400 8.337000 6700 8.338000 7100 8.339000 7400 8.340000 7700 8.341000 8000 8.4

If pressurization can not be maintained, refer to PRESSURIZATION AUTOMATIC SYSTEM FAILURE/CABIN DEPRESSURIZATION Procedure (EAP 1-12).

END


ORIGINAL NAP-33 Q

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MAIN DOOR BLOCKED

Light: DOOR BLOCKED (Attendant's Panel).

No

Yes

Hydraulic System 1 ................................OFF Main Door Alternative

Opening Valve....................................TURN CLOCKWISE AND HOLD

.............................................................WAIT 2 MINUTES

Outside Area ...........................................CHECK CLEAR

Door .........................................................OPEN

NAV/FLIGHT INSTRUMENTS FAILURE

LOCATION ANNUNCIATOR/FAILURE

ACTION

ATT: CAGE (amber)

Press the CAGE push button in order to recover attitude indication. Caging the ISIS in flight will result in loss of attitude indication for up to 10 seconds and the amber message ATT 10s will be presented during this time. Until attitude indication is available again use the primary indication source.

ISIS

ATT, ALT, SPD, M, HDG (red)

Use the primary indication source.

HDG FAIL (red)

Use cross-side heading by pressing the IRS button on associated reversionary panel or use RMU or standby attitude indicator. PFD and

MFD

HDG (amber)

Compare data with the Magnetic Compass. After identifying the failed side, use cross-side data by pressing the IRS button on associated reversionary panel.

MFD MENU INOP (amber) Crew awareness.


END

ON GROUND?


NAP-34 ORIGINAL Q

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LOCATION ANNUNCIATOR/FAILURE

ACTION

ATT FAIL (red) Use cross-side attitude by pressing the IRS Button on associated reversionary panel or use standby attitude indicator.

"X" (red) over IAS tape

Use cross-side airspeed by pressing the ADC button on associated reversionary panel or use standby airspeed indicator.

"X" (red) over altitude tape

Use cross-side altitude by pressing the ADC button on associated reversionary panel or use standby altimeter.

"X" (red) over course scale

Select another sensor.

VS (red) Use cross-side vertical speed by pressing the ADC button on associated reversionary panel.

ROL, PIT, ATT, IAS, or ALT

(amber)

Compare data with Standby Indicator. For altitude compare the PFD altimeters setting also. If required, use cross-side data by pressing the appropriate button on associated reversionary panel.

RA (amber) Compare both radio altimeter indications. If required, consider only the lower indication. Otherwise, disregard Radio Altitude.

RA1 (2) (amber) Radio altimeter automatic reversion has occurred. No action is required.

PFD

PFD or EICAS Blank or "X"

(red)

Use the MFD Knob to present the required information on MFD.

END


ORIGINAL NAP-35 Q

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ONE ENGINE INOPERATIVE APPROACH AND LANDING

Before Landing:

Inoperative Engine Thrust Lever.................................. IDLE


Thrust Rating .....................................TAKEOFF MODE

Fuel XFeed .........................................OFF

Autopilot/Yaw Damper ......................DISENGAGE Landing configuration:

Flaps ...................................................22°

VREF......................................................VREF45 + 10 KIAS


END


NAP-36 REVISION 8 Q

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OVERWEIGHT LANDING

No

Yes


CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY AT LEAST 1.45.

Reduce the engine thrust only after the touchdown.

Before touchdown: Emerg Lts ...........................................AS REQUIRED APU Fuel Shutoff Valve.....................CLOSE Rate of Descent..................................MAX 300 FT/MIN

Touch smoothly the runway surface.

Landing configuration: Landing Gear......................................DOWN Flaps....................................................45° VREF ......................................................VREF45

CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY AT LEAST 1.06.

Reduce the engine thrust only after the touchdown.

Before touchdown: Emerg Lts ...........................................AS REQUIRED APU Fuel Shutoff Valve.....................PUSH IN Rate of Descent..................................MAX 300 FT/MIN

Touch smoothly the runway surface.

END

ICING CONDITIONS?

END


ORIGINAL NAP-37 Q

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OXYGEN LEAKAGE

Condition: Evidence of oxygen leakage through the crew mask, mask hose, flow indicator (blinker), or oxygen line.

No Smoking ................................................. ON

No

Yes

Affected Mask .............................................. REMOVE FROM STOWAGE BOX

Stowage Box Doors..................................... CLOSE Shutoff Sliding Control ............................... ACTUATE Oxygen Pressure .........................................CHECK

No

Yes

Altitude .........................................................MEA OR 10’000 FT, WHICHEVER IS HIGHER

Keep one Portable Oxygen Cylinder available for the pilot of the affected side. The oxygen supply by the Portable Oxygen Cylinder will last at least 30 minutes. Oxygen Cylinder Shutoff Valve .................. OFF Altitude .........................................................MEA OR


END

END

IS THE LEAKAGE IN THE CREW MASK, MASK HOSE, OR FLOW INDICATOR?

OXYGEN PRESSURE BELOW MINIMUM REQUIRED FOR DISPATCH?

END


NAP-38 REVISION 10 Q

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PARTIAL OR GEAR UP LANDING

Condition: Airplane committed to land with gear up or in transit.

EICAS Indication: Abnormal landing gear position.

EICAS Warning: LG/LEVER DISAGREE may be presented.

ATC...........................................................NOTIFY Burn fuel to reduce touchdown speed. Transponder ............................................7700 FSTN Belts...............................................ON Cabin Crew ..............................................NOTIFY Passengers (and Crew) ..........................PREPARE FOR

EMERGENCY LANDING AND EVACUATION

Below 10’000 ft: GPWS CB (D2 or J8) ..........................PULL Aural Warn CB’s (B4 and E29

or B4 and E30)...............................PULL Emerg Lts ...........................................ON ELT ......................................................ON

Prior to approach: Hydraulic Elec Pumps 1 and 2 .........OFF Cabin ...................................................DEPRESSURIZE Engine Bleeds 1 and 2.......................PUSH OUT

When committed to land: FUS TK XFER .....................................OFF APU Master.........................................OFF APU Fuel Shutoff Valve.....................PUSH IN Landing Gear......................................AS REQUIRED

The decision to land with all gear up or with any gear extended is left to pilots. Ground spoilers, thrust reversers, steering and normal brakes may not operate if any main gear is up.

No Yes

Flaps.........................................................22° If it is not possible to achieve the selected flap position, maintain airspeed according to the following:

FLAPS POSITION MIN AIRSPEED0 to 8° VREF45 + 30 KIAS

9° to 21° VREF45 + 10 KIAS22° to 44° VREF45 + 5 KIAS

45° VREF45

Apply thrust reverser (if available) after touchdown. When the airplane stops:

Engines START/STOP Selectors......STOP Fire Extinguishing Handles ..............PULL AND ROTATE APU Fuel Shutoff Valve.....................CLOSE

ICING CONDITIONS?



REVISION 7 NAP-39 Q

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CONTINUED FROM PREVIOUS PAGE Engines and APU Fire Extinguishing

Bottles (if necessary) ...................DISCHARGE Fuel Pumps Pwr 1 and 2 ...................OFF Evacuation ......................................... INITIATE

Before leaving the airplane: Batteries 1 and 2................................OFF

Flaps ........................................................45° If it is not possible to achieve the selected flap position, maintain airspeed according to the following:

FLAPS POSITION MIN AIRSPEED0 to 8° VREF45 + 30 KIAS

9° to 21° VREF45 + 10 KIAS22° to 44° VREF45 + 5 KIAS

45° VREF45

Apply thrust reverser (if available) after touchdown. When the airplane stops:

Engines START/STOP Selectors .....STOP Fire Extinguishing Handles ..............PULL AND ROTATE APU Fuel Shutoff Valve ....................CLOSE Engines and APU Fire Extinguishing

Bottles (if necessary) ...................DISCHARGE

Fuel Pumps Pwr 1 and 2 ...................OFF Evacuation ......................................... INITIATE

Before leaving the airplane: Batteries 1 and 2................................OFF

RUDDER ARTIFICIAL FEEL INOPERATIVE

Condition: Rudder pedals become light and do not center by themselves. Yaw trim does not operate properly.


No Yes


Expect greater rudder pedal force. If required, both pilots should act together to control the airplane.

Consider the use of aileron to help in yaw control, and asymmetric thrust to trim the airplane. Avoid airports with anticipated turbulence or crosswind.

END

FAILURE PERSISTS?

END

END


NAP-40 ORIGINAL Q

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YAW TRIM DISPLACED FROM NEUTRAL?

RUDDER/YAW TRIM RUNAWAY

Condition: Sudden uncommanded yaw.

EICAS Indication: Associated yaw trim indication changes.

Quick Disconnect Button .....................PRESS AND HOLD

Rudder Shutoff Sys 1 and 2 .................PUSH OUT


Yaw Trim Position...................................CHECK

No

Yes

Yaw Trim CB (F12) ..................................PULL

Quick Disconnect Button.......................RELEASE Rudder Shutoff Sys 1 and 2...................PUSH IN

Quick Disconnect Button.......................RELEASE

Prepare to overcome uncommanded yaw. Rudder Shutoff Sys 1 .............................PUSH IN

No

Yes

Rudder Shutoff Sys 1 .............................PUSH OUT Prepare to overcome uncommanded yaw.


No

Yes


LAND AT NEAREST SUITABLE AIRPORT. Avoid airports with anticipated turbulence or crosswind.

Expect greater rudder pedals force. If required, both pilots should act together to control airplane.

Consider the use of aileron to help in yaw control, and asymmetric thrust to trim the airplane.

END

RUNAWAY PERSISTS?


END


ORIGINAL NAP-41

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SINGLE ENGINE BLEED OPERATION IN ICING CONDITIONS

XBleed........................................................ OPEN

Altitude ...................................................... MAX 15’000 FT, MIN MEA

If it is not possible to descend below 15’000 ft:

Icing Conditions .................................. EXIT Refer to associated anti-icing failure procedure if any message is presented.

STIFFENED ELEVATOR

Condition: Elevator control columns movement is stiffened.

EICAS Warning: AUTOPILOT FAIL (may be presented), SPS 1-2 INOP (may be presented).

EICAS Caution: STICK PUSHER FAIL (may be presented).

Autopilot .................................................... DISENGAGE

Pitch Trim .................................................. AS REQUIRED

Avoid abrupt and large elevator inputs.

Consider descent to a warmer altitude. Freezing conditions may lead to de/anti-icing fluids residues to stiffen the elevator.

No

Yes

JAMMED ELEVATOR Procedure (NAP-10)............................. ACCOMPLISH

END

END

ELEVATOR CONTROL COLUMNS MOVEMENT RECOVERED?

END


NAP-42 REVISION 3 Q

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STRUCTURAL DAMAGE

LAND AT THE NEAREST SUITABLE AIRPORT. At safe altitude, evaluate airplane aero dynamical behavior and take extra caution varying airspeed and attitude. Use the flight controls with caution avoiding high maneuvering loads.

Aileron and Rudder deflection ................ MAX 30%

Airspeed under turbulence ...................... MAX 200 KIAS

No

Yes

Oxygen Masks........................................... AS REQUIRED

Altitude....................................................... MEA OR 10’000 FT, WHICHEVER IS HIGHER

When reaching 10’000 ft:

Pressurization Dump Button............ PUSH IN

Rate of Descent......................................... MAX 300 FT/MIN Land as smooth as possible.

SUSPECTED FUEL LEAK

Condition: - FMS Fuel Remaining quantity is above the MFD or EICAS total fuel indication.

- Excessive Fuel flow from one of the engines.

- Fuel imbalance develops. - Fuel quantity of a tank decreases at an

abnormal rate.

No

Yes

LAND AT THE NEAREST SUITABLE AIRPORT. XFEED ...........................................................OFF Asymmetric Thrust ......................................AS REQUIRED

Use crossfeed operation in order to achieve fuel balance.


END

FUSELAGE DAMAGED OR SUSPECTED DAMAGED?

FMS FUEL REMAINING QUANTITY IS MORE THAN 300 KG ABOVE MFD

END


REVISION 3 NAP-43 Q

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Set engines at the same N1 and compare the Fuel Flow indications. No Yes

At pilot’s discretion.


When the desired balance is achieved:

XFEED........................................................... OFF

Monitor total fuel indication on MFD Fuel Page with FMS Fuel Remaining information.

UNCOMMANDED AILERON OR ELEVATOR DISCONNECTION

Light: Amber ELEV DISC or AIL DISC on Pedestal.

Condition: One control column or control wheel moves independently of the other.

Affected Surface Disconnection

Handle...................................................... PULL If aileron is affected, aileron artificial feel not available on left side.

Avoid airports with anticipated turbulence or crosswind.

FUEL FLOW INDICATION SUGGESTS FUEL LEAK?

END

END

END


NAP-44 REVISION 8 Q

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UNRELIABLE AIRSPEED

Autopilot/Yaw Damper..................... DISENGAGE

Flight Director 1 & 2 ......................... OFF

Rudder Shutoff Sys 1....................... PUSH OUT

CAUTION: AVOID USING THE SPEEDBRAKE.

Attitude/Thrust ................................. ADJUST Maintain airplane control. Refer to Unreliable Airspeed tables (PD-2A) in the Performance Data section. Altitude and/or Vertical Speed indications may also be unreliable.

Ground speed indication is available in the FMS for reference.

VOLCANIC ASH

LAND AT THE NEAREST SUITABLE AIRPORT. Volcanic Ash Area .................................... EXIT/AVOID

APU (if available)....................................... START

Thrust Levers (if altitude permits)........... IDLE

Anti-Icing Buttons (Engine, Wing and Stabilizer........................................ PRESSED

Ice Detection Override Knob.................... ALL

ITT............................................................... MONITOR No

Affected Engine......................................... SHUT DOWN After affected engine has cooled down:

Affected Engine ................................... RESTART If the affected engine fails to restart, repeated attempts should be made immediately.

Restore systems to normal operation.

ATC............................................................. NOTIFY

END

SPEED INDICATION ON BOTH PFD BELOW 135

Yes

No

END

ITT INCREASES?

Yes

EMERGENCY/ABNORMAL PROCEDURES Index

REVISION 9 EAP 0-1

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INDEX BY EICAS MESSAGE

TYPE MESSAGE PAGE OR

INSTRUCTION

AIRPLANE FUEL LOAD EAP 9-3 APU FIRE EAP 3-3 ATTCS FAIL EAP 6-3 AUTOPILOT FAIL EAP 2-3 BAGG SMOKE S-3 BATT 1 OVTEMP EAP 5-3 BATT 2 OVTEMP EAP 5-3 BLD 1 LEAK EAP 1-4 BLD 1 OVTEMP EAP 1-5 BLD 2 LEAK EAP 1-4 BLD 2 OVTEMP EAP 1-5 BLD APU LEAK EAP 1-3 E1 ATTCS NO MRGN EAP 6-5 E1 LOW N1 Crew Awareness

E1 OIL LOW PRESS EAP 6-7 E2 ATTCS NO MRGN EAP 6-5 E2 LOW N1 Crew Awareness

E2 OIL LOW PRESS EAP 6-7 ELEC ESS XFR FAIL EAP 5-3 ENG 1 FIRE EAP 6-6 ENG 2 FIRE EAP 6-6 ENG 1-2 OUT EAP 6-3 FUEL 1 LO LEVEL EAP 9-3 FUEL 2 LO LEVEL EAP 9-3 FUEL XFER CRITICAL EAP 9-4 ICE COND-A/I INOP EAP 11-3 LAV SMOKE S-3 LG/LEVER DISAGREE EAP 12-3 MAIN DOOR OPN EAP 4-3 NO TAKEOFF CONFIG EAP 14-4 PTRIM BACKUP INOP EAP 8-3 PTRIM MAIN INOP EAP 8-3 SPS 1 INOP EAP 14-3 SPS 1-2 INOP EAP 14-3

W A R N I N G

SPS 2 INOP EAP 14-3


EAP 0-2 REVISION 9

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INSTRUCTION

115 VAC BUS OFF EAP 5-4 A/ICE LOW CAPACIT EAP 11-4 A/ICE SWITCH OFF EAP 11-4 ACCESS DOORS OPN EAP 4-4 AIL SYS 1 INOP EAP 8-5 AIL SYS 1-2 INOP EAP 8-5 AIL SYS 2 INOP EAP 8-5 AOA 1 HEAT INOP EAP 11-4 AOA 2 HEAT INOP EAP 11-4 AP AIL MISTRIM EAP 2-3 AP ELEV MISTRIM EAP 2-3 APU BLD VLV FAIL EAP 1-5 APU CNTOR CLSD EAP 3-4 APU EXTBTL INOP EAP 7-3 APU FAIL EAP 3-4 APU FIREDET FAIL EAP 7-3 APU FUEL LO PRESS EAP 3-5 APU FUEL SOV INOP EAP 9-5 APU GEN OFF BUS EAP 5-12 APU GEN OVLD EAP 5-12 APU OIL HI TEMP EAP 3-6 APU OIL LO PRESS EAP 3-6 AURAL WARN FAIL EAP 14-6 AUTO TRIM FAIL EAP 2-3 BAGG ACCESS OPN EAP 4-5 BAGG EXTBTL INOP EAP 7-4 BAGGAGE DOOR OPN EAP 4-4 BATT1 OFF BUS EAP 5-4 BATT2 OFF BUS EAP 5-4 BKUP BATT OFF BUS EAP 5-4 BLD 1 LOW TEMP EAP 1-6 BLD 1 VLV FAIL EAP 1-7 BLD 2 LOW TEMP EAP 1-6 BLD 2 VLV FAIL EAP 1-7 BRAKE DEGRADED EAP 12-5 BRAKE OVERHEAT EAP 12-4 BRK INBD INOP EAP 12-6 BRK OUTBD INOP EAP 12-6 CHECK IC 1 SW Crew Awareness

CHECK IC 2 SW Crew Awareness

CHECK PFD 1 EAP 2-6

CHECK PFD 2 EAP 2-6

C A U T I O N

CHK IC CONFIG Crew Awareness


REVISION 9 EAP 0-3

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INSTRUCTION

CLR ICE 1 Crew Awareness

CLR ICE 2 Crew Awareness

CLR /I INOP 1 Crew Awareness

CLR /I INOP 2 Crew Awareness

CREW OXY LO PRESS EAP 13-3 CROSS BLD FAIL EAP 1-8 CROSS BLD SW OFF Crew Awareness

DAU AC ID MISCMP Crew Awareness

DAU1 A FAIL EAP 2-4 DAU1 ENG MISCOMP EAP 2-5 DAU1 SYS MISCOMP EAP 2-5 DAU1 WRN MISCOMP EAP 2-5 DAU2 A FAIL EAP 2-4 DAU2 ENG MISCOMP EAP 2-5 DAU2 SYS MISCOMP EAP 2-5 DAU2 WRN MISCOMP EAP 2-5 DC BUS 1 OFF EAP 5-5 DC BUS 2 OFF EAP 5-6 DFDR FAIL Crew Awareness

E1 A/ICE FAIL EAP 11-5 E1 ATS SOV OPN EAP 6-8 E1 CTL FAIL EAP 6-9 E1 EXCEEDANCE Crew Awareness

E1 EXTBTLA INOP EAP 7-5 E1 EXTBTLB INOP EAP 7-5 E1 FIREDET FAIL EAP 7-4 E1 FPMU NO DISP Crew Awareness

E1 FUEL LO PRESS EAP 9-6 E1 FUEL LO TEMP EAP 9-7 E1 FUEL SOV INOP EAP 9-7 E1 NO DISP Crew Awareness

E2 A/ICE FAIL EAP 11-5 E2 ATS SOV OPN EAP 6-8 E2 CTL FAIL EAP 6-9 E2 EXCEEDANCE Crew Awareness

E2 EXTBTLA INOP EAP 7-5 E2 EXTBTLB INOP EAP 7-5 E2 FIREDET FAIL EAP 7-4 E2 FPMU NO DISP Crew Awareness

E2 FUEL LO PRESS EAP 9-6 E2 FUEL LO TEMP EAP 9-7 E2 FUEL SOV INOP EAP 9-7 E2 NO DISP Crew Awareness

ELEC EMERG ABNORM EAP 5-7

C A U T I O N

ELEKBAY OVTEMP EAP 2-7


EAP 0-4 REVISION 9

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INSTRUCTION

EMERG EXIT OPN EAP 4-5 EMERG LT NOT ARMD EAP 5-7 EMRG BRK LO PRES EAP 12-7 ENG NO TO DATA Crew Awareness

ENG REF A/I DISAG Crew Awareness

ENG1 OUT EAP 6-10 ENG1 REV DISAGREE EAP 6-12 ENG1 REV FAIL EAP 6-12 ENG1 TLA FAIL EAP 6-11 ENG2 OUT EAP 6-10 ENG2 REV DISAGREE EAP 6-12 ENG2 REV FAIL EAP 6-12 ENG2 TLA FAIL EAP 6-11 ESS BUS 1 OFF EAP 5-8 ESS BUS 1-2 OFF EAP 5-10 ESS BUS 2 OFF EAP 5-9 FADEC ID NO DISP Crew Awareness

FLAP FAIL EAP 8-6 FUEL IMBALANCE EAP 9-13 FUEL TANK LO TEMP EAP 9-9 FUEL TK VENT OPEN EAP 9-10 FUEL XFEED FAIL EAP 9-8 FUEL XFEED MISCMD EAP 9-9 FUEL XFER 1 INOP EAP 9-11 FUEL XFER 2 INOP EAP 9-11 FUEL XFER CHECK EAP 9-10 FUEL XFER OVFLOW EAP 9-16 FUELING DOOR OPN Crew Awareness FUSELAGE FUEL IMB EAP 9-13 GEN 1-2-3-4 OFF BUS EAP 5-13 GEN 1 OFF BUS EAP 5-12 GEN 1 OVLD EAP 5-12 GEN 2 OFF BUS EAP 5-12 GEN 2 OVLD EAP 5-12 GEN 3 OFF BUS EAP 5-12 GEN 3 OVLD EAP 5-12 GEN 4 OFF BUS EAP 5-12 GEN 4 OVLD EAP 5-12 HGS FAIL Crew Awareness

HS VLV 1 FAIL EAP 1-8 HS VLV 2 FAIL EAP 1-8 HYD SYS 1 FAIL EAP 10-5 HYD SYS 1 OVHT EAP 10-8 HYD SYS 1-2 FAIL EAP 10-3 HYD SYS 2 FAIL EAP 10-6 HYD SYS 2 OVHT EAP 10-8 IC 1 OVERHEAT EAP 2-9

C A U T I O N

IC 1 WOW INOP Crew Awareness


REVISION 9 EAP 0-5

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IC 2 OVERHEAT EAP 2-9 IC 2 WOW INOP Crew Awareness

IC BUS FAIL EAP 2-8 ICE DET1 FAIL EAP 11-5 ICE DET2 FAIL EAP 11-5 ICE DETECTORS FAIL EAP 11-5 IRS 1 ALN FAULT EAP 2-9 IRS 1 FAIL EAP 2-10 IRS 1 OVERHEAT EAP 2-11 IRS 2 ALN FAULT EAP 2-9 IRS 2 FAIL EAP 2-10 IRS 2 OVERHEAT EAP 2-11 LATERAL MODE OFF EAP 2-7 LG AIR/GND FAIL EAP 12-8 NLG UP/DOOR OPN EAP 12-9 NO ICE-A/ICE ON EAP 11-6 PACK 1 OVHT EAP 1-9 PACK 1 OVLD EAP 1-10 PACK 1 VLV FAIL EAP 1-11 PACK 2 OVHT EAP 1-9 PACK 2 OVLD EAP 1-10 PACK 2 VLV FAIL EAP 1-11 PAX OXY LO PRESS EAP 13-3 PITOT 1 INOP EAP 11-6 PITOT 2 INOP EAP 11-6 PITOT 3 INOP EAP 11-6 PRESN AUTO FAIL EAP 1-12 PTRIM BKP SW FAIL EAP 8-8 PTRIM CPT SW FAIL EAP 8-8 PTRIM F/O SW FAIL EAP 8-8 RAM AIR VLV FAIL EAP 1-13 RUD HDOV PROTFAIL EAP 8-8 RUDDER OVERBOOST EAP 8-9 RUDDER SYS 1 INOP EAP 8-10 RUDDER SYS 1-2 INOP EAP 8-10 RUDDER SYS 2 INOP EAP 8-10 RUD STOP DISAGREE EAP 8-8 SHED BUS 1 OFF Crew Awareness

SHED BUS 2 OFF Crew Awareness

SPBK LVR DISAGREE EAP 8-11 SPC FAIL Crew Awareness

SPOILER FAIL EAP 8-7 SPS ADVANCED EAP 14-5 STAB A/ICE FAIL EAP 11-8 STEER INOP EAP 12-9

C A U T I O N

STICK PUSHER FAIL EAP 14-7


EAP 0-6 REVISION 9

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TAT 1 HEAT INOP EAP 11-7 TAT 2 HEAT INOP EAP 11-7 TERR INOP EAP 14-6 VERTICAL MODE OFF EAP 2-7 W/S 1 HEAT FAIL EAP 11-7 W/S 2 HEAT FAIL EAP 11-7 WG A/ICE FAIL EAP 11-8 WINDSHEAR INOP EAP 14-8 WING FUEL IMBALANCE EAP 9-15

C A U T I O N

YAW DAMPER FAIL EAP 2-12


REVISION 10 EAP 0-7

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AIII NOT AVAIL Crew Awareness

APU FUEL SOV CLSD Crew Awareness

BLD 1 VLV CLSD EAP 1-14 BLD 2 VLV CLSD EAP 1-14 CHECK A1E PERF Crew Awareness

CHECK A1P PERF Crew Awareness

CMC FAIL Crew Awareness

CONFIG MISMATCH Crew Awareness

CROSS BLD OPEN Crew Awareness

DATALINK FAIL Crew Awareness

DAU1 B FAIL EAP 2-4 DAU 1 REVERSION Crew Awareness

DAU2 B FAIL EAP 2-4 DAU 2 REVERSION Crew Awareness

DU 1 FAN FAIL Crew Awareness

DU 1 OVHT Crew Awareness









E1 FUEL IMP BYP EAP 6-12 E1 FUELSOV CLSD Crew Awareness

E1 HYD PUMP FAIL EAP 10-8 E1 HYDSOV CLSD Crew Awareness

E1 IDL STP FAIL EAP 6-13 E1 OIL IMP BYP Crew Awareness

E1 SHORT DISP Crew Awareness

E1-2 HYD PUMP FAIL EAP 10-3 E2 FUEL IMP BYP EAP 6-12 E2 FUELSOV CLSD Crew Awareness

E2 HYD PUMP FAIL EAP 10-8 E2 HYDSOV CLSD Crew Awareness

E2 IDL STP FAIL EAP 6-13 E2 OIL IMP BYP Crew Awareness

E2 SHORT DISP Crew Awareness

ENG A/ICEOVERPRES Crew Awareness

A D V I S O R Y

FDAU FAIL Crew Awareness


EAP 0-8 REVISION 10

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FLAP LOW SPEED EAP 8-11 FUEL XFEED OPEN Crew Awareness

GEN1 BRG FAIL Crew Awareness




HI ALT LDG-T/O Crew Awareness

HYD PUMP SELEC OF Crew Awareness HYD1 LO QTY EAP 10-9 HYD2 LO QTY EAP 10-9 IC1 CONFIG FAIL Crew Awareness IC 1 FAN FAIL Crew Awareness IC2 CONFIG FAIL Crew Awareness IC 2 FAN FAIL Crew Awareness ICE CONDITION Crew Awareness SPS/ICE SPEEDS Crew Awareness IRS 1 ALN EAP 2-12 IRS 1 ATT MODE EAP 2-13 IRS 1 EXC MOTION Crew Awareness

IRS 1 NO MAG HDG Crew Awareness

IRS 1 NO PPOS Crew Awareness

IRS 1 ON BATT EAP 2-14 IRS 2 ALN EAP 2-12 IRS 2 ATT MODE EAP 2-13 IRS 2 EXC MOTION Crew Awareness

IRS 2 NO MAG HDG Crew Awareness

IRS 2 NO PPOS Crew Awareness

IRS 2 ON BATT EAP 2-14 PACK 1 VLV CLSD EAP 1-14 PACK 2 VLV CLSD EAP 1-14 RAAS INHIBITED Crew Awareness

RAAS NOT AVAIL Crew Awareness

RAD ALT 1 FAIL EAP 2-14 RAD ALT 2 FAIL EAP 2-14 RAD ALT FAIL EAP 2-14 SATCOM FAIL Crew Awareness

A D V I S O R Y

VHF 3 FAIL Crew Awareness

EMERGENCY/ABNORMAL PROCEDURES Air Conditioning, Pneumatics & Pressurization

ORIGINAL EAP 1-1

TABLE OF CONTENTS

ANNUNCIATED PROCEDURES

BLEED APU LEAK...............................................EAP 1-3

BLEED ENGINE LEAK.........................................EAP 1-4

BLEED OVERTEMPERATURE............................EAP 1-5

APU BLEED VALVE FAILURE............................EAP 1-5

BLEED LOW TEMPERATURE ............................EAP 1-6

BLEED VALVE FAILURE.....................................EAP 1-7

CABIN DEPRESSURIZATION .............................EAP 1-12

CROSSBLEED FAILURE.....................................EAP 1-8

HIGH STAGE VALVE FAILURE ..........................EAP 1-8

PACK OVERHEAT ...............................................EAP 1-9

PACK OVERLOAD...............................................EAP 1-10

PACK VALVE FAILURE.......................................EAP 1-11

PRESSURIZATION AUTOMATIC SYSTEM FAILURE / CABIN DEPRESSURIZATION......EAP 1-12

RAM AIR VALVE FAILURE .................................EAP 1-13

BLEED VALVE CLOSED .....................................EAP 1-14

PACK VALVE CLOSED .......................................EAP 1-14

NON ANNUNCIATED PROCEDURES

AIR CONDITIONING SMOKE. .................. refer to S-4

EMERGENCY DESCENT.......................... refer to NAP-6

RAPID CABIN DEPRESSURIZATION ...... refer to NAP-14

LOSS OF PRESSURIZATION INDICATION.......................................... refer to NAP-31

SINGLE ENGINE BLEED OPERATION IN ICING CONDITIONS .. refer to NAP-41


EAP 1-2 ORIGINAL


BLD APU LEAK .................................................EAP 1-3

BLD 1 (2) LEAK .................................................EAP 1-4

BLD 1 (2) OVTEMP............................................EAP 1-5 APU BLD VLV FAIL ...........................................EAP 1-5

BLD 1 (2) LOW TEMP........................................EAP 1-6

BLD 1 (2) VLV FAIL ...........................................EAP 1-7

CROSS BLD FAIL..............................................EAP 1-8

HS VLV 1 (2) FAIL..............................................EAP 1-8

PACK 1 (2) OVHT ..............................................EAP 1-9

PACK 1 (2) OVLD ..............................................EAP 1-10

PACK 1 (2) VLV FAIL ........................................EAP 1-11

PRESN AUTO FAIL ...........................................EAP 1-12

RAM AIR VLV FAIL............................................EAP 1-13

BLD 1 (2) VLV CLSD .........................................EAP 1-14

PACK 1 (2) VLV CLSD.......................................EAP 1-14


ORIGINAL EAP 1-3

BLEED APU LEAK

EICAS Warning: BLD APU LEAK

APU Bleed......................................... PUSH OUT Bleed 1 and 2 .................................... AS REQUIRED

...................................................... WAIT 3 MINUTES

No

Yes

APU.................................................... SHUTDOWN

No

Yes

BLEED ENGINE LEAK Procedure (EAP 1-4).................... ACCOMPLISH

Start the procedure considering BLD 1 LEAK.

MESSAGE PERSISTS?

END

END

MESSAGE STILL PERSISTS?


EAP 1-4 ORIGINAL

BLEED ENGINE LEAK

EICAS Warning: BLD 1 (2) LEAK Light: Red LEAK inscription in affected push

button.

Consider diversion. XBleed ............................................... CLOSED Affected Bleed .................................. PUSH OUT APU Bleed......................................... PUSH OUT Altitude.............................................. MAX 25’000 FT,

MIN MEA Icing Conditions ............................... EXIT/AVOID

...................................................... WAIT 3 MINUTES No

Yes

BLD 1 (2) VLV FAIL

BLD 1 (2) VLV CLSD

Opposite Bleed................................. PUSH OUT Associated Bleed ............................. PUSH IN

...................................................... WAIT 3 MINUTES

No

Yes

Associated Bleed ............................. PUSH OUT Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR


Associated Thrust Lever ................. IDLE

...................................................... WAIT 3 MINUTES


BLD 1 (2 OR APU) LEAK MESSAGE EXTINGUISHES?

END

END

ASSOCIATED MESSAGE?

BLD 1 (2 OR APU) LEAK MESSAGE PERSISTS?


ORIGINAL EAP 1-5

CONTINUED FROM PREVIOUS PAGE No Yes

Associated ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)..................... ACCOMPLISH

BLEED OVERTEMPERATURE EICAS Warning: BLD 1 (2) OVTEMP MFD Indication: Bleed Temp pointer may be in red

range or out of view. XBleed ............................................... OPEN

Associated Bleed ............................. PUSH OUT Altitude.............................................. MAX 25’000 FT,

MIN MEA

...................................................... WAIT 3 MINUTES No

Associated Bleed ............................. PUSH IN Opposite Bleed................................. PUSH OUT

SINGLE ENGINE BLEED OPERATION IN ICING CONDITIONS Procedure (NAP-41)..................... AS REQUIRED

APU BLEED VALVE FAILURE EICAS Caution: APU BLD VLV FAIL

No

Yes

No

Yes

APU.................................................... SHUTDOWN

Bleeds 1 and 2 .................................. AS REQUIRED

FAILED IN THE OPEN POSITION?

ANY BLEED LEAK EXISTS?

END

END

BLD 1 (2 or APU) LEAK MESSAGE PERSISTS?

END

BLD 1 (2) OVTEMP MESSAGE PERSISTS?

Yes


EAP 1-6 REVISION 9

BLEED LOW TEMPERATURE EICAS Caution: BLD 1 (2) LOW TEMP

MFD Indication: Bleed Temp pointer may be amber or may be out of view.

No

Yes

Message ............................................ DISREGARD

Ice Detection Override Knob........... ALL Associated Thrust Lever ................. ADVANCE

Adjust affected Thrust Lever until message disappears or pointer of the affected side reaches green range or opposite pointer.

...................................................... WAIT 1 MINUTE No

Yes

Affected Bleed .................................. PUSH OUT Altitude.............................................. MAX 25’000 FT,

MIN MEA

No

Yes

XBleed ............................................... OPEN Altitude.............................................. MAX 15’000 FT,

MIN MEA If it is not possible to descend below 15’000 ft:

Ice Conditions.............................. EXIT

...................................................... WAIT 2 MINUTES Ice Detection Override Knob........... AUTO

Ice Detection Override Knob........... AUTO

END

END

BLEED TEMP IN GREEN RANGE OR POINTER OUT OF VIEW?

MESSAGE PERSISTS?

END

ICING CONDITIONS?


ORIGINAL EAP 1-7

BLEED VALVE FAILURE EICAS Caution: BLD 1 (2) VLV FAIL

No

Yes

Bleed 2

Bleed 1

No

Yes

XBleed ............................................... CLOSED APU.................................................... START Altitude.............................................. MAX 37’000 FT,

MIN MEA APU Bleed......................................... PUSH IN SINGLE ENGINE BLEED OPERATION

IN ICING CONDITIONS Procedure (NAP-41)..................... AS REQUIRED

XBleed ............................................... OPEN Altitude.............................................. MAX 25’000 FT,

MIN MEA SINGLE ENGINE BLEED OPERATION

IN ICING CONDITIONS Procedure (NAP-41)..................... AS REQUIRED

END

APU SERVICEABLE?

BLD 1 (2) VLV CLSD MESSAGE PRESENTED?

END

AFFECTED BLEED VALVE?


EAP 1-8 ORIGINAL

CROSSBLEED FAILURE EICAS Caution: CROSS BLD FAIL

No

Yes

No

Yes

Consider diversion. Bleeds 1 and 2 .................................. PUSH OUT APU Bleed......................................... PUSH OUT Icing Conditions ............................... EXIT/AVOID Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR 10’000 FT,

WHICHEVER IS HIGHER

HIGH STAGE VALVE FAILURE EICAS Caution: HS VLV 1 (2) FAIL

Yes

Associated BLEED OVERTEMPERATURE Procedure (EAP 1-5).................... ACCOMPLISH

Yes

Associated BLEED LOW TEMPERATURE Procedure (EAP 1-6).................... ACCOMPLISH

CROSS BLD OPEN MESSAGE PRESENTED?

END

ASSOCIATED MFD BLEED POINTER INDICATES RED RANGE?

END

ASSOCIATED TO BLEED LEAK OR ENGINE OVERTEMPERATURE?

END

ASSOCIATED MFD BLEED POINTER INDICATES WHITE RANGE?

END

No

No


REVISION 10 EAP 1-9

PACK OVERHEAT EICAS Caution: PACK 1 (2) OVHT

Associated Temperature & Mode Selector .............................. AUTO/FULL COLD

Cabin Temperature .......................... MONITOR Affected Pack ................................... PUSH OUT

...................................................... WAIT 3 MINUTES Affected Pack ................................... PUSH IN

No

Yes

Associated Temperature & Mode Selector .............................. MANUAL/FULL

COLD Cabin Temperature .......................... MONITOR Affected Pack ................................... PUSH OUT

...................................................... WAIT 3 MINUTES Affected Pack ................................... PUSH IN

No

Yes

Affected Pack ..................................PUSH OUT No

Yes

Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR 10’000 FT,

WHICHEVER IS HIGHER

At least one bleed source must be kept open. When reaching 10’000 ft:

Cabin............................................. DEPRESSURIZE

Altitude.............................................. MAX 25’000 FT, MIN MEA

MESSAGE PERSISTS?

MESSAGE PERSISTS?

END

END

END

BOTH PACKS AFFECTED?


EAP 1-10 REVISION 10

PACK OVERLOAD EICAS Caution: PACK 1 (2) OVLD

Recirculation Fan .......................... PUSH IN Associated Temperature &

Mode Selector ........................... AUTO/ 12 O’CLOCK POSITION

Affected Pack ................................ PUSH OUT

................................................... WAIT 3 MINUTES Affected Pack ................................ PUSH IN

No

Yes

Associated Temperature & Mode Selector ........................... MANUAL/

12 O’CLOCK POSITION

Affected Pack ................................ PUSH OUT

................................................... WAIT 3 MINUTES Affected Pack ................................ PUSH IN No Yes

Affected Pack ................................ PUSH OUT Associated Engine Bleed ............. CHECK PUSHED IN

No

Yes

Oxygen Masks ............................... AS REQUIRED Altitude........................................... MEA OR 10’000 FT,

WHICHEVER IS HIGHER


Cabin.......................................... DEPRESSURIZE

Altitude........................................... MAX 25’000 FT,

MIN MEA


END

MESSAGE PERSISTS?

END



REVISION 5 EAP 1-11

PACK VALVE FAILURE EICAS Caution: PACK 1 (2) VLV FAIL

No

Yes

Altitude........................................... MAX 25’000 FT, MIN MEA

No

Yes


WHICHEVER IS HIGHER

When reaching 10’000 ft: Cabin.......................................... DEPRESSURIZE

Yes

Altitude........................................... MAX 25’000 FT, MIN MEA

Pack 2

Pack 1 or Both Packs

APU Bleed...................................... PUSH OUT

XBleed ............................................ CLOSED Associated Bleed(s)...................... PUSH OUT Icing Conditions ............................ EXIT/AVOID

No

Yes


WHICHEVER IS HIGHER


Cabin.......................................... DEPRESSURIZE

PACK 1 (2) VLV CLSD MESSAGE PRESENTED?

END


END

AFFECTED PACK(S)?

NEED TO CLOSE THE AFFECTED PACK?


No


EAP 1-12 REVISION 5

PRESSURIZATION AUTOMATIC SYSTEM FAILURE/CABIN DEPRESSURIZATION

EICAS Caution: PRESN AUTO FAIL may be presented.

EICAS Indication: Abnormal cabin altitude (amber or red) may be presented.

Pressurization Manual Controller ........11 O'CLOCK

POSITION At least one bleed source must be kept open. Pressurization Mode Selector ..............PUSH IN (MAN) Pressurization Manual Controller ........AS REQUIRED

Wait for system response and stabilization.

No

Yes

Cabin Altitude........................................CONTROL Set and control cabin altitude according to the AIRPLANE/CABIN ALTITUDE conversion table on NAP-31.

No

Yes

RAPID CABIN DEPRESSURIZATION Procedure (NAP-14)..........................ACCOMPLISH

Oxygen Masks .......................................AS REQUIRED Altitude...................................................MEA OR


When reaching 10’000 ft: Pressurization Manual Controller ...FULL DOWN Pressurization Mode Selector .........PUSH OUT Pressurization Dump Button ...........PUSH IN (ON)

MANUAL CONTROL POSSIBLE?

END

CABIN AURAL WARNING VOICE MESSAGE SOUNDS?

END

END


REVISION 5 EAP 1-13

RAM AIR VALVE FAILURE EICAS Caution: RAM AIR VLV FAIL

Air Conditioning System ................. MONITOR

No

Yes

Associated Pack............................... PUSH OUT Altitude.............................................. MAX 25’000 FT,

MIN MEA No

Yes

Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR 10’000 FT,

WHICHEVER IS HIGHER


Cabin............................................. DEPRESSURIZE

ANY PACK 1 (2) OVLD OR PACK 1 (2) OVHTMESSAGE PRESENTED?


END


EAP 1-14 REVISION 4

BLEED VALVE CLOSED EICAS Advisory: BLD 1 (2) VLV CLSD

Associated Pack............................... PUSH OUT, THEN PUSH IN

Associated Bleed ............................. PUSH IN

No

Yes

Affected BLEED VALVE FAILURE Procedure (EAP 1-7).................... ACCOMPLISH

PACK VALVE CLOSED EICAS Advisory: PACK 1 (2) VLV CLSD

Associated Pack............................... PUSH OUT, THEN PUSH IN

No

Yes

No

Yes

Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR


When reaching 10’000 ft, if at least one bleed source is available:

Pressurization Mode Selector.................................... PUSH IN

Pressurization Manual Controller................................. AS REQUIRED

If required: Pressurization Manual

Controller ............................ FULL UP

Altitude...................................................MAX 25’000 FT,

MIN MEA

END

MESSAGE PERSISTS?

MESSAGE PERSISTS?

END


END

EMERGENCY/ABNORMAL PROCEDURES Autopilot, Flight Instruments & Navigation

ORIGINAL EAP 2-1

TABLE OF CONTENTS


AUTOPILOT FAILURE........................................EAP 2-3

AUTOPILOT AILERON MISTRIM .......................EAP 2-3

AUTOPILOT ELEVATOR MISTRIM....................EAP 2-3

AUTOPILOT TRIM FAILED.................................EAP 2-3

DAU FAILURE.....................................................EAP 2-4

DAU MISCOMPARE............................................EAP 2-5

DISPLAY FAILURE .............................................EAP 2-6

ELECTRONIC BAY OVERTEMPERATURE.......EAP 2-7

FD LATERAL MODE OFF...................................EAP 2-7

FD VERTICAL MODE OFF..................................EAP 2-7

IC BUS FAILURE ................................................EAP 2-8

IC FAILURE .........................................................EAP 2-8

IC OVERHEAT.....................................................EAP 2-9

IRS ALIGNMENT FAULT ....................................EAP 2-9

IRS FAIL ..............................................................EAP 2-10

IRS OVERHEAT ..................................................EAP 2-11

YAW DAMPER FAILURE....................................EAP 2-12

IRS ALIGNMENT.................................................EAP 2-12

IRS ATTITUDE MODE.........................................EAP 2-13

IRS ON BATTERY...............................................EAP 2-14

RADIO ALTIMETER FAIL ...................................EAP 2-14


CAS MESSAGE MISCOMPARISON......refer to NAP-17

IRS/MSU FAILURE ANNUNCIATION ....refer to NAP-29

NAV/FLIGHT INSTRUMENTS FAILURE ..............................................refer to NAP-33


EAP 2-2 ORIGINAL


AUTOPILOT FAIL................................................EAP 2-3

AP AIL MISTRIM .................................................EAP 2-3

AP ELEV MISTRIM..............................................EAP 2-3

AUTO TRIM FAIL ................................................EAP 2-3

CHECK PFD 1 (2) ................................................EAP 2-6

DAU1 (2) A FAIL..................................................EAP 2-4

DAU1 (2) ENG MISCOMP ...................................EAP 2-5

DAU1 (2) SYS MISCOMP....................................EAP 2-5

DAU1 (2) WRN MISCOMP ..................................EAP 2-5

ELEKBAY OVTEMP............................................EAP 2-7

IC BUS FAIL ........................................................EAP 2-8

IC 1 (2) OVERHEAT ............................................EAP 2-9

IRS 1 (2) ALN FAULT..........................................EAP 2-9

IRS 1 (2) FAIL......................................................EAP 2-10

IRS 1 (2) OVERHEAT..........................................EAP 2-11

LATERAL MODE OFF.........................................EAP 2-7

VERTICAL MODE OFF .......................................EAP 2-7

YAW DAMPER FAIL ...........................................EAP 2-12

IRS 1 (2) ALN ......................................................EAP 2-12

IRS 1 (2) ATT MODE ...........................................EAP 2-13

IRS 1 (2) ON BATT..............................................EAP 2-14

RAD ALT 1 (2) FAIL ............................................EAP 2-14

RAD ALT FAIL.....................................................EAP 2-14


REVISION 8 EAP 2-3

AUTOPILOT FAILURE

EICAS Warning: AUTOPILOT FAIL Aural Warning: AUTOPILOT Voice message (only

below 2500 ft Radio Altitude, when autopilot is disconnected).

No

Yes

Autopilot ................................................DISENGAGE Autopilot Disengagement.....................CHECK Trim ........................................................AS REQUIRED

AUTOPILOT AILERON MISTRIM

EICAS Caution: AP AIL MISTRIM for more than 10 s. Condition: Autopilot is engaged with aileron out

of trim.

Control Wheel........................................HOLD FIRMLY Quick Disconnect Button .....................PRESS Roll Trim.................................................AS REQUIRED Yaw Trim ................................................AS REQUIRED Autopilot ................................................AS REQUIRED

AUTOPILOT ELEVATOR MISTRIM

EICAS Caution: AP ELEV MISTRIM Condition: Autopilot is engaged with pitch out of

trim.

Control Column .....................................HOLD FIRMLY Quick Disconnect Button .....................PRESS Pitch Trim...............................................AS REQUIRED Autopilot ................................................AS REQUIRED

AUTOPILOT TRIM FAILED

EICAS Caution: AUTO TRIM FAIL

Control Column .....................................HOLD FIRMLY Quick Disconnect Button .....................PRESS Pitch Trim...............................................AS REQUIRED Autopilot ................................................AS REQUIRED

END

END

END

END

MESSAGE PRESENTED ON MFD?


EAP 2-4 ORIGINAL

DAU FAILURE

EICAS Caution: DAU1 (2) A FAIL

The following message may be displayed: EICAS Advisory: DAU1 (2) B FAIL

No

Yes

No

Yes

Associated DAU on EICAS Rev (Pedestal Panel) ............PUSH IN

DAU 2

DAU 1

- Lost Indications: engine 1 oil (temperature, pressure and level), battery 1 and 2 temperature, fuel tank temperature, roll trim position, cockpit temperature, bleed 1 temperature and landing gear position (including RMU indication).

- Lost Messages: FUEL TANK LO TEMP, E1 FUEL LO TEMP, BLEED 1 OVTEMP.

- BLD 1 LOW TEMP message will appear.

- Lost Indications: engine 2 oil (temperature, pressure and level), engine 2 fuel temperature, hydraulic quantity 1 and 2, yaw trim position, cabin temperature, bleed 2 temperature and flaps indication (including RMU indication).

- Lost Messages: BLEED 2 OVTEMP, E2 FUEL LO TEMP, HYD 1 LO QTY, HYD 2 LO QTY.

- BLD 2 LOW TEMP and APU OIL HI TEMP messages will appear.


END

ONLY CHANNEL B AFFECTED?

ONLY CHANNEL A AFFECTED?

END

WHICH DAU IS AFFECTED?

END


ORIGINAL EAP 2-5


LAND AT THE NEAREST SUITABLE AIRPORT. DAU 2

DAU 1

- All messages and indications of the following systems are lost: Oxygen, Steering, Landing Gear, Roll Trim, and the message EMERG LIGHT NOT ARMED.

- Some messages and indications of the following system are lost: Doors, Stall Protection, Electrical, Fire Protection, Fuel, APU, Power Plant, Thrust Reverser, Spoiler, Brakes, Air Conditioning, Ice and Rain Protection.

- All messages and indications of the following systems are lost: Smoke, Hydraulic, Rudder and Yaw Trim.

- Some messages and indications of the following systems are lost: Doors, Stall Protection, Electrical, Fire Protection, Fuel, APU, Power Plant, Thrust Reverser, Flap, Brakes, Air Conditioning, Ice and Rain Protection.

DAU MISCOMPARE

EICAS Caution: DAU1 (2) ENG MISCOMP or DAU1 (2) SYS MISCOMP or DAU1 (2) WRN MISCOMP

Associated DAU on EICAS Rev (Pedestal Panel) ............PUSH IN

NOTE: For each miscompare message and each side, check the following parameters before and after the reversion:

- Engine: N1, N2, ITT. - System: Battery voltage and temperature, Takeoff

temperature, Hydraulic pressure, Oxygen pressure. - Warning: all warning messages, if any.

END

END

WHICH DAU IS AFFECTED?

END


EAP 2-6 ORIGINAL

DISPLAY FAILURE

EICAS Caution: CHECK PFD 1 (2) message is presented if PFD is the failed display.

No

Yes

IC FAILURE/IC BUS FAILURE Procedure (EAP 2-8).........................ACCOMPLISH

No

Yes

LAND AT THE NEAREST SUITABLE AIRPORT. Icing Conditions ....................................AVOID/EXIT RMU ........................................................AS REQUIRED

Use RMU to access Engine and Navigation back up pages.

Affected MFD Selector Knob................PFD

Any MFD Selector Knob .......................EICAS

FAILED DISPLAYS PRESENT A RED X?

END

ALL 5 DISPLAYS FAILED?

END

END

WHICH DISPLAY FAILED?

END

END

MFDPFD

EICAS


REVISION 4 EAP 2-7

ELECTRONIC BAY OVERTEMPERATURE

EICAS Caution: ELEKBAY OVTEMP

Turn off non-essential equipment.

The following equipment is installed in the forward electronic compartment:

ADC;

Transponder Mode S;

Integrated Communication Unit;

Aural Warning Computer;

FMS;

IRS;

Passenger Address;

Integrated Navigation Unit;

Inverter;

Dimmers;

Backup Battery.

No

Yes

LAND AT THE NEAREST SUITABLE AIRPORT. Maintain a cross-check between main and standby instruments. In case of disagreement, follow the standby instruments indication.

FD LATERAL MODE OFF/ FD VERTICAL MODE OFF

EICAS Caution: LATERAL MODE OFF or VERTICAL MODE OFF

At crew discretion, re-select the affected Flight Director or select the other.

MESSAGE PERSISTS?

END

END


EAP 2-8 REVISION 10

IC FAILURE/IC BUS FAILURE

EICAS Caution: IC BUS FAIL may be presented. Condition: Associated Display Units present a

red X.

The following features will be inoperative: - EICAS messages miscompare monitoring. - Takeoff speeds synchronization. - Check List Display synchronization. - Flight Director mode synchronization.

PFD 2 and MFD 2 (IC 2 Failed)

PFD 1, MFD 1 and EICAS (IC 1 Failed)

SG on Reversionary Panel 1 ................PUSH IN

NOTE: - The PIT TRIM 1 (2) INOP or PTRIM MAIN INOP and PTRIM BACKUP INOP messages may not be available.

- Do not press the SG button again within a 3-second interval. In some cases, this action may cause loss of PFD indication. The display indication can be recovered by reverting the MFD to PFD and returning to the normal configuration.

SG on Reversionary Panel 2 ................PUSH IN

NOTE: Do not press the SG button again within a 3-second interval. In some cases, this action may cause loss of PFD indication. The display indication can be recovered by reverting the MFD to PFD and returning to the normal configuration.

FAILED DISPLAYS?

END

END


REVISION 10 EAP 2-9

IC OVERHEAT

EICAS Caution: IC 1 (2) OVERHEAT Associated CB (C3 or D32)...................PULL

No

Yes IC 2

IC 1

Backup Battery......................................PUSH OUT SG on Associated

Reversionary Panel ..........................PUSH IN

NOTE: Do not press the SG button again within a 3-second interval. In some cases, this action may cause loss of PFD indication. The display indication can be recovered by reverting the MFD to PFD and returning to the normal configuration.

No

Yes

ELECTRICAL SYSTEM FIRE OR SMOKE Procedure (S-6)...................ACCOMPLISH

IRS ALIGNMENT FAULT

EICAS Caution: IRS 1 (2) ALN FAULT

Check and reenter present position. If necessary, reenter present position once again.

END

WHICH IC IS AFFECTED?

SMOKE PERSISTS?

END

ASSOCIATED WITH SMOKE?


EAP 2-10 ORIGINAL

IRS FAIL

EICAS Caution: IRS 1 (2) FAIL

In Flight

Power On or Alignment

Affected IRU...........................................OFF Wait MSU lights extinguish. Affected IRU...........................................NAV

IRS on Associated Reversionary Panel ..........................PUSH IN

No

Yes

Affected IRU...........................................ATT

Maintain wings level and constant airspeed for approximately 20 seconds until IRS 1 (2) ALN message is no longer displayed and attitude is recovered.

Magnetic Heading .................................ENTER

CAUTION: FOR IRS IN ATTITUDE MODE, NAVIGATION AND ATTITUDE OUTPUTS ARE NOT AS ACCURATE AS IN THE NAV MODE. MAGNETIC HEADING MUST BE ENTERED AND UPDATED PERIODICALLY FROM THE BEST AVAILABLE ALTERNATIVE SOURCE, THROUGH THE FMS CDU.

Relevant Inoperative Item: Autopilot

OPERATION PHASE?

END

REMAINING IRU DATA NORMAL?

END

END


ORIGINAL EAP 2-11

IRS OVERHEAT

EICAS Caution: IRS 1 (2) OVERHEAT

No

Yes

Associated Circuit Breaker ..................PULL Backup Battery......................................PUSH OUT IRS FAIL Procedure (EAP 2-10)............ACCOMPLISH

Yes

Presented

Not presented

Not illuminated

IRS on Associated Reversionary Panel ..........................PUSH IN

Affected IRU...........................................OFF Autopilot ................................................DISENGAGE

During final approach, if additional attitude reference is necessary:

Affected IRU......................................ATT

CAUTION: FOR IRS IN ATT MODE, NAVIGATION AND ATTITUDE OUTPUTS ARE NOT AS ACCURATE AS IN THE NAV MODE. MAGNETIC HEADING MUST BE ENTERED AND UPDATED PERIODICALLY FROM THE BEST AVAILABLE ALTERNATIVE SOURCE, THROUGH THE FMS CDU.

Relevant Inoperative Item: Autopilot

END

IRS DATA NORMAL?

MSU FAULT LIGHT?

END

IRS 1 (2) FAIL MESSAGE?

ASSOCIATED TO SMOKE OR FIRE?

No

Illuminated


EAP 2-12 ORIGINAL

YAW DAMPER FAILURE

EICAS Caution: YAW DAMPER FAIL

Yaw Damper...........................................DISENGAGE Autopilot ................................................AS REQUIRED

No

Yes

Autopilot ................................................DISENGAGE

Altitude...................................................MAX 35000 ft MINIMUM MEA

IRS ALIGNMENT

EICAS Advisory: IRS 1 (2) ALN

IRU mode select switch ........................CHECK NAV This message is only presented during alignment phase or

while the IRU mode select switch is set at ALIGN position.

FAILURE PERSISTS?

END

END

FLIGHT ABOVE MACH 0.7?No

Yes


REVISION 2 EAP 2-13

IRS ATTITUDE MODE

EICAS Advisory: IRS 1 (2) ATT MODE

No

Yes

Affected IRU...........................................OFF

Wait MSU lights extinguish. Affected IRU...........................................NAV

END

ON GROUND?

END


EAP 2-14 ORIGINAL

IRS ON BATTERY

EICAS Advisory: IRS 1 (2) ON BATT

Associated IRU will operate for 40 minutes.

RADIO ALTIMETER FAIL

EICAS Advisory: RAD ALT 1 (2) FAIL or RAD ALT FAIL may be presented.

No

Yes

Consider pulling respective radio altimeter circuit breaker (D14 or D21) to inhibit undesired nuisance warnings.

No

Yes

Do not perform CAT II or CAT III approaches.

No

Yes

Do not perform CAT II or CAT III approaches.

ASSOCIATED WITH ERRONEOUS EGPWS ACTIVATION?

END

ALL RADIO ALTIMETERS AFFECTED (RAD ALT FAIL MESSAGE PRESENTED)?

END

RA1 (2) AMBER ANNUNCIATOR PRESENTED IN BOTH PFDs?

END

END

EMERGENCY/ABNORMAL PROCEDURES Auxiliary Power Unit

ORIGINAL EAP 3-1

TABLE OF CONTENTS


APU FIRE ............................................................EAP 3-3

BLEED APU LEAK................................ refer to EAP 1-3

APU BLEED VALVE FAILURE............. refer to EAP 1-5

APU CONTACTOR CLOSED..............................EAP 3-4

APU FAIL.............................................................EAP 3-4

APU FUEL LOW PRESSURE .............................EAP 3-5

APU FUEL SHUTOFF VALVE INOPERATIVE .................................. refer to EAP 9-5

APU OIL HIGH TEMPERATURE ........................EAP 3-6

APU OIL LOW PRESSURE.................................EAP 3-6


APU OVERTEMPERATURE ..................refer to NAP-4


EAP 3-2 ORIGINAL


APU FIRE .............................................................EAP 3-3

BLD APU LEAK...................................... refer to EAP 1-3

APU BLD VLV FAIL ............................... refer to EAP 1-5

APU CNTOR CLSD ..............................................EAP 3-4

APU FAIL..............................................................EAP 3-4

APU FUEL LO PRESS .........................................EAP 3-5

APU FUEL SOV INOP............................ refer to EAP 9-5

APU OIL HI TEMP ................................................EAP 3-6

APU OIL LO PRESS.............................................EAP 3-6


ORIGINAL EAP 3-3

APU FIRE

EICAS Warning: APU FIRE Aural Warning: BELL

APU Fuel Shutoff Valve ................... PUSH IN

APU Master Knob............................. OFF


Fuel Pump Pwr 2 .............................. OFF XFeed ................................................ OFF Initiate the descent to MEA or 25’000 ft, whichever is higher.

...................................................... WAIT 30 SECONDS APU Fire Extinguishing Button................................................ PRESS

WARNING: DO NOT ATTEMPT TO RESTART APU.

END

APU FIRE MESSAGE PERSISTS?

APU FUEL SOV CLSD MESSAGE? Displayed

Not Displayed

No

Yes


EAP 3-4 ORIGINAL

APU CONTACTOR CLOSED

EICAS Caution: APU CNTOR CLSD Bus Ties ............................................ OFF Battery 2............................................ OFF

APU FAIL

EICAS Caution: APU FAIL Condition: APU automatically shuts down. Do not try to restart the APU. APU Start .......................................... AS REQUIRED

NOTE: - Up to three APU start attempts may be accomplished, including the first attempt in which the message was displayed.

- The APU Starter Cool-down Limit is 1 MINUTE OFF.

Do not try to restart the APU.

END

END

END

OBVIOUS SAFETY HAZARD?

END

No

No

SHUTDOWN DURING APU START CYCLE?

Yes

Yes


ORIGINAL EAP 3-5

QR

H-1

35

/15

69

END

No

Yes

No

Yes

MESSAGE REMAINS?

MFD UNAVAILABLE OR ALL PUMPS IN ONE TANK ARE INOPERATIVE?

END

APU FUEL LOW PRESSURE

EICAS Caution: APU FUEL LO PRESS Fuel Pump Sel 2 ............................... SELECT ANOTHER Repeat the procedure. Altitude.............................................. MAX 25’000 FT,

MIN MEA

NOTE: If required, Crossfeed may be open above 25’000 ft.


EAP 3-6 ORIGINAL

APU OIL HIGH TEMPERATURE/ APU OIL LOW PRESSURE

EICAS Caution: APU OIL HI TEMP and/or APU OIL LO PRESS

APU OVERTEMPERATURE

Procedure (NAP-4)....................... ACCOMPLISH

APU EGT and RPM........................... MONITOR

APU.................................................... SHUTDOWN

END

END

END

No

No APU RPM OUT OF THE RED RANGE?

APU EGT INTO AMBER OR RED RANGE?

IS APU ESSENTIAL FOR THE FLIGHT? No

Yes

Yes

Yes

EMERGENCY/ABNORMAL PROCEDURES Doors

ORIGINAL EAP 4-1

TABLE OF CONTENTS


MAIN DOOR OPEN ..............................................EAP 4-3

ACCESS DOORS OPEN......................................EAP 4-4

BAGGAGE DOORS OPEN ..................................EAP 4-4

EMERGENCY EXIT OPEN...................................EAP 4-5

INTERNAL BAGGAGE ACCESS DOOR OPEN ...............................................................EAP 4-5


MAIN DOOR BLOCKED........................... refer to NAP-33


EAP 4-2 ORIGINAL


MAIN DOOR OPN.................................................EAP 4-3

ACCESS DOORS OPN ........................................EAP 4-4

BAGG ACCESS OPN……………………………....EAP 4-5

BAGGAGE DOOR OPN .......................................EAP 4-4

EMERG EXIT OPN ...............................................EAP 4-5


REVISION 10 EAP 4-3

MAIN DOOR OPEN

EICAS Warning: MAIN DOOR OPN

MFD Indication: Red DOOR OPEN. FSTN Belts ........................................ ON Door Alignment Red Marks ............. CHECK

No

Yes

No

Yes

Cabin altitude ................................... MONITOR

LAND AT THE NEAREST SUITABLE AIRPORT. Oxygen Masks .................................. AS REQUIRED Altitude.............................................. MEA OR 10’000 FT,

WHICHEVER IS HIGHER

When reaching 10’000 ft: Cabin............................................. DEPRESSURIZE

END

END

DOOR CONFIRMED

CABIN PRESSURIZATION NORMAL?


EAP 4-4 ORIGINAL

ACCESS/BAGGAGE DOORS OPEN

EICAS Caution: ACCESS DOORS OPN or BAGGAGE DOOR OPN

MFD Indication: Red DOOR OPEN. Abrupt Maneuvers............................ AVOID

No

Yes



WHICHEVER IS HIGHER


END

END



ORIGINAL EAP 4-5

EMERGENCY EXIT OPEN

EICAS Caution: EMERG EXIT OPN MFD Indication: Red DOOR OPEN.

FSTN Belts ........................................ ON Affected Exit ..................................... CHECK Remove passenger(s) from exit vicinity.

Emergency exit handle .................... CHECK PUSHED IN

No

Yes

No

Yes



WHICHEVER IS HIGHER


INTERNAL BAGGAGE ACCESS DOOR OPEN

EICAS Caution: BAGG ACCESS OPN MFD Indication: Red DOOR OPEN.

Door Status on MFD......................... CHECK

If message is confirmed or MFD is not available:

Door................................................... CLOSE AND LOCK

END

EMERGENCY EXIT LOCKED?


END

END


EAP 4-6 ORIGINAL

INTENTIONALLY BLANK

EMERGENCY/ABNORMAL PROCEDURES Electrical & Lighting

ORIGINAL EAP 5-1

TABLE OF CONTENTS


BATTERY OVERTEMPERATURE.................... EAP 5-3

ELECTRIC ESSENTIAL TRANSFER FAILURE ................................ EAP 5-3

115 V AC BUS OFF........................................... EAP 5-4

APU CONTACTOR CLOSED.............. refer to EAP 3-4

BACK-UP BATTERY OFF BUS........................ EAP 5-4

BATTERY OFF BUS.......................................... EAP 5-4

DC BUS 1 OFF .................................................. EAP 5-5

DC BUS 2 OFF .................................................. EAP 5-6

ELECTRICAL EMERGENCY ABNORMAL TRANSFER................................................. EAP 5-7

EMERGENCY LIGHTS NOT ARMED ............... EAP 5-7

ESSENTIAL BUS 1 OFF ................................... EAP 5-8

ESSENTIAL BUS 2 OFF ................................... EAP 5-9

ESSENTIAL BUS 1-2 OFF ................................ EAP 5-10

GENERATOR OFF BUS.................................... EAP 5-12

GENERATOR OVERLOAD............................... EAP 5-12

LOSS OF ALL GENERATORS ......................... EAP 5-13


ELECTRICAL SYSTEM FIRE OR SMOKE....................................refer to S-6

ANNEX 01 - AFFECTED EQUIPMENT

DC BUS FAILURE ............................................. EAP 5-14 ESS BUS FAILURE ........................................... EAP 5-15


EAP 5-2 ORIGINAL


BATT 1 (2) OVTEMP ......................................... EAP 5-3

ELEC ESS XFR FAIL ........................................ EAP 5-3

115 VAC BUS OFF............................................ EAP 5-4

APU CNTOR CLSD ............................. refer to EAP 3-4

APU GEN OFF BUS .......................................... EAP 5-12

APU GEN OVLD................................................ EAP 5-12

BKUP BATT OFF BUS...................................... EAP 5-4

BATT1 (2) OFF BUS.......................................... EAP 5-4

DC BUS 1 OFF .................................................. EAP 5-5

DC BUS 2 OFF .................................................. EAP 5-6

ELEC EMERG ABNORM .................................. EAP 5-7

EMERG LT NOT ARMD .................................... EAP 5-7

ESS BUS 1 OFF ................................................ EAP 5-8

ESS BUS 2 OFF ................................................ EAP 5-9

ESS BUS 1-2 OFF ............................................. EAP 5-10

GEN 1-2-3-4 OFF BUS ...................................... EAP 5-13

GEN 1 (2, 3, 4) OFF BUS .................................. EAP 5-12

GEN 1 (2, 3, 4) OVLD ........................................ EAP 5-12


REVISION 9 EAP 5-3

BATTERY OVERTEMPERATURE

EICAS Warning: BATT 1 (2) OVTEMP

MFD Indication: Battery temperature in red.

Affected Battery ....................................OFF

No

Yes


ELECTRIC ESSENTIAL TRANSFER FAILURE

EICAS Warning: ELEC ESS XFR FAIL

Essential Power.....................................PUSH IN

No

Yes

Bus Ties .................................................OFF

No

Yes


Shed Buses............................................OFF

Turn off non essential equipment. Begin with DC Buses 1 and 2 (CB Panel rows D, E, F, G and H).

LOSS OF ALL GENERATORS Procedure (EAP 5-13).......................ACCOMPLISH

ASSOCIATED BATT 1 (2) OFF BUS MESSAGE DISPLAYED?

END

END

END

MESSAGE PERSISTS?



EAP 5-4 ORIGINAL

115 V AC BUS OFF

EICAS Caution: 115 VAC BUS OFF

AC PWR..................................................PUSH OUT, THEN PUSH IN

No

Yes

AC PWR..................................................PUSH OUT Relevant Inoperative Items:

TCAS II Windshear Detection EGPWS

BACK-UP BATTERY OFF BUS

EICAS Caution: BKUP BATT OFF BUS

Backup Battery......................................CHECK PUSHED IN

BATTERY OFF BUS

EICAS Caution: BATT1 (2) OFF BUS MFD Indication: Battery may be amber.

Affected Battery.....................................AUTO

MESSAGE PERSISTS?

END

END

END


REVISION 8 EAP 5-5

DC BUS 1 OFF

EICAS Caution: DC BUS 1 OFF MFD Indication: DC BUS may be amber.

Bus Ties .................................................OVRD

No

Yes

Bus Ties .................................................AUTO Icing Conditions ....................................EXIT/AVOID Altitude...................................................25’000 FT OR

MEA, WHICHEVER IS HIGHER

At pilot’s discretion, on Reversionary Panel 1: MFD Knob..........................................PFD

Relevant Inoperative Items: Autopilot W/S 1 Heating and Wiper EGPWS

FMS 1 Transponder 1 RA 1

Speed Brake Main Pitch Trim TCAS 2000

Pack 1 Thrust Reverser 1 DME 1

Automatic Pressurization Control

Do not set Thrust Lever 1 below idle in flight. Anticipate flap actuation. Landing configuration:

Flaps .................................................... 22° VREF ...................................................... VREF 45° + 30 KIAS


Affected Equipment (EAP 5-14) ...........CHECK

MESSAGE PERSISTS?

END


EAP 5-6 ORIGINAL

DC BUS 2 OFF

EICAS Caution: DC BUS 2 OFF MFD Indication: DC BUS may be amber.

Condition: Noise increase due to nose landing gear doors open.

Bus Ties .................................................OVRD

No

Yes

Bus Ties .................................................AUTO Icing Conditions ....................................EXIT/AVOID Airspeed.................................................MAX 250 KIAS Altitude...................................................25’000 FT OR

MEA, WHICHEVER IS HIGHER

The overhead panel lighting is inoperative, therefore, all striped bars will not illuminate. SG ...........................................................PUSH IN At pilot’s discretion, on Reversionary Panel 2:

MFD Knob..........................................PFD MFD Control is possible through MFD 1 Bezel.

Relevant Inoperative Items: VHF2/ADF2/VOR2/ DME2/ILS2/MB2

W/S 2 Heating and Wiper Steering

Thrust Reverser 2 Transponder 2 Pack 2

Stick Pusher Landing lights FMS 2

Do not set Thrust Lever 2 below idle in flight. Anticipate flap actuation. Landing configuration:

Flaps.....................................................22° VREF.......................................................VREF 45° + 15 KIAS


Affected Equipment (EAP 5-14) ...........CHECK

MESSAGE PERSISTS?

END


REVISION 4 EAP 5-7

ELECTRICAL EMERGENCY ABNORMAL TRANSFER

EICAS Caution: ELEC EMERG ABNORM

Essential Power.....................................CHECK PUSHED OUT

No

Yes

LAND AT THE NEAREST SUITABLE AIRPORT. Emerg Lts...............................................OFF

If required, turn ON Emerg Lts just before landing.

Bus Ties .................................................OFF

Batteries 1 and 2 ...................................OFF

No

Yes

Bus Ties .................................................AUTO

Batteries 1 and 2 ...................................AUTO APU (if serviceable) ..............................START APU Generator ......................................CHECK

PUSHED IN

CAUTION: IF APU GENERATOR IS NOT AVAILABLE AND THE MESSAGE REMAINS, BATTERIES DURATION WILL BE 40 MINUTES.

EMERGENCY LIGHTS NOT ARMED

EICAS Caution: EMERG LT NOT ARMD EMERG LT Switch .................................ARM

No

Yes

EMERG LTS on Forward Attendant Control Panel ..................Check NORM

END

MESSAGE PERSISTS?

MESSAGE PERSISTS?

END



EAP 5-8 REVISION 10

ESSENTIAL BUS 1 OFF

EICAS Caution: ESS BUS 1 OFF

On Reversionary panel 1: SG ................................................. PUSH IN

Fuel Pump 1...................................... 1B OR 1C NOTE: Start selecting the Fuel Pump 1B.

Fuel Pump 2...................................... 2A OR 2C Altitude.............................................. MAX 25’000 FT,

MIN MEA XFEED ............................................... OFF

NOTE: Use asymmetric thrust to improve or maintain wing fuel Balance.

No

Yes XBleed ............................................... OPEN Altitude.............................................. MEA OR


If it is not possible to descend below 15’000 ft: Icing Conditions .......................... EXIT

Monitor fuel quantity indication 1 through FMS. Fuselage Fuel Transfer System ...... CHECK

STATUS If fuel transfer is not observed consider a diversion.

Brake effectiveness will be reduced.

COM 2 on Digital Audio Panel 2...... PUSH IN

Relevant Inoperative Items: ENG 1 Fire Detection System CPAM RMU 1

ADF1/VHF1/VOR1/ILS1/MB1 Audio System 1

Landing Gear Control (Down Override)


No

Yes

Affected Equipment (EAP 5-15 and EAP 5-16) .............................. CHECK


ICING CONDITIONS?

END

EICAS ENERGIZED?


REVISION 10 EAP 5-9


DAU 1 on EICAS Rev ....................... PUSH IN At pilots’s discretion, on Reversionary Panel 1:

MFD Knob..................................... EICAS


ESSENTIAL BUS 2 OFF

EICAS Caution: ESS BUS 2 OFF MFD Indication: ESS BUS may be amber.

Fuel Pump 1...................................... 1A OR 1C Fuel Pump 2...................................... 2B OR 2C

NOTE: Start selecting the Fuel Pump 2B.

Icing Conditions ............................... EXIT/AVOID Altitude.............................................. MAX 25’000 FT,

MIN MEA

Monitor fuel quantity indication 2 through FMS. Fuselage Fuel Transfer System ...... CHECK

STATUS If fuel transfer is not observed consider a diversion.

CAUTION: DO NOT USE CROSSFEED.

Brake effectiveness will be reduced. When necessary to extend landing gear:

Landing Gear ............................... DOWN Gear Electrical Override.............. DOORS

.................................................. WAIT 3 SECONDS Gear Electrical Override.............. GEAR/DOORS

Relevant Inoperative Items: ISIS/Standby altimeter (#) Audio System 2

APU Fire Detection System Pitot Heating 3

ENG 2 Fire Detection System Standby attitude indicator

APU Control RMU 2

Landing Gear Lever Control RH Wing A/Ice

(#) Inoperative ISIS - Applicable for airplanes S/N 484, 495, 528 and 555.



END

END


EAP 5-10 REVISION 4

ESSENTIAL BUS 1-2 OFF

EICAS Caution: ESS BUS 1-2 OFF

Bus Ties .................................................OFF MFD Pictorial Electrical ........................CHECK

No

Yes

Battery 1 and 2.......................................OFF No

Yes

ESSENTIAL BUS 1 OFF Procedure (EAP 5-8).........................AS REQUIRED

No

Yes

ESSENTIAL BUS 2 OFF Procedure (EAP 5-9)..............................AS REQUIRED

No

Yes

Battery 1.................................................OFF ESSENTIAL BUS 1 (2) OFF Procedure

(EAP 5-8 or EAP 5-9) ........................AS REQUIRED No

Yes

Battery 2.................................................OFF ESSENTIAL BUS 1 (2) OFF Procedure

(EAP 5-8 or EAP 5-9) ........................AS REQUIRED


BOTH DC BUSES ENERGIZED?

DC BUS 1 IS ENERGIZED?

DC BUS 2 IS ENERGIZED?

END

ESSENTIAL BUS 1 STILL OFF?

END

ESSENTIAL BUS 2 STILL OFF?


REVISION 4 EAP 5-11


No

Yes

Landing configuration: Flaps ............................................. 22º VREF................................................ VREF45° + 10 KIAS


Affected Equipment (EAP 5-15) .... CHECK


Flaps ............................................. 22º VREF................................................ VREF45° + 30 KIAS


Affected Equipment (EAP 5-15) ...... CHECK

END

END

ICING CONDITIONS?


EAP 5-12 ORIGINAL

GENERATOR OFF BUS

EICAS Caution: GEN 1 (2, 3, 4) OFF BUS or APU GEN OFF BUS

MFD Indication: Generator voltage may be amber.

No

Yes

LOSS OF ALL GENERATORS Procedure (EAP 5-13).......................ACCOMPLISH

Affected Generator................................PUSH OUT, THEN PUSH IN

APU (if serviceable) ..............................AS REQUIRED

GENERATOR OVERLOAD

EICAS Caution: GEN 1 (2, 3, 4) OVLD or APU GEN OVLD

MFD Indication: Generator may be amber.

Shed Buses............................................OFF No

Yes

Electrical Load (affected generator).....REDUCE The equipments that require more electrical load and may be turned OFF, at pilot’s discretion, are: lights, hydraulic electric pump, ice protection and air conditioning related systems. Non-required equipment may also be turned OFF.

No

Yes

APU.........................................................STOP

APU.........................................................START APU GEN................................................CHECK

PUSHED IN

END

END

END

ALL GENERATORS OFF BUS?

MESSAGE PERSISTS?

APU GEN OVLD EICAS MESSAGE DISPLAYED?

END


REVISION 9 EAP 5-13

LOSS OF ALL GENERATORS

EICAS Caution: GEN 1-2-3-4 OFF BUS Condition: Noise increase due to nose landing

gear doors open. The following message may be displayed:

EICAS Caution: APU GEN OFF BUS

Generators .............................................PUSH OUT, THEN PUSH IN

APU Generator ......................................AS REQUIRED No

Yes

LAND AT THE NEAREST SUITABLE AIRPORT. CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED

LANDING DISTANCE BY 1.95. Essential Power.....................................PUSH IN Airspeed.................................................MAX 250 KIAS Altitude...................................................MEA OR


Crew Oxygen .........................................AS REQUIRED Passenger Oxygen................................AS REQUIRED Emerg Lts...............................................OFF

If required, turn on Emergency Lights before landing. Icing Conditions ....................................EXIT/AVOID Use standby instruments and RMU Navigation Backup Page.

CAUTION: BATTERY DURATION IS 40 MINUTES.

FUEL XFER CRITICAL or CHECK ACFT LOAD EICAS Message ................................MONITOR

Do not set Thrust Levers below idle in flight. Do not actuate Thrust Reversers. Landing configuration:

Landing Gear ...................................DOWN If necessary:

LG WARN Cutout.......................PRESS

FLAP POSITION MINIMUM AIRSPEED

0 to 8° VREF 45 + 30 KIAS

9 to 21° VREF 45 + 10 KIAS

22 to 44° VREF 45 + 5 KIAS

45° VREF 45


ANY GENERATOR RECOVERED?

END


EAP 5-14 REVISION 9



Relevant Inoperative Items:

Autopilot W/S 1 and 2 Heating and Wiper EGPWS

FMS 1 and 2 Transponder 1 and 2 RA 1

Speed Brake Main Pitch Trim TCAS

Pack 1 and 2 Stick Pusher Steering

VHF2/ADF2/VOR2/DME2/ILS2/MB2 and DME1 Flaps

Afected Equipment

(EAP 5-15 and 5-16).........................CHECK END


REVISION 9 EAP 5-15

ANNEX 01

In case of electrical bus failure, refer to the following table to verify the affected equipment.

DC BUS 1 DC BUS 2

AILERON CONTROL SYSTEM 1 AIR/GND POSITION SYSTEM A AOA 1 SENSOR HEATING AUTOMATIC PRESSURIZATION CONTROL BRAKES TEMP INDICATION OUTBD CMC CREW PEDAL ADJUSTMENT CREW SEAT ADJUSTMENT 1 EICAS POWER (DAU 1B) ELECTRICAL FLIGHT IDLE STOP 1 ELECTRONIC BAY COOLING (EXHAUST

1 AND RECIRC 2) EMER/PARKING BRAKE ENG 1 FUEL PUMPS 1C ENG 1 THRUST REVERSER COMMAND ENGINE 1 LIP ANTI-ICE FLAP CHANNEL1 FUEL PRESSURE REFUELING FWD/AFT

A1 FUEL PRESSURE REFUELING FWD 1 FUEL TRANSFER 1 GROUND SPOILER OUTBD HYDRAULIC ELECTRIC PUMP 2 HYDR GEN SYS 2 INDICATION ICE DETECTOR 1 CLEAR ICE DET - CHANNEL 1 INVERTER LAVATORY FLUSH LAVATORY SMOKE DETECTOR LAVATORY WATER DRAIN HEATER LIGHTING CABIN 1 LIGHTING OVERHEAD PANEL LIGHT – COCKPIT READING LIGHTS – COURTESY/STAIR 2 LIGHTS – FLOOD/STORM LIGHTS – LANDING 1 LIGHTS – LAVATORY LIGHTS – LOGOTYPE LIGHTS – NAVIGATION LIGHTS – PASSENGER CABIN 1 MAIN DOOR CONTROL 1 PACK VALVE 1 PASSENGER SIGNS PITCH TRIM (MAIN) PITOT 1 HEATING PNEUMATIC HSV 1 SPEED BRAKE STABILIZER ANTI-ICE INDICATION STATIC PORT HEATING 1 STROBE LIGHTS TAT 1 SENSOR HEATING TCAS 2000 WINDSHIELD HEATING 1 WINDSHIELD WIPER 1 WING ANTI-ICE YAW TRIM

ADC 2 AHRS 2 AILERON CONTROL SYSTEM 2 AIR/GND POSITION SYSTEM C AOA 2 SENSOR HEATING AUDIO - OBSERVER (INTPH 3) AURAL WARNING SYSTEM 2 BAGGAGE SMOKE DETECTOR BRAKES TEMP INDICATION INBD CABIN RECIRCULATION CLEAR ICE DET - CHANNEL 2 CLOCK - COPILOT'S CREW SEAT ADJUSTMENT 2 DEFUELING DISPLAY PRCS/CTRL PWR 2 (IC2) EICAS POWER (DAU 2B) ELECTRICAL FLIGHT IDLE STOP 2 ELECTRONIC BAY COOLING (RECIRC 1

AND EXHAUST 2) ENG 2 FUEL PUMPS 2C ENG 2 THRUST REVERSER COMMAND ENGINE 2 LIP ANTI-ICE ENGINE VIBRATION SENSORS FLAP CHANNEL 2 FUEL FUS PUMPS AFT/FWD 2A FUEL FUS PUMPS FWD 2B FUEL TRANSFER 2 GASPER FAN GROUND SPOILER INBD GUST LOCK (ELECTROMECHANICAL) HYDR ELECTRIC PUMP 1 HYDR GEN SYS 1 INDICATION ICE DETECTOR 2 IRS 2 LANDING GEAR DOOR COMMAND LANDING GEAR LEVER SOLENOID LIGHTING OVERHEAD PANEL LIGHTS – COMPARTMENT LIGHTS – INSPECTION LIGHTS – LANDING LIGHTS – PASSENGER CABIN 2/3 LIGHTS – RED BEACON PACK VALVE 2 PITOT 2 HEATING PNEUMATIC HSV 2 ROLL TRIM SYSTEM SENSORS HEATING CONTROL SPOILER INDICATION SPS (SHAKER 2/CHANNEL 2) SPS PUSHER STABILIZER ANTI-ICE STATIC PORT HEATING 2 STEERING TAT 2 SENSOR HEATING WINDSHIELD WIPER 2 WING ANTI-ICE 1 INDICATION


EAP 5-16 REVISION 9

ANNEX 01

In case of electrical bus failure, refer to the following table to verify the affected equipment.

ESSENTIAL BUS 1 ESSENTIAL BUS 2

(#) Applicable for airplanes with AMPL 1 supplied by ESSENTIAL DC BUS 2.

(##) Applicable for airplanes S/N 484, 495, 528 and 555.

ADC 1 AHRS 1 AIR/GND POSITION SYSTEM B APU BLEED AUDIO PILOT/COPILOT (INTPH 1) AURAL WARNING SYSTEM 1 BRAKES OUTBOARD CABIN PRESSURE ACQUISITION MODULE (CPAM) CLOCK PILOT'S DISPLAY PRCS/CTRL PWR 1 (IC 1)EICAS DISPLAY EICAS (DAU 1A) ENG 1 FIRE DETECTION 1 ENG 1 FUEL PUMPS 1A ENG 2 FUEL PUMPS 2B ENGINES 1 AND 2 FADECS A ENGINE 1 STARTING ENGINES N2 SIGNALS 1A AND 2A FDR MANAGEMENT FUEL QUANTITY INDICATION 1 LDG CONTROL (DOWN OVRD) LANDING GEAR NOSE

INDICATION 1 LIGHTS COCKPIT DOME IRS 1 PANEL LIGHTING PILOT'S PASSENGER OXYGEN SYSTEM 1 PNEUMATIC 1 (EBV 1) RAM AIR DISTRIBUTION RMU 1 RUDDER CONTROL SYSTEM 2 SPS (SHAKER 1/CHANNEL 1) VHF 1

AIR/GND POSITION SYSTEM D APU CONTROL APU FIRE DETECTION APU FIRE EXTINGUISHING APU FUEL FEED AUDIO PILOT/COPILOT (INTPH 2) BRAKES INBOARD COCKPIT/ATTENDANT

INTERCOMM CROSSBLEED EICAS (DAU 2A) ENG 2 FIRE DETECTION 2 ENG 1 FUEL PUMPS 1B ENG 2 FUEL PUMPS 2A ENGINES 1 AND 2 FADEC B ENGINE 2 ANTI-ICE INDICATION ENGINE 2 STARTING ENGINES N2 SIGNALS 1B AND 2B FUEL CROSS FEED FUEL QUANTITY INDICATION 2 ISIS (##) LANDING GEAR CONTROL LDG NOSE INDICATION 2 LIGHTING EMERGENCY CTRL LIGHTING PANEL COPILOT'S AND

PEDESTAL PASSENGER OXYGEN SYSTEM 2 PITCH TRIM BACKUP PITOT HEATING 3 PNEUMATIC 2 (EBV 2) PUBLIC ADDRESS (#) RMU 2 RUDDER CONTROL SYSTEM 1 STANDBY ALTIMETER STANDBY ATTITUDE INDICATOR VOICE RECORDER WING ANTI-ICE INDICATION 2

EMERGENCY/ABNORMAL PROCEDURES Engine

REVISION 9 EAP 6-1 QR

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TABLE OF CONTENTS ANNUNCIATED PROCEDURES

ATTCS FAILURE.................................................EAP 6-3

BLEED ENGINE LEAK ......................... refer to EAP 1-4

DUAL ENGINE FAILURE....................................EAP 6-3

ENGINE ATTCS NO MARGIN.............................EAP 6-5

ENGINE FIRE, SEVERE DAMAGE OR SEPARATION .................................................EAP 6-6

ENGINE OIL LOW PRESSURE ..........................EAP 6-7

ENGINE ANTI-ICING FAILURE ............ refer to EAP 11-5

ENGINE ATS SHUTOFF VALVE OPEN .............EAP 6-8

ENGINE CONTROL FAILURE ............................EAP 6-9

ENGINE FUEL LOW PRESSURE......... refer to EAP 9-6

ENGINE FUEL LOW TEMPERATURE . refer to EAP 9-7

ENGINE FUEL SHUTOFF VALVE INOPERATIVE ...................................refer to EAP 9-7

ENGINE OUT.......................................................EAP 6-10

ENGINE THRUST LEVER FAILURE ..................EAP 6-11

ENGINE THRUST REVERSER FAILURE/DISAGREE .....................................EAP 6-12

ENGINE FUEL FILTER IMPENDING BYPASS ...................................EAP 6-12

ENGINE HYDRAULIC PUMP FAILURE...........................................refer to EAP 10-8

ENGINE IDLE STOP FAILURE..........................EAP 6-13


ABNORMAL ENGINE START................refer to NAP-15

ENGINE ABNORMAL VIBRATION........refer to NAP-18

ENGINE AIRSTART ...............................refer to NAP-19

ENGINE FAILURE/SHUTDOWN............refer to NAP-23

ENGINE OIL HIGH PRESSURE.............refer to NAP-24

ENGINE OIL HIGH TEMPERATURE .....refer to NAP-24

ENGINE OIL LOW LEVEL......................refer to NAP-24

ENGINE OIL LOW PRESSURE .............refer to NAP-25

ENGINE OVERTEMPERATURE............refer to NAP-25

LOSS OF ENGINE INDICATIONS .........refer to NAP-30

ONE ENGINE INOPERATIVE APPROACH AND LANDING.............refer to NAP-35

SINGLE ENGINE BLEED OPERATION IN ICING CONDITIONS .....................refer to NAP-41


EAP 6-2 REVISION 9

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ATTCS FAIL ........................................................EAP 6-3

BLD 1 (2) LEAK..................................... refer to EAP 1-4

E1 (2) ATTCS NO MRGN ....................................EAP 6-5

E1 (2) OIL LOW PRESS......................................EAP 6-7

ENG 1 (2) FIRE....................................................EAP 6-6

ENG 1-2 OUT.......................................................EAP 6-3

E1 (2) A/ICE FAIL ................................. refer to EAP 11-5

E1 (2) ATS SOV OPN.........................................EAP 6-8

E1 (2) CTL FAIL ..................................................EAP 6-9

E1 (2) FUEL LO PRESS........................ refer to EAP 9-6

E1 (2) FUEL LO TEMP .......................... refer to EAP 9-7

E1 (2) FUEL SOV INOP......................... refer to EAP 9-7

ENG1 (2) OUT......................................................EAP 6-10

ENG1 (2) REV DISAGREE..................................EAP 6-12

ENG1 (2) REV FAIL.............................................EAP 6-12

ENG1 (2) TLA FAIL .............................................EAP 6-11

E1 (2) FUEL IMP BYP ........................................EAP 6-12

E1 (2) HYD PUMP FAIL........................ refer to EAP 10-8

E1 (2) IDL STP FAIL...........................................EAP 6-13



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ATTCS FAILURE

EICAS Warning: ATTCS FAIL

Thrust Levers ........................................MAX

Another takeoff is not permitted.

DUAL ENGINE FAILURE

EICAS Warning: ENG 1-2 OUT may be presented.

Oxygen Mask .........................................AS REQUIRED Fuel Pump Pwr Tank 1 and 2 ...............ON Fuel Pump Sel 1 and 2 ..........................A OR B APU.........................................................START Airspeed for engine windmilling start: Above 10’000 ft .................................MIN 250 KIAS Below 10’000 ft..................................220 TO 250 KIAS

Transponder ..........................................7700 TCAS ......................................................TA ONLY

No

Yes

Thrust Levers ........................................IDLE Engine 1 and 2 Start/Stop Selectors ...STOP APU Bleed..............................................PUSH IN Engine Bleeds 1 and 2 ..........................PUSH OUT Below 25’000 ft:

Engine 1 Start/Stop Selector ...........START, THEN RUN

No

Yes

ENGINE 2 AIRSTART Procedure (NAP-19)..........................ACCOMPLISH

Engine 1 Start/Stop Selector................STOP Engine 2 Start/Stop Selector................START, THEN

RUN


END

END

ENGINE 1 STARTS?

APU SERVICEABLE?


EAP 6-4 REVISION 9 QR

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CONTINUED FROM PREVIOUS PAGE No

Yes ENGINE 1 AIRSTART

Procedure (NAP-19)..........................AS REQUIRED

NOTE: Windmilling starts can be attempted in both engines simultaneously.

N2............................................................MIN 10%

Initiate windmilling start with N2 as high as possible. Once N2 is below 10%, it may not be recovered.

Thrust Levers ........................................IDLE Engine 1 and 2 Start/Stop Selectors....STOP Engine 1 and 2 Start/Stop Selectors....START, THEN

RUN No

Yes No

Yes

ENGINE AIRSTART (inoperative engine) Procedure (NAP-19)..........................AS REQUIRED

ENGINE FAILURE/SHUTDOWN

(inoperative engine) Procedure (NAP-23)..........................AS REQUIRED

DITCHING (NAP-5) OR FORCED LANDING (NAP-8) Procedure ..........ACCOMPLISH

END

ENGINE 2 STARTS?

END

ANY ENGINE STARTS?

END

INOPERATIVE ENGINE START CONSIDERED?

END



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ENGINE ATTCS NO MARGIN

EICAS Warning: E1 (2) ATTCS NO MRGN

Do not takeoff. END



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ENGINE FIRE, SEVERE DAMAGE OR SEPARATION

EICAS Warning: ENG 1 (2) FIRE (in case of fire). Light: Engine Fire Handle Aural Warning: BELL (in case of fire).

Associated Thrust Lever ......................IDLE Associated Start/Stop Selector............STOP Associated Fire Extinguishing Handle................................................PULL (DO NOT

ROTATE) FUS TK XFER.........................................OFF

LAND AT THE NEAREST SUITABLE AIRPORT. TCAS ......................................................TA ONLY

Displayed

Not Displayed XFeed .....................................................OFF Associated Fuel Pump Power..............OFF

...........................................................WAIT 30 SECS No

Yes

Fire Extinguishing Handle (1st shot) ....ROTATE

...........................................................WAIT 30 SECS

No

Yes

Fire Extinguishing Handle (2nd shot). . ROTATE

No

Yes

Fire Extinguishing Handle (one shot, if available)......................ROTATE

No

Yes

Autopilot ................................................DISENGAGE Yaw Damper...........................................DISENGAGE Airspeed.................................................REDUCE

Chase the better airspeed to reduce the vibration. Airspeeds around 180 KIAS are recommended.


ENG 1 (2) FIRE MESSAGE PERSISTS?

ENG 1 (2) FIRE MESSAGE PERSISTS?

E1 (2) FUELSOV CLSD MESSAGE?

ENGINE FAILURE ASSOCIATED TO HIGH VIBRATION?

E1 (2) FIREDET FAIL MESSAGE DISPLAYED?



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CONTINUED FROM PREVIOUS PAGE Associated Bleed ..................................PUSH OUT Remaining Engine Thrust Rating ........CON APU.........................................................START APU Bleed..............................................AS REQUIRED XBleed ....................................................AS REQUIRED

Altitude...................................................MAX 25’000 FT, MIN MEA

No

Yes

Altitude...................................................MAX 15’000 FT, MIN MEA

If it is not possible to descend below 15’000 ft: Icing Conditions ...............................EXIT

ONE ENGINE INOPERATIVE APPROACH AND LANDING Procedure (NAP-35) ........AS REQUIRED

ENGINE OIL LOW PRESSURE

EICAS Warning: E1 (2) OIL LOW PRESS may be presented.

EICAS Indication: Oil pressure may be red.

No

Yes

Associated Thrust Lever ......................IDLE

Reduce Thrust Lever to at least N2 below 88%, until pressure is within limits.

No

Yes

Associated ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)..........................ACCOMPLISH

Message .................................................DISREGARD

END

ICING CONDITIONS?

END

OIL PRESSURE IN THE RED RANGE?

OIL PRESSURE STILL IN THE RED RANGE?


EAP 6-8 REVISION 10

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ENGINE ATS SHUTOFF VALVE OPEN

EICAS Caution: E1 (2) ATS SOV OPN

XBleed ....................................................CLOSE Associated Bleeds

(including APU bleed) ......................PUSH OUT No

Yes

Thrust Levers ........................................IDLE Associated Start/Stop Selector............STOP

NOTE: If engine shutdown does not occur, pull the fire extinguishing handle.

Icing Conditions ....................................EXIT/AVOID Altitude...................................................MAX 25’000 FT,

MIN MEA

END

END

ON GROUND?


REVISION 9 EAP 6-9

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ENGINE CONTROL FAILURE

EICAS Caution: E1 (2) CTL FAIL may be presented.

CAUTION: DO NOT MANUALLY ALTERNATE ASSOCIATED FADECS.

FADEC In Control ..................................CHECK Associated FADEC................................RESET

No

Yes

Avoid quick movements of the associated Thrust Lever.

NOTE: Thrust Lever movements may cause surge or an uncommanded engine shutdown.

Affected ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)..........................AS REQUIRED

Engine control recovered.

FADEC IN CONTROL CHANGES?

END

END


EAP 6-10 REVISION 9

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ENGINE OUT

EICAS Caution: ENG1 (2) OUT

Associated Thrust Lever ......................IDLE Associated Start/Stop Selector............STOP

NOTE: If engine shutdown does not occur, pull the associated fire extinguishing handle.

Engine Thrust Rating............................CON APU (if available) ...................................START APU Bleed..............................................AS REQUIRED XBleed ....................................................AS REQUIRED Fuel.........................................................BALANCE

No

Yes

Affected ENGINE AIRSTART Procedure (NAP-19)..........................ACCOMPLISH

LAND AT THE NEAREST SUITABLE AIRPORT. TCAS ......................................................TA ONLY Altitude...................................................MAX 25’000 FT,

MIN MEA No

Yes

XBleed ....................................................OPEN Altitude...................................................MEA OR


If it is not possible to descend below 15’000 ft: Icing Conditions ...............................EXIT

ONE ENGINE INOPERATIVE

APPROACH AND LANDING Procedure (NAP-35)..........................AS REQUIRED

ENGINE RESTART CONSIDERED?

END

END

ICING CONDITIONS?


REVISION 9 EAP 6-11

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ENGINE THRUST LEVER FAILURE

EICAS Caution: ENG1 (2) TLA FAIL

Associated FADEC................................RESET No

Yes

Associated FADEC................................ALTN

No

Yes

Thrust can be partially controlled through the Thrust Rating Buttons.

Affected ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)..........................AS REQUIRED

THRUST LEVER CONTROL RECOVERED?

END

THRUST LEVER CONTROL RECOVERED?

END

END



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ENGINE THRUST REVERSER FAILURE/DISAGREE

EICAS Caution: ENG1 (2) REV FAIL or ENG1 (2) REV DISAGREE

No

Yes

Do not takeoff.

No

Yes

LAND AT THE NEAREST SUITABLE AIRPORT. Associated Thrust Lever ......................IDLE

Airspeed.................................................MAX 200 KIAS

Associated ENGINE FAILURE/SHUTDOWN Procedure (NAP-23)..........................ACCOMPLISH

Message .................................................DISREGARD

ENGINE FUEL FILTER IMPENDING BYPASS

EICAS Advisory: E1 (2) FUEL IMP BYP No

Yes

LAND AT NEAREST SUITABLE AIRPORT.

END

ASSOCIATED N1 INDICATION BELOW THRUST LEVER SETTING?

ON GROUND?

END

END

BOTH FILTERS AFECTED?

END


REVISION 9 EAP 6-13

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ENGINE IDLE STOP FAILURE

EICAS Advisory: E1 (2) IDL STP FAIL

Protection against thrust lever movement below flight idle is not available.

Be careful when reducing engines near IDLE.

CAUTION: NEVER SET THRUST LEVER BELOW IDLE INFLIGHT.

END



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INTENTIONALLY BLANK

EMERGENCY/ABNORMAL PROCEDURES Fire Protection

ORIGINAL EAP 7-1

TABLE OF CONTENTS ANNUNCIATED PROCEDURES

BAGGAGE SMOKE................................refer to S-3

ENGINE FIRE, SEVERE DAMAGE OR SEPARATION ....................................refer to EAP 6-6

APU FIRE DETECTION FAILURE .......................EAP 7-3

APU FIRE EXTINGUISHING INOPERATIVE.......EAP 7-3

BAGGAGE COMPARTMENT FIRE EXTINGUISHING INOPERATIVE....................EAP 7-4

ENGINE FIRE DETECTION FAILURE.................EAP 7-4

ENGINE FIRE EXTINGUISHING INOPERATIVE .................................................EAP 7-5


CABIN FIRE OR SMOKE .......................refer to S-5

ELECTRICAL SYSTEM FIRE OR SMOKE ............................................refer to S-6


EAP 7-2 ORIGINAL


BAGG SMOKE .......................................refer to S-3

ENG 1 (2) FIRE.......................................refer to EAP 6-6

APU FIREDET FAIL .............................................EAP 7-3

APU EXTBTL INOP .............................................EAP 7-3

BAGG EXTBTL INOP...........................................EAP 7-4

E1 (2) FIREDET FAIL ..........................................EAP 7-4

E1 (2) EXTBTLA INOP ........................................EAP 7-5

E1 (2) EXTBTLB INOP ........................................EAP 7-5


ORIGINAL EAP 7-3

APU FIRE DETECTION FAILURE

EICAS Caution: APU FIREDET FAIL

APU FIRE Procedure (EAP 3-3)............ACCOMPLISH

APU FIRE Procedure (EAP 3-3)............ACCOMPLISH

The APU fire detection system is inoperative.

APU FIRE EXTINGUISHING INOPERATIVE

EICAS Caution: APU EXTBTL INOP Condition: Affected bottle has not been

discharged intentionally.

APU fire protection is not available. Consider shutting the APU down. END

END

ASSOCIATED TO SUSPECTED APU FIRE OR OVERHEAT?

END

ASSOCIATED TO APU FAILURE?

END

No

Yes

No

Yes


EAP 7-4 ORIGINAL

BAGGAGE COMPARTMENT FIRE EXTINGUISHING INOPERATIVE

EICAS Caution: BAGG EXTBTL INOP (if installed). Condition: Affected bottle has not been

discharged intentionally.

LAND AT THE NEAREST SUITABLE AIRPORT. BAGGAGE SMOKE Procedure (S-3)....AS REQUIRED

Baggage fire protection is not available.

ENGINE FIRE DETECTION FAILURE

EICAS Caution: E1 (2) FIREDET FAIL

Affected ENGINE FIRE, SEVERE DAMAGE OR SEPARATION Procedure (EAP 6-6).........................ACCOMPLISH

Affected ENGINE FIRE, SEVERE DAMAGE OR SEPARATION Procedure (EAP 6-6).........................ACCOMPLISH

The associated engine fire detection system is inoperative.

END

BAGG SMOKE MESSAGE DISPLAYED?

END

No

Yes

ASSOCIATED TO ENGINE FAILURE?

END

No

Yes

No

END

ASSOCIATED TO SUSPECTED ENGINE FIRE OR OVERHEAT?

END

Yes


ORIGINAL EAP 7-5

ENGINE FIRE EXTINGUISHING INOPERATIVE

EICAS Caution: E1 (2) EXTBTLA INOP or E1 (2) EXTBTLB INOP

Condition: Affected bottle has not been discharged intentionally.

Only one bottle is available to protect both engines against fire.

END


EAP 7-6 ORIGINAL

INTENTIONALLY BLANK

EMERGENCY/ABNORMAL PROCEDURES Flight Controls

ORIGINAL EAP 8-1

TABLE OF CONTENTS


PITCH TRIM INOPERATIVE ...............................EAP 8-3

AILERON SYSTEM INOPERATIVE ....................EAP 8-5

FLAP FAILURE ...................................................EAP 8-6

INADVERTENT SPOILER OPEN........................EAP 8-7

PITCH TRIM SWITCH INOPERATIVE ................EAP 8-8

RUDDER HARDOVER PROTECTION FAILURE.........................................................EAP 8-8

RUDDER MOVABLE STOPS DISAGREE ..........EAP 8-8

RUDDER OVERBOOST......................................EAP 8-9

RUDDER SYSTEM INOPERATIVE.....................EAP 8-10

SPEED BRAKE LEVER DISAGREE...................EAP 8-11

FLAP LOW ACTUATION SPEED .......................EAP 8-11


AILERON RUNAWAY ........................... refer to NAP-3

JAMMED AILERON............................... refer to NAP-10

JAMMED ELEVATOR ........................... refer to NAP-10

JAMMED RUDDER ............................... refer to NAP-11

PITCH TRIM RUNAWAY....................... refer to NAP-13

ROLL TRIM RUNAWAY........................ refer to NAP-3

AILERON ARTIFICIAL FEEL INOPERATIVE .................................. refer to NAP-17

ASYMMETRIC RUDDER OPERATION ..................................... refer to NAP-17

GUST LOCK FAILURE.......................... refer to NAP-27

RUDDER ARTIFICIAL FEEL INOPERATIVE .................................. refer to NAP-39

RUDDER RUNAWAY ............................ refer to NAP-40

STIFFENED ELEVATOR....................... refer to NAP-41

UNCOMMANDED AILERON DISCONNECTION ............................ refer to NAP-43

UNCOMMANDED ELEVATOR DISCONNECTION ............................ refer to NAP-43

YAW TRIM RUNAWAY ......................... refer to NAP-40


EAP 8-2 ORIGINAL


PTRIM BACKUP INOP........................................EAP 8-3

PTRIM MAIN INOP ..............................................EAP 8-3

AIL SYS 1 (2) INOP .............................................EAP 8-5

FLAP FAIL...........................................................EAP 8-6

PTRIM BKP SW FAIL..........................................EAP 8-8

PTRIM CPT SW FAIL ..........................................EAP 8-8

PTRIM F/O SW FAIL ...........................................EAP 8-8

RUD HDOV PROTFAIL .......................................EAP 8-8

RUD STOP DISAGREE.......................................EAP 8-8

RUDDER OVERBOOST......................................EAP 8-9

RUDDER SYS 1 (2) INOP....................................EAP 8-10

RUDDER SYS 1-2 INOP......................................EAP 8-10

SPBK LVR DISAGREE .......................................EAP 8-11

SPOILER FAIL.....................................................EAP 8-7

FLAP LOW SPEED .............................................EAP 8-11


ORIGINAL EAP 8-3

PITCH TRIM INOPERATIVE

EICAS Warning: PTRIM MAIN INOP and/or PTRIM BACKUP INOP

The following message may be displayed: EICAS CAUTION: AUTO TRIM FAIL

Both

Main Backup

Pitch Trim Main Sys Cutout..................PUSH OUT Autopilot ................................................DISENGAGE

Back up system can be used to trim the airplane.

Pitch Trim Backup Sys Cutout.............PUSH OUT Main system can be used to trim the airplane. Autopilot is available.

Pitch Trim Main Sys Cutout..................PUSH OUT Pitch Trim Backup Sys Cutout.............PUSH OUT Consider LANDING AT THE NEAREST SUITABLE AIRPORT Autopilot ................................................DISENGAGE

Continue the flight using operative switch. If Main Pitch Trim System is inoperative, do not engage the Autopilot.


END

END

INOPERATIVE SYSTEM(S)?

Yes

No MESSAGE DISPLAYED WITHOUT PRESSING ANY PITCH TRIM SWITCH?

AIRPLANE PITCH UP TENDENCY?

Yes

No

ANY PITCH TRIM SWITCH (PILOT, COPILOT OR BACKUP) WORKING?

END

Yes

No


EAP 8-4 ORIGINAL


WARNING: DO NOT OPEN SPEEDBRAKE.

Airspeed.................................................REDUCE If it is necessary to reduce airspeed below 180 KIAS (or 200 KIAS in icing conditions), extend flaps to 9° (at 20000 ft maximum). If it is necessary to reduce airspeed below 160 KIAS, extend flaps to 22°.

NOTE: Turning the airplane and extending the landing gear helps to maintain minimum airspeed with unwanted pitch up tendency.

Landing Configuration: Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 10 KIAS CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED

LANDING DISTANCE BY 1.45.

WARNING: DO NOT OPEN SPEEDBRAKE.

Airspeed.................................................REDUCE Below 250 KIAS ................................FLAPS 9°

(MAX 20’000 FT) Below 180 KIAS ................................FLAPS 22°

Reducing speed and extending flaps helps to reduce control forces.

Landing Configuration:

Landing Gear ....................................DOWN Delay gear extension as long as possible. Flaps ..................................................22° VREF.....................................................VREF45 + 25 KIAS CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED


END

END

AIRPLANE PITCH DOWN TENDENCY?No

Yes


ORIGINAL EAP 8-5

AILERON SYSTEM INOPERATIVE

EICAS Caution: AIL SYS 1 (2) INOP

Affected Aileron Shutoff .......................PUSH OUT Airspeed.................................................MAX 250 KIAS

Yes

Remaining Aileron Shutoff ...................PUSH OUT Autopilot ................................................DISENGAGE

Expect greater aileron control force. If required, both pilots should act together to control airplane.

Avoid landing at airports with anticipated turbulence, gusts or crosswind. Perform a long final approach. Landing Configuration:

Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 10 KIAS


END

BOTH SYSTEMS FAILED? No


EAP 8-6 REVISION 8

FLAP FAILURE

EICAS Caution: FLAP FAIL Condition: Flap operation is not possible. EICAS Indication: Flap position may become amber.

If flap indication on EICAS is not available, use the RMU Engine Backup Page 2 or flap position marks on the wing.

With flaps at intermediate positions, limit airspeed according to the following:

FLAPS POSITION MAX AIRSPEED

1° to 9° 250 KIAS

10° to 22° 180 KIAS

23° to 45° 145 KIAS

VREF:

FLAPS POSITION VREF


9° to 21° VREF45 + 10 KIAS

22° to 44° VREF45 + 5 KIAS

45° VREF45

At crew discretion: EGPWS CB’s (D2 or J8) ...................PULL

CAUTION: • IF FLAPS FAILED BETWEEN 22° AND 45° POSITIONS, EXIT OR AVOID ICING CONDITIONS.

MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY:

FLAPS POSITION FACTOR

0 to 8° 1.70

9° to 21° 1.40

22° to 44° 1.20

END


REVISION 10 EAP 8-7

INADVERTENT SPOILER OPEN

EICAS Caution: SPOILER FAIL (may be presented). Condition: Sudden airspeed or altitude loss,

buffeting or roll tendency.

EICAS Indication: SPLRS OPN

Speed Brake ..........................................CLOSE

Spoilers CB’s F13, F14 and F20 or F21..........................................PULL

Do not reduce Thrust during flare.


Flaps ..................................................22°

VREF45 ..................................................VREF45 + 10 KIAS

Jammed Open

Jammed Closed or Floating



END

PANEL FAILURE MODE?

END


EAP 8-8 ORIGINAL

PITCH TRIM SWITCH INOPERATIVE

EICAS Caution: PTRIM CPT SW FAIL, PTRIM F/O SW FAIL or PTRIM BKP SW FAIL

No

Yes

Deenergize the airplane and energize it again.

Use another serviceable switch.

RUDDER HARDOVER PROTECTION FAILURE

EICAS Caution: RUD HDOV PROTFAIL

Rudder hardover protection is not available.

RUDDER MOVABLE STOPS DISAGREE

EICAS Caution: RUD STOP DISAGREE (some airplanes may have an indication light instead of EICAS message).

No

Yes

Confirm the stop position with maintenance personnel.

Beyond 10°

10°

Use takeoff performance charts.

Do not takeoff.

More rudder travel may be available. Use rudder with caution.

ON GROUND?

END

END

END

END

ON GROUND?

END

RUDDER STOP POSITION?


ORIGINAL EAP 8-9

RUDDER OVERBOOST

EICAS Caution: RUDDER OVERBOOST

Rudder Shutoff 2 ...................................PUSH OUT

No

Yes

Rudder Shutoff 2 ...................................PUSH IN Rudder Shutoff 1 ...................................PUSH OUT Below 135 KIAS:

Rudder Shutoff 1 ..............................PUSH IN

Below 135 KIAS:

Rudder Shutoff 2 ..............................PUSH IN

END

RUDDER OVERBOOST MESSAGE PERSISTS?

END


EAP 8-10 ORIGINAL

RUDDER SYSTEM INOPERATIVE

EICAS Caution: RUDDER SYS 1 (2) INOP or RUDDER SYS 1-2 INOP

No

Yes

RUDDER RUNAWAY Procedure (NAP-40)..........................ACCOMPLISH

Only one (1 or 2)

Affected Rudder Shutoff.......................PUSH OUT

Rudder Shutoff 2 ...................................PUSH OUT

Yes

Rudder Shutoff 1 ...................................PUSH OUT Rudder Shutoffs 1 and 2.......................PUSH IN

Yes

Expect heavier than normal rudder pedals. If required, combine effort of both pilots.

Consider use of aileron and asymmetric thrust to control the airplane.

Avoid airports with reported gusts, turbulence or crosswind.


END

INOPERATIVE SYSTEM?

RUDDER 1-2 INOP MESSAGE PERSISTS?

RUDDER 1-2 INOP MESSAGE PERSISTS?

FOLLOWING A RUDDER RUNAWAY?

END

Both (1 and 2)

No

No


ORIGINAL EAP 8-11


No

Yes


Flaps ..................................................22°

VREF45 ..................................................VREF45 + 10 KIAS


SPEED BRAKE LEVER DISAGREE

EICAS Caution: SPBK LVR DISAGREE

Speed Brake Lever................................CLOSE

FLAP LOW ACTUATION SPEED

EICAS Advisory: FLAP LOW SPEED

Anticipate flap actuation.

END

END

END

LANDING IN ICING CONDITIONS?


EAP 8-12 ORIGINAL

INTENTIONALLY BLANK

EMERGENCY/ABNORMAL PROCEDURES Fuel

REVISION 9 EAP 9-1

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TABLE OF CONTENTS


CHECK AIRCRAFT LOAD................................ EAP 9-3

FUEL LOW LEVEL............................................ EAP 9-3

FUEL TRANSFER CRITICAL............................ EAP 9-4

APU FUEL LOW PRESSURE .............. refer to EAP 3-5

APU FUEL SHUTOFF VALVE INOPERATIVE ................................. EAP 9-5

ENGINE FUEL LOW PRESSURE..................... EAP 9-6

ENGINE FUEL LOW TEMPERATURE ............. EAP 9-7

ENGINE FUEL SHUTOFF VALVE INOPERATIVE .............................................. EAP 9-7

FUEL CROSSFEED FAILURE.......................... EAP 9-8

FUEL CROSSFEED MISCOMMAND ................ EAP 9-9

FUEL IMBALANCE ........................................... EAP 9-13

FUEL TANK LOW TEMPERATURE ................. EAP 9-9

FUEL TANK VENTILATION VALVE OPEN ............................................... EAP 9-10

FUEL TRANSFER CHECK................................ EAP 9-10

FUEL TRANSFER INOPERATIVE.................... EAP 9-11

FUSELAGE FUEL IMBALANCE....................... EAP 9-13

WING FUEL IMBALANCE................................. EAP 9-15

WING TANKS OVERFLOW .............................. EAP 9-16

ENGINE FUEL FILTER IMPENDING BYPASS ......................refer to EAP 6-12


EAP 9-2 REVISION 9

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CHECK ACFT LOAD......................................... EAP 9-3

FUEL 1 (2) LO LEVEL....................................... EAP 9-3

FUEL XFER CRITICAL...................................... EAP 9-4 APU FUEL LO PRESS ......................... refer to EAP 3-5

APU FUEL SOV INOP....................................... EAP 9-5

E1 (2) FUEL LO PRESS.................................... EAP 9-6

E1 (2) FUEL LO TEMP ...................................... EAP 9-7

E1 (2) FUEL SOV INOP..................................... EAP 9-7

FUEL IMBALANCE ........................................... EAP 9-15

FUEL TANK LO TEMP...................................... EAP 9-9

FUEL TK VENT OPEN ...................................... EAP 9-10

FUEL XFEED FAIL............................................ EAP 9-8

FUEL XFEED MISCMD ..................................... EAP 9-9

FUEL XFER 1 (2) INOP ..................................... EAP 9-11

FUEL XFER CHECK.......................................... EAP 9-10

FUEL XFER OVFLOW....................................... EAP 9-16

FUSELAGE FUEL IMB...................................... EAP 9-13

E1 (2) FUEL IMP BYP .......................... refer to EAP 6-12


REVISION 9 EAP 9-3

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CHECK AIRCRAFT LOAD

EICAS Warning: CHECK ACFT LOAD

Thrust Levers ................................... LONG RANGE SET

FUS TK XFER.................................... FUS 1 OR FUS 2 Fuel Transfer System....................... CHECK STATUS

Yes

Consider diversion. Remaining Fuel ................................ CHECK Avoid rapid maneuvers and flying in severe turbulence conditions.

Before touchdown: Rate of Descent ........................... MAX 450 FT/MIN

Touch smoothly the runway surface. Reduce engine thrust only after touchdown.

FUEL LOW LEVEL

EICAS Warning: FUEL 1 (2) LO LEVEL MFD Indication: Fuel quantity in red range.

Thrust Levers ..................................... LONG RANGE CRUISE

Level the airplane and check available fuel quantities. If necessary, use available auxiliary fuel tanks. No

Yes

LAND AT THE NEAREST SUITABLE AIRPORT. Avoid attitudes in excess of 10° nose down or 10° nose up attitude, uncoordinated maneuvers and negative g's.

XFeed Operation ................................ AS REQUIRED

FUEL TRANSFER OPERATIVE?

END

END

No

END

END

FUEL QUANTITY IS SUFFICIENT?


EAP 9-4 REVISION 9

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FUEL TRANSFER CRITICAL

EICAS Warning: FUEL XFER CRITICAL

Thrust Levers ................................... LONG RANGE SET

FUS TK XFER.................................... FUS 1 OR FUS 2 Fuel Transfer System....................... CHECK STATUS

Yes

Consider diversion. Remaining Fuel ................................ CHECK Avoid rapid maneuvers and flying in severe turbulence conditions.

Before touchdown: Rate of Descent ........................... MAX 450 FT/MIN

Touch smoothly the runway surface. Reduce engine thrust only after touchdown.

FUEL TRANSFER OPERATIVE?

END

END

No


REVISION 9 EAP 9-5

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APU FUEL SHUTOFF VALVE INOPERATIVE

EICAS Caution: APU FUEL SOV INOP

APU Fuel Shutoff Button ................. CHECK NOT PRESSED

No Yes

Disregard the message.

No Yes

APU Master Knob............................. OFF

APU RUNNING NORMALLY?

END

APU SHUTOFF VALVE REMAINS CLOSED?

END


EAP 9-6 REVISION 10

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ENGINE FUEL LOW PRESSURE

EICAS Caution: E1 (2) FUEL LO PRESS Condition: One or more affected tank electric fuel

pump may be inoperative

Associated Fuel Pump Sel .............. SELECT ANOTHER

No

Yes


Avoid rapid thrust lever movements and set minimum required thrust.

NOTE: If required, the flight may proceed above 25’000 ft using XFEED.

No

Yes


Avoid rapid thrust lever movements and set minimum required thrust.

NOTE: If required, the flight may proceed above 25’000 ft using XFEED.

OPERATING WITH TS-1 KEROSENE?

ALL PUMPS INOPERATIVE IN THE AFFECTED TANK?

END


REVISION 9 EAP 9-7

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ENGINE FUEL LOW TEMPERATURE

EICAS Caution: E1 (2) FUEL LO TEMP

WARNING: ENGINE FLAMEOUT MAY OCCUR IF FUEL TANK LO TEMP MESSAGE IS PRESENTED, OR E1 (2) FUEL LO TEMP IS PRESENTED WITHOUT FUEL ICING INHIBITOR.

No Yes

Do not takeoff.

Descend to lower altitude and monitor engine indications as long as the message remains.

ENGINE FUEL SHUTOFF VALVE INOPERATIVE

EICAS Caution: E1 (2) FUEL SOV INOP Engine Fuel Indications..........................MONITOR

No Yes

XFEED ......................................................OFF Associated Fuel Pump Pwr ....................OFF

Fire Extinguishing Handle......................CHECK IN

No Yes

Message ...................................................DISREGARD

LAND AT THE NEAREST SUITABLE AIRPORT. Associated ENGINE FAILURE/SHUTDOWN

Procedure (NAP-23)............................ACCOMPLISH

END

AFTER PULLING FIRE HANDLE?

END

ENGINE OPERATION NORMAL?

END

END

ON GROUND?

END


EAP 9-8 REVISION 9

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FUEL CROSSFEED FAILURE

EICAS Caution: FUEL XFEED FAIL

Crossfeed.......................................... OFF Fuel Imbalance ................................. MONITOR Asymmetric Thrust........................... AS REQUIRED No

Yes

Avoid uncoordinated maneuvers, flying in turbulence conditions and negative g's.

END

END

FUEL XFEED OPEN?


REVISION 9 EAP 9-9

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FUEL CROSSFEED MISCOMMAND

EICAS Caution: FUEL XFEED MISCMD XFEED ............................................... OFF Fuel Imbalance ................................. CHECK XFEED ............................................... AS REQUIRED Check XFEED selector knob properly positioned to correct wing fuel imbalance.

FUEL TANK LOW TEMPERATURE

EICAS Caution: FUEL TANK LO TEMP MFD Indication: Fuel temperature in amber range.

WARNING: ENGINE FLAMEOUT MAY OCCUR.

No Yes

Do not takeoff.

Descend to lower altitude and monitor engine indications as long as the message remains.

END

END

END

ON GROUND?


EAP 9-10 REVISION 9

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FUEL TANK VENTILATION VALVE OPEN

EICAS Caution: FUEL TK VENT OPEN

No

Yes

Do not takeoff.

While there is fuel in aft auxiliary fuel tanks: Altitude.............................................. MAX 25’000 FT,

MIN MEA Airspeed............................................ MAX 300 KIAS

Avoid pitch attitudes in excess of 5° nose up attitude, uncoordinated maneuvers and negative g's.

FUEL TRANSFER CHECK

EICAS Caution: FUEL XFER CHECK

FUS TK XFER.................................... FUS 1 OR FUS 2

ON GROUND?

END

END

END


REVISION 9 EAP 9-11

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FUEL TRANSFER INOPERATIVE

EICAS Caution: FUEL XFER 1 (2) INOP

Yes

Do not takeoff.

Fuel Pump Sel ..............................SELECT ANOTHER

No

Yes

Altitude..........................................MIN 20’000 FT

No

Yes

FUS TK XFER Knob .....................CHECK POSITION

FUS TK XFER Knob .....................OFF

................................................. WAIT 10 SECS

FUS TK XFER Knob .................... RESELECT SAME CHECKED POSITION

Fuel Quantity ................................MONITOR

Check remaining fuel quantity available and consider diversion.

ON GROUND?

MESSAGE PERSISTS?

END

END

MESSAGE PERSISTS?

No


EAP 9-12 REVISION 9

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REVISION 9 EAP 9-13

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FUSELAGE FUEL IMBALANCE

EICAS Caution: FUSELAGE FUEL IMB If fuel imbalance is confirmed:

FUEL XFER MASTER Knob ...............OFF

Auxiliary Tanks Quantity on MFD .....CHECK

Yes

FUS TK XFER Knob ................................ FUS 1

Yes

FUS TK XFER Knob ................................ FUS 2

No

Yes

During approach:

Autopilot..............................................DISENGAGE

END

ANY LEFT SIDE AUXILIARY TANKS QUANTITY DECREASES?

ANY RIGHT SIDE AUXILIARY TANKS QUANTITY DECREASES?

END

No

No

END

MESSAGE PERSISTS?


EAP 9-14 REVISION 9

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REVISION 9 EAP 9-15

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WING FUEL IMBALANCE

EICAS Caution: WING FUEL IMBALANCE No Yes

FUEL LEAK Procedure (NAP-42) .............ACCOMPLISH

If wing fuel imbalance is confirmed:

XFEED Operation................................ACCOMPLISH

END

FUEL LEAK SUSPECTED?

END


EAP 9-16 REVISION 9

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WING TANKS OVERFLOW

EICAS Caution: FUEL XFER OVFLOW

FUS TK XFER.........................................OFF When required: FUS TK XFER ....................................FUS 1 OR FUS 2

Wing Fuel Quantity...........................MONITOR Monitor wing fuel quantity and turn Fuselage Tank Transfer Knob OFF when wing fuel reaches 2400 kg.

END

EMERGENCY/ABNORMAL PROCEDURES Hydraulics

ORIGINAL EAP 10-1

TABLE OF CONTENTS


BOTH HYDRAULIC SYSTEMS FAILURE ..........EAP 10-3

HYDRAULIC SYSTEM 1 FAILURE.....................EAP 10-5

HYDRAULIC SYSTEM 2 FAILURE.....................EAP 10-6

HYDRAULIC SYSTEM OVERHEAT ...................EAP 10-8

ENGINE HYDRAULIC PUMP FAILURE .............EAP 10-8

HYDRAULIC SYSTEM LOW QUANTITY............EAP 10-9


EAP 10-2 ORIGINAL


HYD SYS 1-2 FAIL ..............................................EAP 10-3

HYD SYS 1 FAIL..................................................EAP 10-5

HYD SYS 2 FAIL..................................................EAP 10-6

HYD SYS 1 (2) OVHT ..........................................EAP 10-8

E1 (2) HYD PUMP FAIL.......................................EAP 10-8

HYD1 (2) LO QTY................................................EAP 10-9


REVISION 10 EAP 10-3

BOTH HYDRAULIC SYSTEMS FAILURE

EICAS Caution: HYD SYS 1-2 FAIL MFD Indication: Hydraulic pressure may be amber. Condition: Noise increase due to nose landing

gear doors open.

The following messages will be displayed: EICAS Caution: AIL SYS 1-2 INOP,

RUDDER SYS 1-2 INOP

EICAS Advisory: E1-2 HYD PUMP FAIL

CAUTION: DO NOT OPEN THE SPEED BRAKES.

Airspeed............................................ MAX 250 KIAS

No

Yes

System(s) in green range: Hydraulic Elec Pump(s) .............. ON

No

Yes Hydraulic 2

Hydraulic 1

HYDRAULIC SYSTEM 2 FAILURE Procedure (EAP 10-6).................. AS REQUIRED


LAND AT THE NEAREST SUITABLE AIRPORT. CAUTION: MULTIPLY THE FLAPS 45° UNFACTORED


Autopilot/Yaw Damper..................... DISENGAGE Both Hydraulic Elec Pumps ............ OFF

Expect greater aileron and rudder control force. If required, both pilots should act together to control airplane. Consider using aileron and asymmetric thrust to help yaw control.

NOTE: Pitch Trim and Roll Trim Systems are available.

ANY HYDRAULIC SYSTEM FLUID QUANTITY IN GREEN RANGE?

AT LEAST ONE SYSTEM RECOVERED?

END

WHICH SYSTEM RECOVERED?

END



EAP 10-4 REVISION 4


Relevant Inoperative Items:

Normal gear extension Anti-skid Thrust reversers

Normal brakes Steering Spoilers

Main door retraction

Approach: APU ....................................................AS REQUIRED Altimeters ..........................................SET AND CROSS

CHECKED Approach Aids ..................................SET AND

CROSS CHECKED

Speed Bugs.......................................SET

Set speed bugs considering the new landing configuration presented below.

Pressurization...................................CHECK Go-Around Procedure...........................REVIEW

If necessary, accomplish a normal go-around procedure except that landing gear cannot be retracted.

Before Landing: Free Fall Lever ..................................ACTUATE Landing Gear Lever..........................DOWN

Perform a long final approach. Avoid landings at airports with anticipated crosswind or turbulence.

CAUTION: DO NOT FLARE.

Use rudder for directional control on ground. During landing run, pull Emergency Brake Handle carefully. Landing Configuration:



END


ORIGINAL EAP 10-5

HYDRAULIC SYSTEM 1 FAILURE

EICAS Caution: HYD SYS 1 FAIL MFD Indication: Hydraulic pressure may be amber. Condition: Noise increase due to nose landing

gear doors open.

The following messages will be displayed: EICAS Caution: AIL SYS 1 INOP,

RUDDER SYS 1 INOP

EICAS Advisory: E1 HYD PUMP FAIL

Yes

Hydraulic Elec Pump 1 .........................ON

No

Yes

Hydraulic Elec Pump 1 .........................OFF Airspeed.................................................MAX 250 KIAS Relevant Inoperative Items:

Inboard Spoiler Normal gear extension Thrust reverser 1

Steering Main door retraction Outboard brakes

Before Landing:

Free Fall Lever ..................................ACTUATE

Landing Gear Lever..........................DOWN


Do not actuate engine 1 Thrust Reverser.

No

Yes


Flaps ..................................................22° VREF.....................................................VREF45 + 10 KIAS



HYDRAULIC SYSTEM 1 FLUID QUANTITY IN GREEN RANGE?

SYSTEM RECOVERED?

END

END


No


EAP 10-6 ORIGINAL



Flaps ............................................. 45° VREF................................................ VREF45


HYDRAULIC SYSTEM 2 FAILURE

EICAS Caution: HYD SYS 2 FAIL MFD Indication: Hydraulic pressure may be amber.

The following messages will be displayed: EICAS Caution: AIL SYS 2 INOP,

RUDDER SYS 2 INOP

EICAS Advisory: E2 HYD PUMP FAIL

CAUTION: DO NOT OPEN THE SPEED BRAKES.

Yes

Hydraulic Elec Pump 2..................... ON

No

Yes

Hydraulic Elec Pump 2..................... OFF Airspeed............................................ MAX 250 KIAS Relevant Inoperative Items:

Outboard Spoiler Thrust reverser 2 Inboard brakes

The Emergency/Parking Brake has accumulator pressure only.


Do not actuate engine 2 Thrust Reverser.


HYDRAULIC SYSTEM 2 FLUID QUANTITY IN GREEN RANGE?

SYSTEM RECOVERED?

END

END

No


ORIGINAL EAP 10-7


No

Yes

Landing Configuration: Landing Gear ............................... DOWN Flaps ............................................. 22° VREF................................................ VREF45 + 10 KIAS


Landing Configuration: Landing Gear ............................... DOWN Flaps ............................................. 45° VREF................................................ VREF45

CAUTION: MULTIPLY THE FLAPS 45 UNFACTORED LANDING DISTANCE BY 1.56.

END

END



EAP 10-8 REVISION 9

HYDRAULIC SYSTEM OVERHEAT

EICAS Caution: HYD SYS 1 (2) OVHT

Turn the affected system OFF: Associated Hydraulic

Eng Pump Shutoff................... PUSH IN Associated Hydraulic

Elec Pump................................ OFF EICAS Messages related to associated hydraulic system will be displayed while system is set to OFF.

Airspeed............................................ MAX 250 KIAS For remainder of flight, even if the message is displayed:

Affected Hydraulic System ......... 15 MINUTES OFF, 1 MINUTE ON

NOTE: To turn the hydraulic system ON, first turn the Hydraulic Elec Pump to AUTO. As soon as the system pressure is recovered, push out the Hydraulic Eng Pump Shutoff button.

During Approach and Landing or when required: Affected Hydraulic System ......... ON

After reaching taxi speed or when the system is no longer required:

Affected Hydraulic System ......... OFF

ENGINE HYDRAULIC PUMP FAILURE

EICAS Advisory: E1 (2) HYD PUMP FAIL Altitude.............................................. MAX 37000 FT Associated Hydraulic Elec Pump ... CHECK ON

Hydraulic 2

Hydraulic 1


NOTE: Do not open the Speed Brakes.


END

END

AFFECTED SYSTEM?

END


ORIGINAL EAP 10-9

HYDRAULIC SYSTEM LOW QUANTITY

EICAS Advisory: HYD1 (2) LO QTY MFD Indication: Hydraulic fluid quantity may be amber.

Affected Hydraulic System.............. MONITOR

Hydraulic 2

Hydraulic 1


NOTE: Do not open the Speed Brakes.


END

END

AFFECTED SYSTEM?


EAP 10-10 ORIGINAL

INTENTIONALLY BLANK

EMERGENCY/ABNORMAL PROCEDURES Ice & Rain Protection

ORIGINAL EAP 11-1

TABLE OF CONTENTS


ICING CONDITIONS WITH ANTI-ICING INOPERATIVE...............................................EAP 11-3

ANTI-ICING LOW CAPACITY.........................EAP 11-4

ANTI-ICING SWITCH OFF ..............................EAP 11-4

AOA HEATING INOPERATIVE.......................EAP 11-4

ENGINE ANTI-ICING FAILURE ......................EAP 11-5

ICE DETECTOR FAIL .....................................EAP 11-5

NO ICE - ANTI-ICE ON....................................EAP 11-6

PITOT HEATING INOPERATIVE ....................EAP 11-6

STABILIZER ANTI-ICING FAILURE...............EAP 11-8

TAT HEATING INOPERATIVE........................EAP 11-7

WINDSHIELD HEATING FAILURE.................EAP 11-7

WING ANTI-ICING FAILURE ..........................EAP 11-8


SINGLE ENGINE BLEED OPERATION IN ICING CONDITIONS..................... refer to NAP-41


EAP 11-2 ORIGINAL


ICE COND-A/I INOP ........................................EAP 11-3

A/ICE LOW CAPACIT .....................................EAP 11-4

A/ICE SWITCH OFF ........................................EAP 11-4

AOA 1 (2) HEAT INOP ....................................EAP 11-4

E1 (2) A/ICE FAIL............................................EAP 11-5

ICE DET1 (2) FAIL...........................................EAP 11-5

ICE DETECTORS FAIL ...................................EAP 11-5

NO ICE-A/ICE ON............................................EAP 11-6

PITOT 1 (2, 3) INOP ........................................EAP 11-6

STAB A/ICE FAIL............................................EAP 11-8

TAT 1 (2) HEAT INOP .....................................EAP 11-7

W/S 1 (2) HEAT FAIL ......................................EAP 11-7

WG A/ICE FAIL ...............................................EAP 11-8


ORIGINAL EAP 11-3

ICING CONDITIONS WITH ANTI-ICING INOPERATIVE

EICAS Warning: ICE COND-A/I INOP

No

Yes

Thrust Levers .................................IDLE Ice Detection Override Knob.........AUTO Ice Detection Test Knob ................1, FOR 5 SECONDS,

THEN 2, FOR 5 SECONDS

No

Yes

No

Yes

TAKEOFF Procedure .....................ACCOMPLISH

Do not takeoff. Ice Detection Override Knob.........ALL Associated Failure Procedure ......ACCOMPLISH Icing Conditions .............................EXIT

END

END

END

ON GROUND?

ALL OPEN INSCRIPTIONS FLASH AT LEAST ONCE AND ICE DET 1 (OR 2) FAIL AND ICE CONDITION DISPLAYED?

ANTI-ICING SYSTEM EICAS MESSAGES DISAPPEAR WITHIN 60 SECONDS?


EAP 11-4 REVISION 4

ANTI-ICING LOW CAPACITY

EICAS Caution: A/ICE LOW CAPACIT

The following message will be displayed: EICAS Warning: ICE COND-A/INOP

The following messages may be displayed: EICAS Caution: WG A/ICE FAIL,

STAB A/ICE FAIL

Thrust Levers ................................... ADVANCE Advance Thrust Levers to at least 55% N1.

...................................................... WAIT 5 SECONDS No

Yes WING ANTI-ICING FAILURE OR

STABILIZER ANTI-ICING FAILURE Procedure (EAP 11-8).................. AS REQUIRED

ANTI-ICING SWITCH OFF

EICAS Caution: A/ICE SWITCH OFF

All Ice Protection Buttons ............... PUSH IN

AOA HEATING INOPERATIVE

EICAS Caution: AOA 1 (2) HEAT INOP

Minimum Airspeed ........................... FLAP MANEUVERING SPEED (PD-2)

END

END

MESSAGE PERSISTS?

END


ORIGINAL EAP 11-5

ENGINE ANTI-ICING FAILURE

EICAS Caution: E1 (2) A/ICE FAIL

Thrust Levers ........................................ADVANCE No

Yes

Ice Detection Override Knob................ALL

No

Yes

Ice Protection Engine Air Inlet .............PUSH OUT, THEN PUSH IN

No

Yes

Icing Conditions ....................................AVOID/EXIT Two minutes after exiting icing conditions:

Ice Detection Override Knob ...........AUTO

Engine Vibration....................................MONITOR If vibration increases, advance thrust levers one at a time, to 60% N1 minimum for 5 seconds. If vibration increases to unacceptable values or engine parameters indicate abnormal values, exit icing conditions.

ICE DETECTOR FAIL

EICAS Caution: ICE DET1 (2) FAIL or ICE DETECTORS FAIL

When flying in icing conditions: Ice Detection Override Knob ...........ALL

Two minutes after exiting icing conditions: Ice Detection Override Knob ...........AUTO

END

MESSAGE PERSISTS?



END


EAP 11-6 ORIGINAL

NO ICE - ANTI-ICE ON

EICAS Caution: NO ICE-A/ICE ON

Ice Detection Override Knob........... AUTO No

Yes

No

Yes


APU.................................................... START APU Bleed......................................... PUSH IN XBleed ............................................... OPEN Engine Bleeds .................................. PUSH OUT

Ice Protection Buttons..................... PUSH OUT

Operate the Anti-Icing Systems through the buttons, pushing them in again whenever icing conditions are encountered.

PITOT HEATING INOPERATIVE

EICAS Caution: PITOT 1 (2, 3) INOP

Instruments information supplied by the affected system may be unreliable. Cross-check and do not use the affected system if a disagreement is found. If the Pitot 3 heating is inoperative, standby instruments and pressurization system may be affected. If necessary:

ADC on Associated Reversionary Panel................. PUSH IN

END

MESSAGE PERSISTS?

ASSOCIATED TO EITHER WG A/ICE FAIL OR STAB A/ICE FAIL MESSAGE?

END

END



TAT HEATING INOPERATIVE

EICAS Caution: TAT 1 (2) HEAT INOP

Associated TAT, TAS and SAT indication may be unreliable.

WINDSHIELD HEATING FAILURE

EICAS Caution: W/S 1 (2) HEAT FAIL

Associated Ice Protection Windshield ................................... PUSH OUT

END

END


EAP 11-8 REVISION 4

WING ANTI-ICING FAILURE OR STABILIZER ANTI-ICING FAILURE

EICAS Caution: WG A/ICE FAIL or STAB A/ICE FAIL

Ice Detector Override Knob..................ALL Thrust Levers ........................................ADVANCE

No

Yes

Affected Ice Protection Button.............PUSH OUT, THEN PUSH IN

No

Yes

Associated Ice Protection Button........PUSH OUT Icing Conditions ....................................AVOID/EXIT Two minutes after exiting icing conditions: Ice Detector Override Knob .............AUTO Bank Angle ............................................MAX 30° Airspeed (Flaps 0° or 9°).......................MIN 190 KIAS

No

Yes

Stab

Wing or Wing+Stab

Landing configuration: Landing Gear ....................................DOWN Flaps ..................................................22° VREF.....................................................VREF45 + 30 KIAS




END

MESSAGE PERSISTS?


AFFECTED SYSTEM(S)?

LANDING IN ICING CONDITIONS OR WITH ICE ACCRETION?

END

EMERGENCY/ABNORMAL PROCEDURES Landing Gear & Brakes

ORIGINAL EAP 12-1

TABLE OF CONTENTS


LANDING GEAR/LEVER DISAGREE............... EAP 12-3

BRAKE OVERHEAT.......................................... EAP 12-4

BRAKES DEGRADED....................................... EAP 12-5

BRAKES INOPERATIVE................................... EAP 12-6

EMERGENCY/PARKING BRAKE LOW PRESSURE ......................................... EAP 12-7

LANDING GEAR AIR/GROUND SYSTEM FAILURE ....................................... EAP 12-8

NOSE LANDING GEAR UP DOOR OPEN ....... EAP 12-9

STEERING SYSTEM INOPERATIVE................ EAP 12-9

UNCOMMANDED SWERVING ON GROUND............................ EAP 12-9


ABNORMAL LANDING GEAR EXTENSION ..........................................refer to NAP-16

EMERGENCY/PARKING BRAKE HANDLE DISAGREE..............................refer to NAP-18

GEAR LEVER CANNOT MOVE UP AFTER TAKEOFF ..................................refer to NAP-27

PARTIAL OR GEAR UP LANDING........refer to NAP-38


EAP 12-2 ORIGINAL


LG/LEVER DISAGREE...................................... EAP 12-3

BRAKE DEGRADED......................................... EAP 12-5

BRAKE OVERHEAT.......................................... EAP 12-4

BRK INBD INOP................................................ EAP 12-6

BRK OUTBD INOP............................................ EAP 12-6

EMRG BRK LO PRES....................................... EAP 12-7

LG AIR/GND FAIL ............................................. EAP 12-8

NLG UP/DOOR OPN ......................................... EAP 12-9

STEER INOP ..................................................... EAP 12-9


REVISION 4 EAP 12-3

LANDING GEAR/LEVER DISAGREE

EICAS Warning: LG/LEVER DISAGREE EICAS Indication: Landing gear abnormal indication. Condition: Landing gear cannot move to desired

position.

The following message may be displayed:

EICAS Caution: NLG UP/DOOR OPN No

Yes

Consider to stop the airplane. Takeoff is not permitted.

Confirm the message on EICAS, check landing gear indication and, even if Landing Gear Indication shows three green lights:

Airspeed.................................................MAX 200 KIAS Landing Gear .........................................CYCLE

No

Yes Extended

Retracted

LAND AT THE NEAREST SUITABLE AIRPORT. Landing Gear Lever ..............................DOWN Airspeed.................................................MAX 250 KIAS Icing Conditions ....................................AVOID/EXIT Fuel Consumption.................................MONITOR

ABNORMAL LANDING GEAR EXTENSION Procedure (NAP-16)..........................ACCOMPLISH

END

END

LG/LEVER DISAGREE MESSAGE PERSISTS?

DESIRED LANDING GEAR POSITION?

END

ON GROUND?


EAP 12-4 ORIGINAL

BRAKE OVERHEAT EICAS Caution: BRAKE OVERHEAT

No

Yes

If necessary, reduce brake pressure. Use of full reverse thrust is recommended. Airplane..................................................STOP Chocks ...................................................ON Parking Brake ........................................RELEASE Airspeed.................................................MAX 250 KIAS Landing Gear Lever ..............................DOWN Brakes Temperature .............................CHECK IN THE

GREEN RANGE Airspeed.................................................MAX 200 KIAS Landing Gear Lever ..............................UP

END

END

ON GROUND?


ORIGINAL EAP 12-5

ICING CONDITIONS?

BRAKES DEGRADED EICAS Caution: BRAKE DEGRADED

During landing run: Brakes........................................... APPLY NORMALLY Use thrust reverser if available.

Brake effectiveness and symmetry may be affected.

Approach Configuration:

Yes

Landing configuration: Landing Gear ............................... DOWN Flaps ............................................. 22° VREF................................................ VREF45 + 10 KIAS

MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.71.


Landing Gear ............................... DOWN Flaps ............................................. 45° VREF................................................ VREF45

MULTIPLY THE FLAPS 45° UNFACTORED LANDING DISTANCE BY 1.20.

END

END

No


EAP 12-6 ORIGINAL

ICING CONDITIONS?

BRAKES INOPERATIVE EICAS Caution: BRK OUTBD (INBD) INOP

During landing run:

If available, use thrust reverser.

Both (OUTBD and INBD)

Only one (OUTBD or INBD)

Brakes ............................................... APPLY NORMALLY

No

Yes



Landing configuration: Landing Gear ....................................DOWN Flaps ..................................................45° VREF.....................................................VREF45


Emergency Brake Handle ................ PULL CAREFULLY

Relevant Inoperative Item: Anti-skid




END

BRAKES INOPERATIVE?

END

END

ICING CONDITIONS?

Yes

No


ORIGINAL EAP 12-7




EMERGENCY/PARKING BRAKE LOW PRESSURE

EICAS Caution: EMRG BRK LO PRES

Emergency/Parking Brake performance may be degraded. When parking the airplane, use wheel chocks.

END

END


EAP 12-8 REVISION 4

ICING CONDITIONS?

LANDING GEAR AIR/GROUND SYSTEM FAILURE

EICAS Caution: LG AIR/GND FAIL

Thrust Reversers and Ground Spoilers may not be available.

Depending on the failed condition, Ground Idle may not be selectable.

If the message is presented on ground, a loss of the main brake capacity may occur (below 10 kt ground speed) and steering may not be available.

Refer to the associated procedure for each case.

No

Yes

Anti-Icing System..................................MONITOR If any anti-ice valve does not open or anti-ice failure messages appear, leave and avoid icing conditions.

After exiting icing conditions, proceed as follows: Bank Angle........................................MAX 30° Airspeed for Flaps up or 9°..............MIN 190 KIAS



Icing Conditions ....................................AVOID



END

END



NOSE LANDING GEAR UP DOOR OPEN EICAS Caution: NLG UP/DOOR OPN EICAS Indication: Landing gear abnormal indication. Condition: Landing gear cannot move to desired

position.

The following message may be displayed: EICAS Warning: LG/LEVER DISAGREE

Confirm the message on EICAS, check landing gear indication and, even if Landing Gear Indication shows three green lights:

Airspeed.................................................MAX 200 KIAS Landing Gear .........................................CYCLE

No

Yes Extended

Retracted

LAND AT THE NEAREST SUITABLE AIRPORT. Landing Gear Lever ..............................DOWN Airspeed.................................................MAX 250 KIAS Icing Conditions ....................................AVOID/EXIT Fuel Consumption.................................MONITOR

ABNORMAL LANDING GEAR EXTENSION

Procedure (NAP-16)..........................ACCOMPLISH

STEERING SYSTEM INOPERATIVE OR UNCOMMANDED SWERVING ON GROUND EICAS Caution: STEER INOP may be displayed.

Steering Handwheel..............................DO NOT USE Steering Disengagement Button .........PRESS

Control the airplane using differential brakes and rudder. If serviceable, consider the use of differential thrust reverser.

END

END

LG/LEVER DISAGREE MESSAGE PERSISTS?

DESIRED LANDING GEAR POSITION?

END


EAP 12-10 ORIGINAL

INTENTIONALLY BLANK

EMERGENCY/ABNORMAL PROCEDURES Oxygen

ORIGINAL EAP 13-1

TABLE OF CONTENTS


CREW OXYGEN LOW PRESSURE...................EAP 13-3

PASSENGER OXYGEN LOW PRESSURE .......EAP 13-3


OXYGEN LEAKAGE ................................ refer to NAP-37


EAP 13-2 ORIGINAL


CREW OXY LO PRESS......................................EAP 13-3

PAX OXY LO PRESS .........................................EAP 13-3


ORIGINAL EAP 13-3

CREW OXYGEN LOW PRESSURE

EICAS Caution: CREW OXY LO PRESS

MFD Indication: Oxygen pressure red or amber.

Altitude.............................................. MEA OR 10’000 FT,

WHICHEVER IS HIGHER

PASSENGER OXYGEN LOW PRESSURE

EICAS Caution: PAX OXY LO PRESS

MFD Indication: Oxygen pressure red or amber.

Altitude.............................................. MEA OR 10’000 FT,

WHICHEVER IS HIGHER

END

END


EAP 13-4 ORIGINAL

INTENTIONALLY BLANK

EMERGENCY/ABNORMAL PROCEDURES Warning System

REVISION 9 EAP 14-1

TABLE OF CONTENTS


STALL PROTECTION INOPERATIVE.............. EAP 14-3

TAKEOFF CONFIGURATION WARNING ........ EAP 14-4

ADVANCED STALL PROTECTION.................. EAP 14-5

AURAL WARNING FAIL ................................... EAP 14-6

EGPWS INOPERATIVE..................................... EAP 14-6

STICK PUSHER FAILURE................................ EAP 14-7

WINDSHEAR DETECTION INOPERATIVE ...... EAP 14-8


AIRPLANE OVERSPEED.......................refer to NAP-4

ERRONEOUS STALL PROTECTION ACTUATION ......................................refer to NAP-26A


EAP 14-2 REVISION 4


SPS 1 (2) INOP.................................................. EAP 14-3

SPS 1-2 INOP .................................................... EAP 14-3

NO TAKEOFF CONFIG..................................... EAP 14-4

AURAL WARN FAIL.......................................... EAP 14-6

SPS ADVANCED............................................... EAP 14-5

STICK PUSHER FAIL........................................ EAP 14-7

TERR INOP........................................................ EAP 14-6

WINDSHEAR INOP ........................................... EAP 14-8


REVISION 4 EAP 14-3

STALL PROTECTION INOPERATIVE

EICAS Warning: SPS 1 (2) INOP or SPS 1-2 INOP

The following messages will be displayed: EICAS CAUTION: SPS ADVANCED STICK PUSHER FAIL

Affected Stall Protection Cutout Button ...................................PUSH OUT

Avoid skidding the airplane.

NOTE: - The remaining stick shaker is available. - Stick pusher is not available.

Yes

Add 15 KIAS to go-around speed. Landing configuration:






END

END

ICING CONDITIONS? No



TAKEOFF CONFIGURATION WARNING

EICAS Warning: NO TAKEOFF CONFIG Aural Warning: Voice Messages TAKEOFF-BRAKES,

TAKEOFF-FLAPS, TAKEOFF-TRIM, TAKEOFF-SPOILERS, TAKEOFF-FUEL

EICAS Indication: Spoiler and pitch trim may be red.

Do not takeoff.

Airplane Configuration .........................CORRECT

TO Config Button ..................................PRESS

END


REVISION 4 EAP 14-5

ADVANCED STALL PROTECTION

EICAS Caution: SPS ADVANCED

Above 25’000 ft: Minimum Airspeed ...........................150 KIAS

Below 25’000 ft: Minimum Airspeed ...........................FLAP

MANEUVERING SPEED (PD-2)

No

Yes Add 15 KIAS to go-around speed. Landing configuration:






END

ICING CONDITIONS?

END



AURAL WARNING FAIL

EICAS Caution: AURAL WARN FAIL

Visually monitor every EICAS, MFD and PFD indication specially related to TCAS, Windshear Detection, GPWS, IC-600, Fire Detection, Stall Protection, Trims, Flaps, Brakes, Spoilers, Radio Altimeter, Autopilot, Landing gear, ADC, Pressurization, SELCAL. No aural warning will be available. Do not perform CAT II or CAT III approaches.

EGPWS INOPERATIVE

EICAS Caution: TERR INOP, GPWS INOP, WINDSHEAR INOP

Monitor visually any trend toward terrain contact, excessive sink rate, marginal flight path and airplane configuration. No aural warning related to the system will be available.

END

END


REVISION 4 EAP 14-7

STICK PUSHER FAILURE

EICAS Caution: STICK PUSHER FAIL The following message will be displayed:

EICAS Warning: SPS 1-2 INOP

Control Column .....................................TOWARD NEUTRAL

Airspeed.................................................MIN FLAP MANEUVERING SPEED (PD-2)

No

Yes

JAMMED ELEVATOR Procedure (NAP-10)..........................ACCOMPLISH

Both stick shaker 1 and 2 are still available. No

Yes

Add 15 KIAS to go-around speed.


Landing gear .....................................DOWN

Flaps ..................................................22°

Airspeed ............................................VREF 45 + 15 KIAS


Add 5 KIAS to go-around speed.


Landing gear .....................................DOWN

Flaps ..................................................45°

Airspeed ............................................VREF 45 + 5 KIAS


STICK PUSHER JAMMED?

END

ICING CONDITIONS?

END

END


EAP 14-8 REVISION 4

WINDSHEAR DETECTION INOPERATIVE

EICAS Caution: WINDSHEAR INOP

Windshear detection is not available.

END

PERFORMANCE DATA ALL ENGINES

REVISION 5 PD-1

5 10 15 20 25 30 35 40 45 50

80 100

5 10 15 20 25 30 34 39 44 49

70 110

5 9 14 19 23 28 33 38 42 47

60 120

4 9 13 17 22 26 30 35 39 43

50 130

4 8 11 15 19 23 27 31 34 38

40 140

3 6 10 13 16 19 22 26 29 32

30 150

3 5 8 10 13 15 18 20 23 25

20 160

2 3 5 7 9 10 12 14 15 17

10 170

1 2 3 3 4 5 6 7 8 9

-5 -10

-15

-20

-25

-30

-34

-39

-44

-49

-5 -9 -14

-19

-23

-28

-33

-38

-42

-47

-4 -9 -13

-17

-22

-26

-30

-35

-39

-43

-4 -8 -11

-15

-19

-23

-27

-31

-34

-38

-3 -6 -10

-13

-16

-19

-22

-26

-29

-32

-3 -5 -8 -10

-13

-15

-18

-20

-23

-25

-2 -3 -5 -7 -9 -10

-12

-14

-15

-17

-1 -2 -3 -3 -4 -5 -6 -7 -8 -9

1 2 3 3 4 5 6 7 8 9

2 3 5 7 9 10 12 14 15 17

3 5 8 10 13 15 18 20 23 25

3 6 10 13 16 19 22 26 29 32

4 8 11 15 19 23 27 31 34 38

4 9 13 17 22 26 30 35 39 43

5 9 14 19 23 28 33 38 42 47

5 10 15 20 25 30 34 39 44 49

5 10 15 20 25 30 35 40 45 50

Exa

mpl

e: G

iven

Win

d S

peed

=20

kt

and

Ang

le (

betw

een

win

d an

d no

se)=

30°

, th

e H

eadw

ind

Com

pone

nt is

17

kt a

nd t

he C

ross

win

d co

mpo

nent

is 1

0 kt

.

WIN

D C

OM

PO

NE

NT

TA

BL

E

AN

GL

E B

ET

WE

EN

WIN

D D

IRE

CT

ION

AN

D H

EA

DIN

G (

LE

FT

OR

RIG

HT

)

170

HE

AD

WIN

D C

OM

PO

NE

NT

(kt

)C

RO

SS

WIN

D C

OM

PO

NE

NT

(kt

)

130

140

1020

3040

TA

ILW

IND

CO

MP

ON

EN

T (

kt)

5060

7015

016

080

100

110

120

MAXIMUM RECOMMENDED CROSSWIND

SURFACE CONDITION MAXIMUM

CROSSWIND

Dry 30 kt

Wet 25 kt

Contaminated by Compacted Snow 20 kt

Contaminated by Standing Water, Slush or Loose Snow

15 kt

Contaminated by Ice (no melting) 10 kt

PERFORMANCE DATA ALL ENGINES

PD-2 REVISION 7

PITCH TRIM UNITS

CG POSITION

(%)

LESS THAN OR

EQUAL TO 26.0

26.1 UP TO

28.5

28.6 UP TO

30.5

30.6 UP TO

33.5

ABOVE OR EQUAL TO

33.6

PITCH TRIM UNITS

8 7 6 5 4

FLAP RETRACTION SCHEDULE

For a flaps 9° takeoff: Flaps 9° to UP

V2 + 15 KIAS

FLAP MANEUVERING SPEED

GEAR/FLAP No Icing Conditions Icing Conditions

UP/0° 180 KIAS 200 KIAS

UP/9° 160 KIAS 160 KIAS

(DN/22°/45°) 140 KIAS 140 KIAS

PERFORMANCE DATA AE3007A1P ENGINES

REVISION 5 PD-2A

UNRELIABLE AIRSPEED (Climb)

Airplane: EMB-145 – Engine: AE3007A1P & A1E – Anti-Ice: OFF

WEIGHT (kg) PRESSURE ALTITUDE (ft)

14000 16000 18000 20000 22000 240000 Pitch (deg) 13 12 11 10 10 9

(240 KIAS) V/S (ft/min) 5018 4248 3656 3192 2818 2504 10000 Pitch (deg) 10 9 8 8 8 8



(0.65 M) V/S (ft/min) 1681 1358 1095 889 721 575 40000 Pitch (deg) 5 5 5 5 5 -

(0.65 M) V/S (ft/min) 785 583 402 201 38 -

UNRELIABLE AIRSPEED (Cruise)



14000 16000 18000 20000 22000 2400015000 Pitch (deg) 1 2 2 2 3 3

(250 KIAS) N1 (%) 68.0 68.9 69.7 70.6 71.4 72.2 20000 Pitch (deg) 1 2 2 2 3 3

(250 KIAS) N1 (%) 70.6 71.6 72.7 73.8 74.9 75.8 25000 Pitch (deg) 1 2 2 2 3 3

(250 KIAS) N1 (%) 73.9 75.2 76.5 77.8 79.0 80.0 30000 Pitch (deg) 2 2 2 3 3 4

(0.63 M) N1 (%) 76.2 77.7 79.1 80.2 81.3 82.5 35000 Pitch (deg) 2 3 3 4 4 5

(0.63 M) N1 (%) 77.2 78.5 80.0 81.4 83.4 85.7 40000 Pitch (deg) 3 4 5 5 6 6

(0.63 M) N1 (%) 79.5 81.3 83.9 87.6 90.9 92.3 45000 Pitch (deg) 5 5 6 6 7 7

(0.63 M) N1 (%) 83.6 88.2 92.2 92.2 92.2 92.2

UNRELIABLE AIRSPEED (Descent)



14000 16000 18000 20000 22000 240000 Pitch (deg) -3 -2 -1 -1 0 0

(240 KIAS) V/S (ft/min) -1756 -1649 -1572 -1504 -1445 -139810000 Pitch (deg) -3 -2 -1 -1 0 0

(240 KIAS) V/S (ft/min) -1828 -1709 -1619 -1547 -1483 -143220000 Pitch (deg) -6 -5 -5 -4 -4 -3



(0.78 M) V/S (ft/min) -1668 -1606 -1652 -1693 -1781 -1949


PD-2B REVISION 5

UNRELIABLE AIRSPEED (Holding)



14000 16000 18000 20000 22000 240005000 Pitch (deg) 3 3 4 5 5 6

(200 KIAS) N1 (%) 54.0 55.3 56.5 58.3 59.8 61.4 10000 Pitch (deg) 3 3 4 5 5 6

(200 KIAS) N1 (%) 57.6 58.9 60.2 62.0 63.6 65.2

UNRELIABLE AIRSPEED (Terminal Area)

Terminal Area (5000 ft) - %N1 for Level Flight


WEIGHT (kg) FLAP POSITION (VREF + INCREMENT)

14000 16000 18000 20000 22000 240000 Pitch (deg) 7 7 7 7 8 8

(VREF45 + 30) N1 (%) 47.2 50.2 53.1 55.8 58.3 60.6 9 Pitch (deg) 7 8 8 8 8 10

(VREF45 + 15) N1 (%) 50.7 54.2 57.3 60.2 63.1 71.5

UNRELIABLE AIRSPEED (Final Approach)

Final Approach (1500 ft) - %N1 for 3° Glideslope


WEIGHT (kg) FLAP POSITION (VREF + INCREMENT)

14000 16000 18000 20000 22000 2400022 Pitch (deg) 3 3 3 4 4 4

(VREF22 + 10) N1 (%) 45.8 48.7 51.5 54.1 56.4 58.7 45 Pitch (deg) 0 0 0 0 1 0

(VREF45 + 10) N1 (%) 59.0 62.2 65.3 68.2 70.6 72.9


ORIGINAL PD-3

TAKEOFF SPEEDS (Balanced Field Length)

V1/VR/V2 SPEEDS ALT T/O-1 MODE - FLAPS 9°

PRESSURE ALTITUDE

(ft)

STATIC AIR TEMPERATURE (C)

SL -40 to 47 48 to 50 1000 -40 to 45 46 to 48 2000 -40 to 41 42 to 46 3000 -40 to 38 39 to 44 4000 -40 to 33 34 to 41 42 to 42 5000 -40 to 29 30 to 37 38 to 40 6000 -40 to 18 19 to 30 31 to 38 7000 -40 to 23 24 to 36 8000 -40 to 9 10 to 29 30 to 348500 -40 to 25 26 to 32

WEIGHT (kg) V1 VR V2 V1 VR V2 V1 VR V2 V1 VR V2

12000 101 120 128 98 115 123 95 110 117 91 105 11212500 100 119 127 98 114 122 95 109 116 93 105 11213000 100 118 126 98 114 121 95 108 115 95 106 11213500 100 118 125 98 113 119 96 109 116 96 107 11314000 101 117 123 98 112 118 98 109 116 98 108 11414500 101 115 122 99 112 118 99 110 116 100 110 11515000 101 114 121 101 112 119 101 111 117 103 111 11715500 102 114 121 102 113 119 103 113 119 105 113 11816000 103 114 121 103 114 120 105 115 120 107 115 12016500 105 116 122 106 116 122 108 117 122 110 117 12217000 107 117 124 108 118 124 110 119 124 112 119 12417500 109 119 125 110 120 125 112 120 125 114 121 12518000 112 121 127 113 122 127 115 122 127 117 123 12718500 114 123 129 115 124 129 117 124 129 117 124 12819000 116 125 130 117 125 130 119 126 130 118 125 12819500 118 127 132 119 127 132 121 128 132 118 125 12820000 120 129 133 121 129 133 123 130 133 118 125 12820500 122 130 135 123 131 135 124 131 134 118 125 12821000 124 132 136 125 132 136 125 132 135 118 125 12821500 126 134 138 127 134 138 125 132 135 118 125 12822000 128 135 139 129 136 139 125 132 135 118 125 12822500 130 137 141 129 136 140 125 132 135 118 125 12823000 131 138 142 130 137 140 125 132 135 118 125 128


PD-4 ORIGINAL

TAKEOFF SPEEDS (Balanced Field Length)

V1/VR/V2 SPEEDS T/O MODE - FLAPS 9°

PRESSURE ALTITUDE

(ft)

STATIC AIR TEMPERATURE (C)

SL -40 to 39 40 to 46 47 to 50 1000 -40 to 37 38 to 43 44 to 48 2000 -40 to 33 34 to 40 41 to 46 3000 -40 to 35 36 to 44 4000 -40 to 31 32 to 40 41 to 42 5000 -40 to 27 28 to 35 36 to 40 6000 -40 to 28 29 to 38 7000 -40 to 21 22 to 36 8000 -40 to 11 12 to 32 33 to 348500 -40 to 2 3 to 28 29 to 32

WEIGHT (kg) V1 VR V2 V1 VR V2 V1 VR V2 V1 VR V2 V1 VR V2

12000 105 127 137 101 121 130 98 115 124 94 110 118 91 104 11212500 105 126 135 101 120 129 98 114 123 94 109 117 93 105 11213000 104 125 134 101 119 128 97 113 121 94 108 115 95 106 11313500 104 124 133 101 118 127 97 113 120 96 109 116 97 107 11414000 104 123 132 101 117 126 98 112 120 98 110 117 98 108 11514500 104 122 131 101 117 124 99 113 120 99 111 118 101 110 11615000 104 122 129 101 116 123 100 114 120 101 112 118 103 112 11715500 104 120 128 102 116 123 102 114 121 103 113 119 105 114 11816000 104 119 126 103 116 123 103 115 121 105 115 120 108 116 12016500 104 119 126 104 117 123 105 116 122 107 117 122 110 118 12217000 104 118 125 105 117 124 107 118 124 109 119 124 112 120 12417500 107 119 126 108 119 125 110 120 125 112 121 125 115 121 12518000 109 120 127 110 121 127 112 122 127 114 122 127 117 123 12718500 111 122 129 113 123 129 114 124 129 116 124 129 119 125 12819000 113 124 130 115 125 130 117 125 130 119 126 130 120 126 13019500 115 126 132 117 126 132 119 127 132 121 128 132 120 126 13020000 118 128 133 119 128 133 121 129 133 123 130 133 120 126 13020500 120 129 135 121 130 135 123 131 135 125 131 135 120 126 13021000 122 131 136 123 132 136 125 132 136 126 133 136 120 126 13021500 124 133 138 125 133 138 126 134 138 126 133 136 120 126 13022000 126 134 139 127 135 139 128 136 139 126 133 136 120 126 13022500 127 136 141 129 137 141 130 137 140 126 133 136 120 126 13023000 129 138 142 131 138 142 131 138 142 126 133 136 120 126 130


ORIGINAL PD-5

APPROACH CLIMB SPEED (VAPPCLB) &

REFERENCE SPEED (VREF) and FINAL SEGMENT SPEED (VFS)

Approach Flaps 9° Landing Flaps 22°

Approach Flaps 9° Landing Flaps 45°

Weight (kg)

VAPPCLB & VREF (KIAS)

VAPPCLB & VREF (KIAS)

VFS

(KIAS)

No ice encounter

After ice encounter

No ice encounter

After ice encounter

13000 116 116 118 118 135

13500 116 118 118 118 137

14000 116 120 118 118 140

14500 116 122 118 119 142

15000 116 124 118 120 144

15500 118 126 118 121 147

16000 120 128 119 123 149

16500 121 129 120 125 151

17000 123 131 121 127 153

17500 125 133 123 129 155

18000 126 134 124 131 157

18500 128 136 126 132 159

19000 130 138 128 134 161

19500 131 139 129 136 162

20000 133 141 131 138 164

20500 134 142 133 139 166

21000 136 144 134 141 168

21500 137 145 136 143 169

22000 139 147 137 144 171

22500 140 148 139 146 173

23000 142 150 141 148 174

APPROACH SPEED (VAPP)

VAPP = VREF + ½ steady headwind component + gust increment above steady wind.


PD-6 ORIGINAL

HOLDING - (All Engines)

CRUISE CONFIGURATION BLEED OPEN ANTI-ICE: OFF MINIMUM FUEL CONSUMPTION SPEED STANDARD ATMOSPHERE

0 5000 10000 15000 20000 25000 30000 35000 39000

IAS KT 180 182 182 183 185 185 188 189 -N1 % 56.5 60.3 64.2 68.0 71.7 76.0 80.5 84.8 -FF kg/H/ENG 489 469 452 441 436 435 442 455 -

IAS KT 175 178 179 179 181 181 183 185 187N1 % 55.3 59.2 63.1 67.0 70.6 74.8 79.4 83.6 90.4FF kg/H/ENG 471 451 434 422 416 414 420 431 454

IAS KT 171 173 175 174 176 177 179 180 182N1 % 54.2 58.0 61.9 65.8 69.5 73.6 78.2 82.4 89.0FF kg/H/ENG 454 433 417 404 397 394 398 408 428

IAS KT 167 168 171 170 171 173 174 176 177N1 % 53.1 56.7 60.7 64.6 68.4 72.3 76.8 81.2 87.4FF kg/H/ENG 438 416 400 386 378 375 376 385 403

IAS KT 163 163 166 166 167 169 169 171 172N1 % 51.9 55.4 59.4 63.3 67.1 71.0 75.5 80.0 85.8FF kg/H/ENG 421 399 382 368 359 355 356 363 378

IAS KT 158 159 161 162 162 164 164 167 167N1 % 50.6 54.1 58.0 62.1 65.9 69.7 74.1 78.7 84.2FF kg/H/ENG 404 382 365 351 341 336 335 341 354

IAS KT 154 154 156 158 157 159 160 161 162N1 % 49.2 52.8 56.6 60.6 64.6 68.3 72.5 77.3 82.8FF kg/H/ENG 388 365 347 334 323 317 315 319 330

IAS KT 150 149 150 153 152 153 155 156 157N1 % 47.9 51.4 55.0 59.1 63.1 66.9 71.0 75.7 81.4FF kg/H/ENG 371 349 330 316 305 298 296 297 308

IAS KT 146 145 145 147 148 148 150 150 152N1 % 46.5 49.9 53.5 57.4 61.5 65.4 69.4 73.9 79.7FF kg/H/ENG 355 332 313 299 288 280 277 277 285

IAS KT 141 140 140 141 143 143 144 145 146N1 % 45.0 48.3 51.9 55.8 59.9 63.9 67.7 72.2 78.0FF kg/H/ENG 339 316 297 282 270 262 257 257 263

17000

16000

15000

14000

21000

20000

19000

18000

ALTITUDE (FT)WEIGHT(kg)

23000

22000


ORIGINAL PD-7

HOLDING - (All Engines)

CRUISE CONFIGURATION, BLEED OPEN, AIRSPEED: 1.3 VS OR 200 KIAS WHICHEVER IS HIGHER ANTI-ICE: ON (NO ICE ACCRETION) STANDARD ATMOSPHERE

0 5000 10000 15000 20000 25000 30000 35000 39000

IAS KT 200 200 200 200 200 200 200 200 -N1 % 57.5 61.2 65.0 68.7 72.2 76.5 80.8 85.0 -FF kg/H/ENG 506 484 467 455 449 448 453 465 -

IAS KT 200 200 200 200 200 200 200 200 -N1 % 56.7 60.4 64.2 67.9 71.4 75.6 80.0 83.9 -FF kg/H/ENG 494 472 454 442 434 432 436 447 -

IAS KT 200 200 200 200 200 200 200 200 -N1 % 56.0 59.5 63.4 67.2 70.6 74.6 79.1 83.0 -FF kg/H/ENG 482 460 442 429 421 418 420 429 -

IAS KT 200 200 200 200 200 200 200 200 -N1 % 55.3 58.7 62.6 66.5 69.9 73.7 78.2 82.1 -FF kg/H/ENG 471 449 430 417 408 404 405 413 -

IAS KT 200 200 200 200 200 200 200 200 -N1 % 54.5 57.9 61.9 65.8 69.2 72.8 77.3 81.3 -FF kg/H/ENG 461 438 419 405 396 391 391 397 -

IAS KT 200 200 200 200 200 200 200 200 200N1 % 53.8 57.2 61.1 65.0 68.5 72.0 76.3 80.5 85.7FF kg/H/ENG 451 428 409 394 384 378 378 383 397

IAS KT 200 200 200 200 200 200 200 200 200N1 % 53.1 56.5 60.3 64.2 67.8 71.3 75.4 79.7 84.7FF kg/H/ENG 442 418 399 384 373 367 365 369 382

IAS KT 200 200 200 200 200 200 200 200 200N1 % 52.4 55.8 59.5 63.5 67.1 70.5 74.6 78.9 83.9FF kg/H/ENG 433 409 390 374 363 356 354 356 368

IAS KT 200 200 200 200 200 200 200 200 200N1 % 51.7 55.2 58.8 62.8 66.5 69.9 73.7 78.2 83.2FF kg/H/ENG 425 401 381 365 354 346 343 344 355

IAS KT 200 200 200 200 200 200 200 200 200N1 % 51.2 54.5 58.1 62.2 65.9 69.2 72.9 77.5 82.4FF kg/H/ENG 417 393 373 357 345 337 333 333 343

17000

16000

15000

14000

21000

20000

19000

18000

WEIGHT(kg)

ALTITUDE (FT)

23000

22000


PD-8 ORIGINAL

DRIFTDOWN TABLE

ANTI-ICE OFF

WEIGHT INITIAL GROSS LEVEL OFF ALTITUDE - FT

(KG) DRIFTDOWN (NET LEVEL OFF ALTITUDE - FT)

START LEVEL SPEED

DRIFTDOWN OFF (KIAS) ISA ISA + 10 ISA + 20

21825 21683 21093 22000 21020 171

(16578) (16379) (16026)

23477 23319 22558 21000 20099 168

(18627) (18368) 17978

24877 24777 23867 20000 19160 164

(20375) (20224) (19722)

26285 26174 25092 19000 18262 161

(21809) (21670) (21086)

27952 27861 26530 18000 17320 157

(23442) (23327) (22581)

29872 29701 28015 17000 16348 153

(25146) (25038) (24086)

31969 31629 29461 16000 15401 149

(26870) (26777) (25588)

33540 33280 30994 15000 14461 144

(28782) (28646) (27181)


ORIGINAL PD-9

UNFACTORED LANDING DISTANCE

UNFACTORED LANDING DISTANCE (METERS) EMB-135BJ - FLAPS 45o

NO ICE ENCOUNTER ISA CONDITIONS - SLOPE 0%

ALTITUDE WEIGHT 0 ft 1000 ft

(kg) WIND WIND -10 kt 0 kt 10 kt 20 kt -10 kt 0 kt 10 kt 20 kt

13000 861 732 692 653 878 748 707 667 14000 857 729 689 650 874 745 704 665 15000 855 727 687 648 872 742 702 662 16000 869 740 700 660 887 756 715 675 17000 905 773 731 691 924 790 748 707 18000 942 806 764 722 962 824 781 739 19000 979 840 796 754 1000 859 815 772 20000 1019 876 831 788 1041 896 851 806

ALTITUDE

WEIGHT 2000 ft 3000 ft


13000 895 764 722 682 914 780 739 698 14000 892 761 720 680 910 777 736 695 15000 889 758 717 677 907 775 733 693 16000 905 772 731 690 923 789 747 706 17000 943 807 764 723 963 825 782 740 18000 982 843 799 757 1004 862 818 775 19000 1022 879 834 790 1045 899 854 810 20000 1064 917 871 826 1088 939 892 847

ALTITUDE

WEIGHT 4000 ft 5000 ft


13000 933 798 755 714 953 816 773 732 14000 929 795 752 711 949 813 770 729 15000 926 792 750 709 946 810 768 726 16000 943 807 764 723 963 826 782 740 17000 984 844 800 758 1006 864 820 777 18000 1026 883 838 794 1049 904 858 814 19000 1068 921 875 830 1093 944 897 851 20000 1113 962 914 868 1140 986 937 891


PD-10 ORIGINAL

UNFACTORED LANDING DISTANCE

UNFACTORED LANDING DISTANCE (METERS) EMB-135BJ - FLAPS 45o

NO ICE ENCOUNTER ISA CONDITIONS - SLOPE 0%

ALTITUDE WEIGHT 6000 ft 7000 ft


13000 974 835 792 749 996 855 811 768 14000 970 832 788 746 992 852 807 765 15000 967 829 786 744 989 849 805 762 16000 985 845 801 759 1007 865 821 778 17000 1028 885 840 796 1052 906 860 816 18000 1074 926 879 834 1099 949 902 856 19000 1119 967 919 873 1146 991 943 896 20000 1167 1011 961 914 1195 1036 987 938

ALTITUDE

WEIGHT 8000 ft

(kg) WIND -10 kt 0 kt 10 kt 20 kt

13000 1018 875 831 787 14000 1014 872 827 784 15000 1011 869 825 781 16000 1030 886 841 797 17000 1077 929 882 837 18000 1125 973 925 878 19000 1174 1017 968 920 20000 1225 1063 1013 963


REVISION 7 PD-11

EMB-135BJ UNFACTORED LANDING DISTANCES -

CONTAMINATED RUNWAYS (m)

ALL ENGINES TYPES – EASA CERTIFICATION

STANDING WATER 4 mm/SLUSH 4 mm

WET SNOW 8 mm/DRY SNOW 32 mm

WEIGHT (kg) FLAP 22° FLAP 45°

13000 1857 1606 13500 1920 1623 14000 1982 1640 14500 2044 1657 15000 2106 1674 15500 2169 1723 16000 2232 1772 16500 2296 1821 17000 2359 1870 17500 2427 1923 18000 2493 1975 18500 2560 2028 19000 2626 2081 19500 2696 2138 20000 2766 2194 20500 2836 2251 21000 2906 2308 21500 2975 2364 22000 3043 2420 22500 3112 2475

CORRECTIONS

ALTITUDE LANDING DISTANCE + 4% per 1000 ft above sea level (Altitude correction limited up to 10000 ft above sea level).

WIND LANDING DISTANCE + 9% per 5 kt tailwind.

OVERSPEED LANDING DISTANCE + 9% per 5 kt above VREF.

TEMPERATURE LANDING DISTANCE + 2% per 5ºC above ISA.

SLOPE LANDING DISTANCE + 8% per 1% slope downhill.


PD-12 REVISION 7







13000 1650 1466 13500 1703 1481 14000 1755 1496 14500 1808 1510 15000 1860 1525 15500 1914 1568 16000 1968 1612 16500 2021 1655 17000 2075 1698 17500 2132 1744 18000 2189 1791 18500 2247 1838 19000 2304 1885 19500 2364 1936 20000 2424 1986 20500 2484 2037 21000 2544 2087 21500 2604 2138 22000 2664 2188 22500 2724 2238

CORRECTIONS







REVISION 7 PD-13







13000 1529 1379 13500 1576 1393 14000 1623 1407 14500 1670 1420 15000 1718 1434 15500 1766 1474 16000 1814 1513 16500 1862 1553 17000 1911 1592 17500 1963 1635 18000 2014 1678 18500 2065 1721 19000 2117 1764 19500 2171 1810 20000 2225 1857 20500 2279 1903 21000 2334 1950 21500 2388 1996 22000 2441 2042 22500 2495 2089

CORRECTIONS







PD-14 REVISION 7




COMPACTED SNOW


13000 1270 1263 13500 1302 1270 14000 1335 1277 14500 1367 1284 15000 1400 1290 15500 1429 1321 16000 1459 1351 16500 1489 1381 17000 1518 1411 17500 1548 1441 18000 1578 1472 18500 1608 1503 19000 1637 1533 19500 1666 1563 20000 1694 1593 20500 1723 1622 21000 1751 1652 21500 1780 1682 22000 1808 1712 22500 1837 1742

CORRECTIONS







REVISION 7 PD-15




ICE


13000 3119 3061 13500 3119 3055 14000 3118 3050 14500 3118 3044 15000 3118 3039 15500 3136 3069 16000 3155 3100 16500 3174 3130 17000 3192 3161 17500 3235 3204 18000 3277 3248 18500 3320 3291 19000 3362 3334 19500 3405 3380 20000 3447 3426 20500 3490 3472 21000 3533 3519 21500 3575 3565 22000 3618 3611 22500 3660 3657

CORRECTIONS







PD-16 REVISION 7

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EMERGENCY/ABNORMAL PROCEDURES Appendix

ORIGINAL APP-1

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H-1

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INTENTIONALLY BLANK

EMERGENCY/ABNORMAL PROCEDURES Appendix

APP-2 REVISION 4

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Parking Brake ................................ APPLY

Cabin .............................................. DEPRESSURIZE

Fire Extinguishing Handles .......... PULL

APU Fuel Shutoff Valve ................ PUSH IN

Fuel Pumps Pwr 1 and 2 ............... OFF

Hydraulic Elec Pumps 1 and 2 .... OFF

Engines and APU Fire Extinguishing Bottles (if necessary).............. DISCHARGE

Cabin Crew..................................... NOTIFY

Emerg Lts....................................... ON

Evacuation ..................................... INITIATE

ATC.................................................. NOTIFY Before leaving the airplane: Batteries 1 and 2........................ OFF

END

EASA/JAA QUICK REFERENCE HANDBOOK

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