Quick Reference Handbook - Aviation For All · ERJ-170 QRH Original 29AUG2005 i ERJ-170 ERJ-170 QRH...

ERJ-170ERJ-170 QRH Bulletins

No. Subject See Page 05-01 NEW EICAS MESSAGE Bleed (1 or 2) Overpress 78 07-01 Passenger Oxygen Selector xviii

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List of Effective Pages:i-xxxiv Dated 29AUG20051-94 Dated 29AUG2005

ERJ-170 QRH Original 29AUG2005 i

ii

Refer to last page for Evacuation Duties

EVACUATION When the aircraft is below 1000 feet AGL, the captain will make a PA announcement “BRACE, BRACE”. this will alert flight attendants and passengers to assume brace position.Time permitting, position the aircraft relative to the wind to prevent fire from enveloping escape routes. Unlock the cockpit door.

Captain:1.Parking Brake .................................................ON2.Thrust Levers............................................... IDLE3.START/STOP 1 & 2................................... STOP4.Evacuation Command..............................Initiate

• Initiate the evacuation by using the passenger address system. “Evacuate, Evacuate”.

5.Captain Evacuation Checklist complete.

First Officer:1.ATC .............................................................Notify2.Fire Handles....PULL and ROTATE (1L and 2R)3.APU EMER STOP...................................PUSH IN4.APU FIRE EXTINGUISHER ...................PUSH IN5.PRESSURIZATION DUMP.....................PUSH IN6.First Officer Evacuation Checklist complete.

As the last step before leaving the cockpit:1.Batteries...................................................... OFF

• The last crewmember leaving the flight deck will turn the batteries off.

Original 29AUG2005 ERJ-170 QRH

ENGINE ABNORMAL START

1.#___START/STOP ....................................................STOP2.If engine dry motoring is considered:

a.Associated engine:(1)IGNITION.............................................OFF(2)START/STOP .................START then RUN

After 30 seconds:(3)START/STOP ................................... STOP(4)IGNITION.......................................... AUTO

3.Engine Abnormal Start Checklist complete.

ERJ-170 QRH Original 29AUG2005 iii

iv

DUAL ENGINE FAILURECondition:Unexpected dual engine shutdown occurred. FAIL

icon on N1 gauge and oil pressure in red zone.

1.Airspeed..........................................250 KIAS MIN2.RAT MANUAL DEPLOY Lever.................... PULL3.Land at nearest suitable airport.4.APU (if available)....................................START5.EMER LT .........................................................OFF6.Thrust Levers ................................................ IDLE7. If one or both engines autorelight:

a.FLIGHT CONTROL MODE (all) ...........................................PUSH IN then OUT(ELEVATORS, RUDDER, SPOILERS)

b.Dual Engine Failure Checklist complete, and* Establish and communicate a plan.* Accomplish “RAT” Deployed Descent

Checklist” and “RAT Deployed Landing Checklist”, page 21.

If at least one engine does not autorelight:a.FUEL XFEED.........................................LOW 1b.START/STOP 1 & 2................................. STOPc. IGNITION 1 & 2.......................................OVRDd.START/STOP 1 & 2...............START then RUN

Cont’d

or


DUAL ENGINE FAILURE (cont.)e. If restart is successful on at least one

engine:(1)FLIGHT CONTROL MODE (all) .. PUSH IN

then OUT(ELEVATORS, RUDDER, SPOILERS)

After engine(s) stabilized at idle:(2)IGNITION 1 & 2 ................................ AUTO(3)Fuel................................................Balance(4)Dual Engine Failure Checklist complete,

and* Establish and communicate a plan.* Accomplish “RAT Deployed Descent

Checklist” and “RAT Deployed Landing Checklist”, page 21.

If repeated restarts are not successful:(1)Airspeed .................... Reduce to green dot(2)Dual Engine Failure Checklist complete,

and* Establish and communicate a plan.* Accomplish “Dual Engine Failure

Descent Checklist” and “Dual Engine Failure Landing Checklist”, page 22.

* This is an NTSB Reportable Event

or

ERJ-170 QRH Original 29AUG2005 v

v

ENGINE FIRE (1 or 2), SEVERE DAMAGE OR SEPARATION

1.Autothrottles .......................................Disengage2.#__ Thrust Lever ....... Confirm ..................... IDLE3.#__ START/STOP ...... Confirm ................... STOP4.#__ Fire Handle ......... Confirm ....................PULL5.#__ Fire Handle ......... Confirm ...............ROTATE

......................................... .................(left or right)Wait 30 seconds.

6.If ENG (1 or 2) FIRE message persists:a.Fire Handle...........Rotate to remaining bottle

7. If there is severe damage or separation:a.Airspeed.................................. 200 KIAS MAXb.Altitude.......... 18,000 ft. max. or safe altitude

(whichever is higher)c. Go to Step 8.If there is not severe damage or separation:a.Go to Step 8.

8.APU (if available)....................................... START9.FUEL......................................................... Balance10.Land at the nearest suitable airport.11.ENG (1 or 2) FIRE, Severe Damage or

Separation Checklist complete, and* Establish and communicate a plan.* If required, accomplish:

• “Driftdown Table”, page 29.• Applicable After Takeoff Checklist items.• “Engine Out Descent Checklist” and “Engine Out

Landing Checklist”, page 25.* This is an NTSB Reportable Event

or

Original 29AUG2005 ERJ-170 QRHi

APU FIRE1.APU EMER STOP .................................. PUSH IN2.APU MASTER ................................................OFF

Note:The message APU FIRE DET FAIL may appear just before the APU FIRE message.

3. If the APU FIRE remains annunciated:a.APU FIRE EXTINGUISHER............... PUSH INb.Land at the nearest suitable airport.c. APU FIRE Checklist complete, and

* Establish and communicate a plan.* This is an NTSB Reportable Event

If the APU FIRE does not remain annunciated:a.Land at the nearest suitable airport.b.APU FIRE Checklist complete, and

* Establish and communicate a plan.* This is an NTSB Reportable Event

BATT (1 or 2) OVERTEMPEICAS Indication: Battery temperature indication in red band.

1.Associated BATT 1 or BATT 2.......................OFF2.APU ....................................................Do not start3.BATT (1 or 2) OVERTEMP Checklist complete.

or

ERJ-170 QRH Original 29AUG2005 vii

v

AIR CONDITIONING SMOKE

1.Oxygen Masks............. Verify ............... ON, EMER2.Crew Communication ...........................Establish3.Cockpit Door ............................................... Close

4.Land at the nearest suitable airport.5.RECIRC ............................................... PUSH OUT6. If smoke stops:

a. If smoke/fumes removal is required, accomplish “Smoke Evacuation Checklist”, page xiii.

If smoke does not stop:a. PACK 1.......................................... PUSH OUTb. If smoke stops:

(1)BLEED 1.................................. PUSH OUT(2)Altitude................................. 31,000 ft. max(3)If smoke/fumes removal is required,

accomplish “Smoke Evacuation Checklist”, page xiii.

If smoke does not stop:(1)PACK 1 ........................................ PUSH IN(2)PACK 2 .................................... PUSH OUT(3)BLEED 2.................................. PUSH OUT(4)Altitude................................. 31,000 ft. max(5)If smoke/fumes removal is required,

Accomplish “Smoke Evacuation Checklist”, page xiii.

Do not activate the PASSENGER OXY-GEN MASK DEPLOY knob.

or

or

Original 29AUG2005 ERJ-170 QRHiii

ELECTRICAL SYSTEM FIRE OR SMOKE

1.Oxygen Masks............. Verify ............... ON, EMER2.Crew Communication ...........................Establish3.Cockpit Door ............................................... Close

4.Land at the nearest suitable airport.5.RECIRC ............................................... PUSH OUT6. If fire or smoke origin is identified:

a.Electrical power (affected equipment) ..Remove(1)If practical, remove power from affected

equipment by push button, knob, or circuit breaker.

(2)If smoke/fumes removal is required, accomplish “Smoke Evacuation Checklist”, page xiii.

If fire or smoke origin is not identified:a.EMER LT....................................................OFFb.RAT Manual Deploy Lever .......................PULLc. Airspeed ..................................... 130 KIAS MINd.Altitude ...................... 10,000 ft. or safe altitude

(whichever is higher)e. IDG 1..........................................................OFFf. IDG 2..........................................................OFFg.APU (if operating).......................................OFF

Note:Do not accomplish ELEC EMERGENCY procedure.

h.If BATT DISCHARGING message annunciated:(1)IDG 1 or IDG 2.................................. AUTO

Cont’d

Do not activate the PASSENGER OXY-GEN MASK DEPLOY knob.

or

ERJ-170 QRH Original 29AUG2005 ix

x

ELECTRICAL SYSTEM FIRE OR SMOKE (Cont.)

i. If smoke stops and/or landing can be accomplished within 30 minutes, and if smoke/ fumes removal is requi red , accomplish “Smoke Evacuation Checklist” page xiii.

j. Icing Conditions........................................ Avoidk. Autothrottles .....................................Disengagel. IDG 1....................................................... AUTOm.IDG 2 ...................................................... AUTOn.DC BUS TIES.............................................OFFo.TRU 1.........................................................OFFp.BATT 1 .......................................................OFF

Note:DC ESS BUS 1 and DC BUS 1 are deenergized.

q. If smoke stops:(1)If smoke/fumes removal is required,


If smoke does not stop:(1)BATT 1...................................................ON(2)TRU 1 ............................................... AUTO(3)TRU 2 ..................................................OFF(4)BATT 2................................................ OFF

Note:DC ESS BUS 2 and DC BUS 2 are deenergized.

(5) If smoke stops:(a)If smoke/fumes removal is required,


If smoke does not stop:(a)BATT 2....................................... AUTO(b)TRU 2 ........................................ AUTO(c)TRU ESS ......................................OFF

Note:DC ESS BUS 3 is deenergized.

Cont’d

or

or


ELECTRICAL SYSTEM FIRE OR SMOKE (Cont.)

(d) If smoke stops:i) If smoke/fumes removal is

required, accomplish “Smoke Evacuation Checklist”, page xiii.

If smoke does not stop:i) TRU ESS ........................... AUTOii) DC BUS TIES .................... AUTO

7. If smoke/fumes removal is required, accomplish “Smoke Evacuation Checklist”, page xiii.If smoke / fumes removal is not required:a.Electrical System Fire or Smoke Checklist

complete, and* Establish and communicate a plan.* If RAT is deployed, accomplish ”Smoke/

Fumes Descent Checklist”, and “Smoke/Fumes Landing Checklist”, page 72.


or

or

ERJ-170 QRH Original 29AUG2005 xi

x

CARGO FORWARD (AFT) SMOKECondition: Associated CARGO SMOKE (FWD or AFT) Fire

Extinguisher push button illuminates.

1.Associated Cargo Fire Extinguisher Button..........................................PUSH

1. On ground:a. If cargo door is open:

(1) Do not discharge the cargo fire extinguisher.(2) Notify ground personnel to investigate the

source of the smoke/fire.(3) CARGO FORWARD (AFT) SMOKE Checklist

complete, and* If required, accomplish “Evacuation,” page

ii.If cargo door is closed:(1) CARGO SMOKE FWD or (AFT) ............ PUSH(2) Notify fire department and appropriate ground

personnel,(3) CARGO FORWARD (AFT) SMOKE Checklist

complete, and* If required, accomplish “Evacuation,” page

ii.In flight:a. CARGO SMOKE (FWD or AFT) ................... PUSHb. Land at the nearest suitable airport.

(1) Confirm the CRG AFT (FWD) FIREX HI ARM message extinguishes and the CRG AFT (FWD) FIREX LO ARM message is displayed.

(2) After 1 minute, confirm the CRG AFT (FWD)FIREX LO ARM message and the cargo fire extinguishing button light extinguish.

c. CARGO FORWARD (AFT) SMOKE Checklist complete, and* Establish and communicate a plan.* If required, accomplish “Smoke Evacuation

Checklist”, page xiii.* If extinguishing agent has been discharged,

notify ground personnel prior to their opening the cargo door.

Do not Discharge the cargo fire extin-guisher on the ground with the cargo door open.

or

or

Original 29AUG2005 ERJ-170 QRHii

SMOKE EVACUATION

1.Oxygen Masks............. Verify ............... ON, EMER2.Crew Communication ...........................Establish3.Pressurization Dump Button ................ PUSH IN4.Emergency Decent (if required)............ Initiate5.Land at the nearest suitable airport.6.When smoke / fumes are cleared:

a.PRESSURIZATION DUMP ............ PUSH OUT7.Smoke Evacuation Checklist complete, and

* Establish and communicate a plan.* If RAT is deployed, accomplish accomplish

”Smoke/Fumes Descent Checklist”, and “Smoke/Fumes Landing Checklist”, page 72.

ERJ-170 QRH Original 29AUG2005 xiii

x

JAMMED CONTROL COLUMN - PITCH

1.ELEVATOR DISCONNECT Handle ..............PULL2.Unrestricted Control Column................. Identify

Identify which side is not jammed by separately moving each column.

3.Autopilot ....................................... Do not engage4.Airspeed..............................................As follows:

5.Considerations:• Expect lower pitch rates and authority• Avoid side slipping the aircraft.• The stick shaker remains operative.

6.Jammed Control Column - Pitch Checklist complete, and* Establish and communicate a plan.* Accomplish “Pitch/Roll Malfunction Descent

Checklist” and “Pitch/Roll Malfunction Landing Checklist”, page 46.


:

If the failure occurs ___ 175 KIAS...

Then maximum airspeed is...

above the current airspeedat or below 175 KIAS

Original 29AUG2005 ERJ-170 QRHiv

JAMMED CONTROL WHEEL - ROLL

1.AILERON DISCONNECT Handle .................PULL2.Unrestricted Control Wheel .................... Identify• Identify which side is not jammed by separately

moving each control wheel.4.Autopilot .......................................Do not engage5.Airspeed..............................................As follows:

6.SPOILER FAULT Procedure .Do not accomplish7.The following components are inoperative:

8.Considerations:• Expect lower roll rates.-• Avoid side slipping the aircraft.• Avoid abrupt and large aileron inputs. • Maintain bank angle below 25°.• Rudder may be used to help in controlling the

aircraft.9.Jammed Control Wheel - Roll

Checklist complete, and* Establish and communicate a plan.* Accomplish “Pitch/Roll Malfunction Descent

Checklist” and “Pitch/Roll Malfunction Landing Checklist”, page 46.


If the failure occurs ___ 175 KIAS...

Then maximum airspeed is...

above the current airspeedat or below 175 KIAS

Affected Side AileronMulti Function Spoiler L3 and R3

Another Multi Function Spoiler Pair depending on the affected side

ERJ-170 QRH Original 29AUG2005 xv

x

PITCH TRIM RUNAWAY

1.AP/TRIM DISC Button ............ PRESS and HOLD2.PITCH TRIM SYS 1 & 2

CUTOUT Button ..................................... PUSH IN3.AP/TRIM DISC...................................... .RELEASE

Prepare to overcome unwanted pitch change:4.PITCH TRIM SYS 1 CUTOUT ............. PUSH OUT

a.Pitch Trim Switch ...............................Actuate5. If Pitch Trim normal:

a.Continue using PITCH TRIM SYS 1 only.b.PITCH TRIM Runaway Checklist complete.If Pitch Trim not normal:a.PITCH TRIM SYS 1 CUTOUT ........... PUSH INb.PITCH TRIM SYS 2 CUTOUT ....... PUSH OUTc. If Pitch Trim normal:

(1)PITCH TRIM Runaway Checklist complete.If Pitch Trim not normal:(1)PITCH TRIM SYS 2 CUTOUT..... PUSH IN(2)PITCH TRIM Runaway Checklist complete.

* Establish and communicate a plan.* Accomplish “Pitch Trim Fail Checklist”,

page 40.* This is an NTSB Reportable Event

Do not open the Speed Brake

or

or

Original 29AUG2005 ERJ-170 QRHvi

ROLL (YAW) TRIM RUNAWAY

1.AP/TRIM DISC Button ............ PRESS and HOLDPrepare to overcome unexpected (ROLL or YAW):2.AP/TRIM DISC.......................................... Release3. If (ROLL or YAW) TRIM normal:

a.Autopilot ..............................Do not reengageb.(ROLL or YAW) TRIM Runaway Checklist

complete.If (ROLL or YAW) TRIM not normal:a.AP/TRIM DISC................... PRESS and HOLDb.(ROLL or YAW) TRIM Electronic CB .......OFF

Turn OFF the (ROLL or YAW) TRIM electronic circuit breakers on the respective MCDU page. (Select on the MCDU: CB > CBMENU > CB BY SYSTEM > NEXT > FLT > CTRL > ROLL TRIM PWR or YAW TRIM PWR)

c.AP/TRIM DISC.................................... Released.Autopilot .................................Do not engagee. (ROLL or YAW) TRIM Runaway Checklist

complete.* This is an NTSB Reportable Event

STEERING RUNAWAY

1.STEER DISC SWITCH ...............................PRESS2.Steer the airplane using differential braking and

rudder.3.Steering Runaway Checklist complete.

or

ERJ-170 QRH Original 29AUG2005 xvii

x

CABIN ALTITUDE HI

Condition:Cabin altitude indicating red and exceeded 10,000 ft.1.Oxygen Masks........... Verify ................ ON, 100%2.Crew Communication .......................... Establish3.Altitude..................................................................

.............. 10,000 ft or MEA (whichever is higher)4.Thrust Levers ............................................... IDLE5.SPEED BRAKE Lever ......................FULL OPEN6.Airspeed............................. MAX/APPROPRIATE7.Transponder ................................................. 77008.ATC...........................................................NOTIFY9. If the PAX OXY NOT DEPLOYED message is

presented:a.Passenger oxygen selector..................OVRD

10.Autopilot (if available) ...................................ON11.NO PED/FSTN BELTS.....................................ON12.Cabin PA ..............................................Complete

Announce “Emergency Descent” using the cabin PA system to alert the flight attendants so they may prepare the cabin.

13.Cabin Altitude........................................MonitorWhen cabin altitude is 14,000 ft. or below:14.Audio Control Panel .................................EMER

Activates the emergency call signal, sounds a triple chime and illuminates a red light in the cabin. The flight crew will establish communication with the flight attendants.

15.Flight Attendants ........................ Notify and obtain status report

When approximately 1,000 ft. above desired altitude:16.SPEED BRAKE Lever ......................... CLOSE17.Speed .............................Adjust as necessary18.Crew O2 (if required)........................... Normal

Flight crew must use oxygen when cabin altitude is above 10,000 ft. To conserve oxygen, position the mask selector to NORM.

19.CABIN ALTITUDE HI Checklist complete, and* Establish and communicate a plan.* If structural damage suspected, accomplish

“Structural Damage Checklist”, page 2.

9. Passenger Oxygen Selector.............. OVRD

Original 29AUG2005 ERJ-170 QRHviii

EMERGENCY DESCENT

1.Seat Belts...................................................... ON2.Altitude. 10,000 ft or MEA whichever is higher3.Thrust Levers ............................................ IDLE4.Speed Brake Lever........................ FULL OPEN5.Airspeed...........................MAX/APPROPRIATE6.Transponder ...............................................77007.ATC........................................................ NOTIFY

ERJ-170 QRH Original 29AUG2005 xix

x

Intentionally Left Blank

Original 29AUG2005 ERJ-170 QRHx

EICAS MESSAGES

MESSAGE PAGE MESSAGE PAGE

AC BUS 1 OFF . . . . . . . . . . . . 14AC BUS 2 OFF . . . . . . . . . . . . 14AC ESS BUS OFF . . . . . . . . . 15AC STBY BUS OFF . . . . . . . . 15ADS 1 FAIL . . . . . . . . . . . . . . . 48ADS 1 HTR FAIL . . . . . . . . . . . 65ADS 1 HTR FAULT . . . . . . . . . 79ADS 2 FAIL . . . . . . . . . . . . . . . 48ADS 2 HTR FAIL . . . . . . . . . . . 65ADS 2 HTR FAULT . . . . . . . . . 79ADS 3 FAIL . . . . . . . . . . . . . . . 49ADS 3 HTR FAIL . . . . . . . . . . . 65ADS 3 SLIPCOMP FAIL . . . . . 79ADS 4 HTR FAIL . . . . . . . . . . . 65ADS 4 SLIPCOMP FAIL . . . . . 79ADS PROBE 1 (2, 3, 4) FAIL . 48AFCS FAULT . . . . . . . . . . . . . 79AFCS PANEL FAIL . . . . . . . . . 79AFCS PANEL FAULT . . . . . . . 79A-I ENG 1 FAIL . . . . . . . . . . . . 65A-I ENG 1 FAULT . . . . . . . . . . 79A-I ENG 1 LEAK . . . . . . . . . . . 79A-I ENG 2 FAIL . . . . . . . . . . . . 65A-I ENG 2 FAULT . . . . . . . . . . 79A-I ENG 2 LEAK . . . . . . . . . . . 79A-I ENG 2 VLV OPEN . . . . . . . 85A-I LO CAPACITY . . . . . . . . . . 66A-I MODE NOT AUTO . . . . . . 79A-I SWITCH OFF . . . . . . . . . . 79A-I WING 1 LEAK . . . . . . . . . . 66A-I WING 2 LEAK . . . . . . . . . . 66A-I WING FAIL . . . . . . . . . . . . 66A-I WING NO DISPATCH . . . . 66A-I WING VLV OPEN . . . . . . . . 85AILERON LH FAIL . . . . . . . . . 74AILERON RH FAIL . . . . . . . . . 74AMS CTRL FAIL . . . . . . . . . . . . 5AMS CTRL FAULT . . . . . . . . . 79AOA LIMIT FAIL . . . . . . . . . . . 36AP FAIL . . . . . . . . . . . . . . . . . . 11AP FAULT . . . . . . . . . . . . . . . . 79AP PITCH MISTRIM . . . . . . . . 11AP PITCH TRIM FAIL . . . . . . . 11AP PITCH TRIM FAULT . . . . . 79AP ROLL MISTRIM . . . . . . . . . 11APM FAIL . . . . . . . . . . . . . . . . 49APM FAULT . . . . . . . . . . . . . . 79APM MISCOMP . . . . . . . . . . . 49APPR 2 NOT AVAIL . . . . . . . . 79APU FAIL . . . . . . . . . . . . . . . . 10APU FAULT . . . . . . . . . . . . . . 10

APU FIRE . . . . . . . . . . . . . . . . . viiAPU FIRE DET FAIL . . . . . . . . 34APU FIREX BTL DISCH . . . . . 80APU FIREX FAIL . . . . . . . . . . . 34APU FUEL SOV CLOSED . . . 85APU FUEL SOV FAIL . . . . . . . 15APU GEN OFF BUS . . . . . . . . 15APU OIL HI TEMP . . . . . . . . . 10APU OIL LO PRESS . . . . . . . . 10APU SHUTTING DOWN . . . . . 85AT FAIL . . . . . . . . . . . . . . . . . . 11AT FAULT . . . . . . . . . . . . . . . . 80AT NOT IN HOLD . . . . . . . . . . 48AURAL WRN SYS FAIL . . . . . 48AURAL WRN SYS FAULT . . . 80AUTO CONFIG TRIM FAIL . . . 80AVNX ASCB FAULT . . . . . . . . 50AVNX DB MODULE FAIL . . . . 80AVNX MAU 1 FAN FAIL . . . . . 50AVNX MAU 1A FAIL . . . . . . . . 50AVNX MAU 1A FAULT . . . . . . 80AVNX MAU 1A OVHT . . . . . . . 52AVNX MAU 1B FAIL . . . . . . . . 50AVNX MAU 1B FAULT . . . . . . 80AVNX MAU 1B OVHT . . . . . . . 52AVNX MAU 2 FAN FAIL . . . . . 50AVNX MAU 2A FAIL . . . . . . . . 50AVNX MAU 2A FAULT . . . . . . 80AVNX MAU 2A OVHT . . . . . . . 52AVNX MAU 2B FAIL . . . . . . . . 51AVNX MAU 2B FAULT . . . . . . 80AVNX MAU 2B OVHT . . . . . . . 52AVNX MAU 3 FAN FAIL . . . . . 50AVNX MAU 3A FAIL . . . . . . . . 51AVNX MAU 3A FAULT . . . . . . 80AVNX MAU 3A OVHT . . . . . . . 52AVNX MAU 3B FAIL . . . . . . . . 51AVNX MAU 3B FAULT . . . . . . 80AVNX MAU 3B OVHT . . . . . . . 52BATT 1 DISCHARGING . . . . . 15BATT 1 OFF . . . . . . . . . . . . . . 14BATT 1 OVERTEMP . . . . . . . . viiBATT 1 TEMP SENS FAULT . 80BATT 1-2 OFF . . . . . . . . . . . . . 12BATT 2 DISCHARGING . . . . . 15BATT 2 OFF . . . . . . . . . . . . . . 16BATT 2 OVERTEMP . . . . . . . . viiBATT 2 TEMP SENS FAULT . 80BATT DISCHARGING . . . . . . . 12BLEED 1 FAIL . . . . . . . . . . . . . . 6BLEED 1 LEAK . . . . . . . . . . . . . 9

ERJ-170 QRH Original 29AUG2005 xxi

x

EICAS MESSAGES (cont’d)


BLEED 1 OFF . . . . . . . . . . . . . .74BLEED 2 FAIL . . . . . . . . . . . . . . .6BLEED 2 LEAK . . . . . . . . . . . . . .9BLEED 2 OFF . . . . . . . . . . . . . .74BLEED APU LEAK . . . . . . . . . . .6BLEED APU VLV OPEN . . . . . .85BRK CONTROL FAULT . . . . . .43BRK LH FAIL . . . . . . . . . . . . . .43BRK LH FAULT . . . . . . . . . . . . .43BRK OVERHEAT . . . . . . . . . . .68BRK PEDL LH SEAT FAIL . . . .80BRK PEDL RH SEAT FAIL . . . .80BRK RH FAIL . . . . . . . . . . . . . .43BRK RH FAULT . . . . . . . . . . . .43CABIN ALTITUDE HI . . . . . . .xviiiCABIN DIFF PRESS FAIL . . . . .6CCD 1 FAULT . . . . . . . . . . . . . .80CCD 2 FAULT . . . . . . . . . . . . . .80CENTER EBAY FANS FAIL . . . .9CHECK EICAS . . . . . . . . . . . . .52CHECK MFD 1 . . . . . . . . . . . . .52CHECK MFD 2 . . . . . . . . . . . . .52CHECK PFD 1 . . . . . . . . . . . . .52CHECK PFD 2 . . . . . . . . . . . . .52CMC FAIL . . . . . . . . . . . . . . . . .80CMF 1 FAIL . . . . . . . . . . . . . . . .80CMF 2 FAIL . . . . . . . . . . . . . . . .80CMS FAIL . . . . . . . . . . . . . . . . .53CMS FAULT . . . . . . . . . . . . . . .80CREW OXY LO PRESS . . . . . .48CREW WRN SYS FAULT . . . . .53CRG AFT FIRE SYS FAIL . . . .34CRG AFT FIREX HI ARM . . . . .80CRG AFT FIREX LO ARM . . . .80CRG AFT SMOKE . . . . . . . . . . xiiCRG FIRE PROT FAULT . . . . .81CRG FIREX HI DISCH . . . . . . .85CRG FIREX LO DISCH . . . . . .85CRG FWD FIRE SYS FAIL . . . .34CRG FWD FIREX HI ARM . . . .81CRG FWD FIREX LO ARM . . .81CRG FWD SMOKE . . . . . . . . . . xiiCRG FWD VENT FAIL . . . . . . .10CVR AFT FAIL . . . . . . . . . . . . .81CVR FWD FAIL . . . . . . . . . . . . .81DC BUS 1 OFF . . . . . . . . . . . . .16DC BUS 2 OFF . . . . . . . . . . . . .17DC ESS BUS 1 OFF . . . . . . . . .18DC ESS BUS 2 OFF . . . . . . . . .19DC ESS BUS 3 OFF . . . . . . . . .20DEFUEL SOV OPEN . . . . . . . .81DISPLAY CTRL FAIL . . . . . . . .49DISPLAY CTRL FAULT . . . . . .53

DOOR CENTER EBAY OPEN . .3DOOR CRG AFT OPEN . . . . . . .3DOOR CRG FWD OPEN . . . . . .3DOOR FUELING OPEN . . . . . . .3DOOR FWD EBAY OPEN . . . . .3DOOR HYD OPEN . . . . . . . . . . .3DOOR PAX AFT OPEN . . . . . . .4DOOR PAX FWD OPEN . . . . . . .4DOOR SERV AFT OPEN . . . . . .4DOOR SERV FWD OPEN . . . . .4EICAS FAULT . . . . . . . . . . . . . .49EICAS OVHT . . . . . . . . . . . . . .49ELEC EMERGENCY . . . . . . . .13ELEV NML MODE FAIL . . . . . .35ELEV THR COMP FAIL . . . . . .36ELEVATOR FAULT . . . . . . . . .36ELEVATOR LH FAIL . . . . . . . .37ELEVATOR RH FAIL . . . . . . . .37EMER BRK FAIL . . . . . . . . . . .68EMER BRK FAULT . . . . . . . . . .75EMER LT BATT FAULT . . . . . .12EMER LT NOT ARMED . . . . . . .5EMER LT ON . . . . . . . . . . . . . . .4ENG 1 CONTROL FAULT . . . .23ENG 1 FADEC FAULT . . . . . . .81ENG 1 FADEC OVERTEMP . . .23ENG 1 FAIL . . . . . . . . . . . . . . .24ENG 1 FIRE . . . . . . . . . . . . . . . viENG 1 FIRE DET FAIL . . . . . . .34ENG 1 FIREX BTL A FAIL . . . .81ENG 1 FIREX BTL B FAIL . . . .81ENG 1 FUEL IMP BYPASS . . 26ENG 1 FUEL LO PRESS . . . . .26ENG 1 FUEL SOV CLOSED . . .85ENG 1 FUEL SOV FAIL . . . . . .28ENG 1 FUEL SW FAIL . . . . . . .81ENG 1 NO DISPATCH . . . . . . .30ENG 1 OIL IMP BYPASS . . . . .81ENG 1 OIL LO LEVEL . . . . . . .30ENG 1 OIL LO PRESS . . . . . . .28ENG 1 OIL SW FAIL . . . . . . . . .81ENG 1 REV DEPLOYED . . . . .23ENG 1 REV FAIL . . . . . . . . . . .30ENG 1 REV INHIBIT . . . . . . . . .85ENG 1 REV PROT FAULT . . . .31ENG 1 REV TLA FAIL . . . . . . .28ENG 1 SHORT DISPATCH . . .81ENG 1 START VLV OPEN . . . .30ENG 1 T2 HEAT FAIL . . . . . . . .30ENG 1 TLA FAIL . . . . . . . . . . . .30ENG 1 TLA NOT IDLE . . . . . . .85ENG 2 CONTROL FAULT . . . .23ENG 2 FADEC FAULT . . . . . . .81

Original 29AUG2005 ERJ-170 QRHxii



ENG 2 FADEC OVERTEMP . . 23ENG 2 FAIL . . . . . . . . . . . . . . . 24ENG 2 FIRE . . . . . . . . . . . . . . . viENG 2 FIRE DET FAIL . . . . . . 34ENG 2 FIREX BTL A FAIL . . . 81ENG 2 FIREX BTL B FAIL . . . 81ENG 2 FUEL IMP BYPASS . . 26ENG 2 FUEL LO PRESS . . . . 26ENG 2 FUEL SOV CLOSED . . 85ENG 2 FUEL SOV FAIL . . . . . 28ENG 2 FUEL SW FAIL . . . . . . 81ENG 2 NO DISPATCH . . . . . . 30ENG 2 OIL IMP BYPASS . . . . 81ENG 2 OIL LO LEVEL . . . . . . . 30ENG 2 OIL LO PRESS . . . . . . 28ENG 2 OIL SW FAIL . . . . . . . . 81ENG 2 REV DEPLOYED . . . . 23ENG 2 REV FAIL . . . . . . . . . . 30ENG 2 REV INHIBIT . . . . . . . . 85ENG 2 REV PROT FAULT . . . 31ENG 2 REV TLA FAIL . . . . . . . 28ENG 2 SHORT DISPATCH . . . 81ENG 2 START VLV OPEN . . . 30ENG 2 T2 HEAT FAIL . . . . . . . 30ENG 2 TLA FAIL . . . . . . . . . . . 30ENG 2 TLA NOT IDLE . . . . . . 85ENG EXCEEDANCE . . . . . . . . 31ENG FIREX BTL A DISCH . . . 81ENG FIREX BTL B DISCH . . . 81ENG NO TAKEOFF DATA . . . 31ENG REF A-I DISAG . . . . . . . 31ENG REF ECS DISAG . . . . . . 31ENG TDS REF A-I ALL . . . . . . 85ENG TDS REF A-I ENG . . . . . 85ENG THR RATING DISAG . . . 31ENG TLA NOT TOGA . . . . . . . 28ENG TLA TRIM FAIL . . . . . . . 81FD FAIL . . . . . . . . . . . . . . . . . . 81FD FAULT . . . . . . . . . . . . . . . . 81FD LATERAL MODE OFF . . . 11FD VERTICAL MODE OFF . . . 11FDR AFT FAIL . . . . . . . . . . . . 82FDR FWD FAIL . . . . . . . . . . . . 82FLAP FAIL . . . . . . . . . . . . . . . . 38FLAP LO RATE . . . . . . . . . . . . 75FLT CTRL ADS FAIL . . . . . . . 82FLT CTRL FAULT . . . . . . . . . . 37FLT CTRL NO DISPATCH . . . 37FLT CTRL TEST FAILED . . . . 82FLT CTRL TEST IN PROG . . . 82FLT CTRL TEST PASSED . . . 82FMS 1 FAIL . . . . . . . . . . . . . . . 75FMS 1 GPS POS DISAG . . . . 82

FMS 2 FAIL . . . . . . . . . . . . . . . 75FMS 2 GPS POS DISAG . . . . 82FMS POS DISAG . . . . . . . . . . 82FUEL 1 LO LEVEL . . . . . . . . . 55FUEL 2 LO LEVEL . . . . . . . . . 55FUEL AC PUMP 1 FAIL . . . . . 55FUEL AC PUMP 2 FAIL . . . . . 55FUEL DC PUMP FAIL . . . . . . . 56FUEL EQUAL-XFEED OPEN . 82FUEL FEED 1 FAULT . . . . . . . 82FUEL FEED 2 FAULT . . . . . . . 82FUEL IMBALANCE . . . . . . . . . 56FUEL KG-LB MISMATCH . . . . 82FUEL TANK LO TEMP . . . . . . 56FUEL XFEED FAIL . . . . . . . . . 56FUEL XFEED SOV OPEN . . . 85FWD EBAY FANS FAIL . . . . . . 9GND PROX FAIL . . . . . . . . . . 54GPU CONNECTED . . . . . . . . . 12GROUND SPOILERS FAIL . . . 42HYD 1 EDP FAIL . . . . . . . . . . . 82HYD 1 EDP NOT D-PRESS . . 65HYD 1 ELEC PUMP FAIL . . . . 75HYD 1 HI TEMP . . . . . . . . . . . 58HYD 1 LO PRESS . . . . . . . . . . 58HYD 1 LO QTY . . . . . . . . . . . . 82HYD 1 OVERHEAT . . . . . . . . . 57HYD 1 SOV CLOSED . . . . . . . 85HYD 1 SOV FAIL . . . . . . . . . . 85HYD 2 EDP FAIL . . . . . . . . . . . 82HYD 2 EDP NOT D-PRESS . . 65HYD 2 ELEC PUMP FAIL . . . . 75HYD 2 HI TEMP . . . . . . . . . . . 58HYD 2 LO PRESS . . . . . . . . . . 58HYD 2 LO QTY . . . . . . . . . . . . 82HYD 2 OVERHEAT . . . . . . . . . 57HYD 2 SOV CLOSED . . . . . . . 85HYD 2 SOV FAIL . . . . . . . . . . 85HYD 3 ELEC PUMP A FAIL . . 75HYD 3 ELEC PUMP B FAIL . . 75HYD 3 HI TEMP . . . . . . . . . . . 58HYD 3 LO PRESS . . . . . . . . . . 58HYD 3 LO QTY . . . . . . . . . . . . 82HYD 3 OVERHEAT . . . . . . . . . 58HYD 3 PUMP A NOT ON . . . . 82HYD 3 VLV FAIL . . . . . . . . . . . 65HYD PTU FAIL . . . . . . . . . . . . 57HYD PTU NOT AUTO . . . . . . . 82HYD PUMP NOT AUTO . . . . . 82HYD TEMP SENS FAIL . . . . . 58ICE CONDITION . . . . . . . . . . . 83ICE DETECTOR 1 FAIL . . . . . 67ICE DETECTOR 2 FAIL . . . . . 67

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x



IDG 1 OFF BUS . . . . . . . . . . . .20IDG 1 OIL . . . . . . . . . . . . . . . . .20IDG 2 OFF BUS . . . . . . . . . . . .20IDG 2 OIL . . . . . . . . . . . . . . . . .20INVERTER FAIL . . . . . . . . . . . .83IRS 1 FAIL . . . . . . . . . . . . . . . .49IRS 1 NAV MODE FAIL . . . . . .75IRS 2 FAIL . . . . . . . . . . . . . . . .49IRS 2 NAV MODE FAIL . . . . . .75IRS ALIGNING . . . . . . . . . . . . .83IRS EXCESSIVE MOTION . . . .49IRS PRES POS INVALID . . . . .75LAV SMOKE . . . . . . . . . . . . . . .73LAV SMOKE DET FAIL . . . . . .83LG LEVER DISAG . . . . . . . . . .67LG NO DISPATCH . . . . . . . . . .76LG NOSE DOOR OPEN . . . . . .68LG TEMP EXCEEDANCE . . . .83LG WOW SYS FAIL . . . . . . . . .43LOAD SHED . . . . . . . . . . . . . . .83

MCDU 1 OVHT . . . . . . . . . . . . .53MCDU 2 OVHT . . . . . . . . . . . . .53MFD 1 FAULT . . . . . . . . . . . . . .53MFD 1 OVHT . . . . . . . . . . . . . .53MFD 2 FAULT . . . . . . . . . . . . . .53MFD 2 OVHT . . . . . . . . . . . . . .53NAVCOM 1 FAIL . . . . . . . . . . . .49NAVCOM 1 OVHT . . . . . . . . . .54NAVCOM 2 FAIL . . . . . . . . . . . .49NAVCOM 2 OVHT . . . . . . . . . .54NO TAKEOFF CONFIG . . . . . .48OBSERVER OXY LO PRESS .76PACK 1 FAIL . . . . . . . . . . . . . . .7PACK 1 OFF . . . . . . . . . . . . . . .76PACK 2 FAIL . . . . . . . . . . . . . . .7PACK 2 OFF . . . . . . . . . . . . . . .76PAX OXY NOT DEPLOYED . . .48PAX OXY SW NOT AUTO . . . .83PFD 1 FAULT . . . . . . . . . . . . . .54PFD 1 OVHT . . . . . . . . . . . . . . .54PFD 2 FAULT . . . . . . . . . . . . . .54PFD 2 OVHT . . . . . . . . . . . . . . .54PITCH CONTROL DISC . . . . . .83PITCH TRIM BKUP FAIL . . . . .83PITCH TRIM FAIL . . . . . . . . . . .40PITCH TRIM SW 1 FAIL . . . . . .83PITCH TRIM SW 2 FAIL . . . . . .83PRESN AUTO FAIL . . . . . . . . . .7PRESN AUTO FAULT . . . . . . 83PRESN MAN FAIL . . . . . . . . . . 7RALT 1 FAIL . . . . . . . . . . . . . . 83

RALT 2 FAIL . . . . . . . . . . . . . . .83RAM AIR FAULT . . . . . . . . . . .83RAT FAIL . . . . . . . . . . . . . . . . .83RECIRC SMK DET FAIL . . . . . . .9RECIRC SMOKE . . . . . . . . . . .73REMOTE CB TRIP . . . . . . . . . .83ROLL CONTROL DISC . . . . . .84RUDDER FAIL . . . . . . . . . . . . .41RUDDER FAULT . . . . . . . . . . .40RUDDER LIMITER FAIL . . . . . .41RUDDER NML MODE FAIL . . .36SHAKER 1 FAIL . . . . . . . . . . . .84SHAKER 2 FAIL . . . . . . . . . . . .84SHAKER ANTICIPATED . . . . .41SLAT FAIL . . . . . . . . . . . . . . . .38SLAT LO RATE . . . . . . . . . . . .75SLAT-FLAP LVR DISAG . . . . .41SPDA FAIL . . . . . . . . . . . . . . . .84SPDBRK LEVER DISAG . . . . .84SPOILER FAULT . . . . . . . . . . .44SPOILER NML MODE FAIL . . .42STAB LOCK FAULT . . . . . . . . .42STALL PROT FAIL . . . . . . . . . .42STALL PROT FAULT . . . . . . . .42STALL PROT ICE SPEED . . . .76STEER FAIL . . . . . . . . . . . . . . .68STEER FAULT . . . . . . . . . . . . .84STEER OFF . . . . . . . . . . . . . . .85SYS CONFIG FAIL . . . . . . . . . .54TAT 1 FAIL . . . . . . . . . . . . . . . .84TAT 2 FAIL . . . . . . . . . . . . . . . .84TCAS FAIL . . . . . . . . . . . . . . . .84TERRAIN FAIL . . . . . . . . . . . . .55TERRAIN NOT AVAILABLE . . .84TRU 1 FAIL . . . . . . . . . . . . . . . .12TRU 2 FAIL . . . . . . . . . . . . . . . .12TRU ESS FAIL . . . . . . . . . . . . .12VALIDATE CONFIG . . . . . . . . .55VHF 1 OVHT . . . . . . . . . . . . . . .54VHF 2 OVHT . . . . . . . . . . . . . . .54VHF 3 FAIL . . . . . . . . . . . . . . . .53VHF 3 OVHT . . . . . . . . . . . . . . .54WINDSHEAR FAIL . . . . . . . . . .55WINDSHIELD 1 HTR FAIL . . . .67WINDSHIELD 2 HTR FAIL . . . .67XBLEED FAIL . . . . . . . . . . . . . .74XBLEED SW OFF . . . . . . . . . . .84XPDR 1 FAIL . . . . . . . . . . . . . .84XPDR 2 FAIL . . . . . . . . . . . . . .84YD FAIL . . . . . . . . . . . . . . . . . .84YD FAULT . . . . . . . . . . . . . . . .84YD OFF . . . . . . . . . . . . . . . . . . .84

Original 29AUG2005 ERJ-170 QRHxiv

NON ANNUNCIATED

PAGE

Abnormal Landing Gear Extension . . . . . . . . . . . . . . . . . . . . . . . . . . . . 69Air Conditioning Smoke. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . viiiAPU Fire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . viiCabin Altitude Hi. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xviiiCargo Forward (Aft) Smoke . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xiiCargo Compartment Fire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35Ditching . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Driftdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29Dual Engine Failure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ivEICAS Spurious Messages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 76Electrical Fire or Smoke. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ixEmergency Descent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .xixEngine Abnormal Start. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iiiEngine Abnormal Vibration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27Engine Airstart . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32Engine Airstart Envelope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33Engine Fire, Severe Damage or Separation . . . . . . . . . . . . . . . . . . . .viEngine ITT Overtemperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28Evacuation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iiForced Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Fuel Leak . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 57Gear Lever Cannot Be Moved Up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 69Impaired or Cracked Windshield . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5Jammed Control Column - Pitch . . . . . . . . . . . . . . . . . . . . . . . . . . . .xivJammed Control Wheel - Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xvJammed Rudder Pedals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47Lightning Strike. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 77Loss of Hydraulic System 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 59Loss of Hydraulic System 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 60Loss of Hydraulic System 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61Loss of Hydraulic Systems 1 and 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . 62Loss of Hydraulic Systems 1 and 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . 63Loss of Hydraulic Systems 2 and 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . 64Loss of Pressurization Indication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8Overweight Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 71Oxygen Leakage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 69Partial or Gear Up Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70PITCH TRIM Runaway . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .xviPrecautionary Engine Shutdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26ROLL TRIM Runaway . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xviiSmoke Evacuation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xiiiSteering Runaway . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xviiStructural Damage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Volcanic Ash Encounter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27YAW TRIM Runaway . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . xvii

ERJ-170 QRH Original 29AUG2005 xxv

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Air Conditioning, Pressurization and PneumaticsAMS CTRL FAIL . . . . . . . . . . . . . . . . . . . . . . . .5AMS CTRL FAULT . . . . . . . . . . . . . . . . . . . . .79BLEED (1 or 2) FAIL . . . . . . . . . . . . . . . . . . . . .6BLEED (1 or 2) LEAK . . . . . . . . . . . . . . . . . . . .9BLEED (1 or 2) OFF . . . . . . . . . . . . . . . . . . . .74BLEED APU LEAK . . . . . . . . . . . . . . . . . . . . . .6BLEED APU VLV OPEN . . . . . . . . . . . . . . . . 85CABIN ALTITUDE HI . . . . . . . . . . . . . . . . . . xviiiCABIN DIFF PRESS FAIL . . . . . . . . . . . . . . . .6CENTER EBAY FANS FAIL . . . . . . . . . . . . . . .9CRG FWD VENT FAIL . . . . . . . . . . . . . . . . . . 10FWD EBAY FANS FAIL . . . . . . . . . . . . . . . . . .9Loss of Pressurization Indication . . . . . . . . . . .8PACK (1 or 2) FAIL . . . . . . . . . . . . . . . . . . . . . .7PACK (1 or 2) OFF . . . . . . . . . . . . . . . . . . . . .76PRESN AUTO FAIL . . . . . . . . . . . . . . . . . . . . .7PRESN AUTO FAULT . . . . . . . . . . . . . . . . . . 83PRESN MAN FAIL . . . . . . . . . . . . . . . . . . . . . .7RAM AIR FAULT . . . . . . . . . . . . . . . . . . . . . .83Structural Damage . . . . . . . . . . . . . . . . . . . . . .2XBLEED FAIL . . . . . . . . . . . . . . . . . . . . . . . . .74XBLEED SW OFF . . . . . . . . . . . . . . . . . . . . .84

APUAPU FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . .10APU FAULT . . . . . . . . . . . . . . . . . . . . . . . . . .10APU FIRE . . . . . . . . . . . . . . . . . . . . . . . . . . . . viiAPU FUEL SOV CLOSED . . . . . . . . . . . . . . . 85APU FUEL SOV FAIL . . . . . . . . . . . . . . . . . . .10APU OIL HI TEMP . . . . . . . . . . . . . . . . . . . . .10APU OIL LO PRESS . . . . . . . . . . . . . . . . . . .10APU SHUTTING DOWN . . . . . . . . . . . . . . . . 85

Auto Flight, Flight Instruments and NavigationADS (1 or 2 or 3) HTR FAIL . . . . . . . . . . . . . . 65ADS (1 or 2) FAIL . . . . . . . . . . . . . . . . . . . . . .48ADS (1 or 2) HTR FAULT . . . . . . . . . . . . . . . . 79ADS 3 FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . .49ADS 3 SLIPCOMP FAIL . . . . . . . . . . . . . . . . . 79ADS 4 HTR FAIL . . . . . . . . . . . . . . . . . . . . . .65ADS 4 SLIPCOMP FAIL . . . . . . . . . . . . . . . . . 79ADS PROBE 1 (2, 3, 4) FAIL . . . . . . . . . . . . .48AFCS FAULT . . . . . . . . . . . . . . . . . . . . . . . . .79AFCS PANEL FAIL . . . . . . . . . . . . . . . . . . . . .79AFCS PANEL FAULT . . . . . . . . . . . . . . . . . . .79AP FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . .11AP FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . .79AP PITCH MISTRIM . . . . . . . . . . . . . . . . . . . .11AP PITCH TRIM FAIL . . . . . . . . . . . . . . . . . . .11AP PITCH TRIM FAULT . . . . . . . . . . . . . . . . . 79AP ROLL MISTRIM . . . . . . . . . . . . . . . . . . . .11APM FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . .49APM FAULT . . . . . . . . . . . . . . . . . . . . . . . . . .79APM MISCOMP . . . . . . . . . . . . . . . . . . . . . . .49APPR 2 NOT AVAIL . . . . . . . . . . . . . . . . . . . .79AT FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . .11

Original 29AUG2005 ERJ-170 QRHxvi

AT FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . . .80AT NOT IN HOLD . . . . . . . . . . . . . . . . . . . . . .48AURAL WRN SYS FAIL . . . . . . . . . . . . . . . . .48

Auto Flight, Flight Instruments and Navigation (cont’d)AURAL WRN SYS FAULT . . . . . . . . . . . . . . .80AVNX ASCB FAULT . . . . . . . . . . . . . . . . . . . .50AVNX DB MODULE FAIL . . . . . . . . . . . . . . . .80AVNX MAU (1 or 2 or 3) FAN FAIL . . . . . . . .50AVNX MAU (1A or 1B) FAULT . . . . . . . . . . . .80AVNX MAU (1A or 1B) OVHT . . . . . . . . . . . . .52AVNX MAU (2A or 2B) FAULT . . . . . . . . . . . .80AVNX MAU (2A or 2B) OVHT . . . . . . . . . . . . .52AVNX MAU (3A or 3B) FAULT . . . . . . . . . . . .80AVNX MAU (3A or 3B) OVHT . . . . . . . . . . . . .52AVNX MAU 1A FAIL . . . . . . . . . . . . . . . . . . . .50AVNX MAU 1B FAIL . . . . . . . . . . . . . . . . . . . .50AVNX MAU 2A FAIL . . . . . . . . . . . . . . . . . . . .50AVNX MAU 2B FAIL . . . . . . . . . . . . . . . . . . . .51AVNX MAU 3A FAIL . . . . . . . . . . . . . . . . . . . .51AVNX MAU 3B FAIL . . . . . . . . . . . . . . . . . . . .51CCD (1 or 2) FAULT . . . . . . . . . . . . . . . . . . . .80CHECK EICAS . . . . . . . . . . . . . . . . . . . . . . . .52CHECK MFD (1 or 2) . . . . . . . . . . . . . . . . . . .52CHECK PFD (1 or 2) . . . . . . . . . . . . . . . . . . .52CMC FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . .80CMF (1 or 2) FAIL . . . . . . . . . . . . . . . . . . . . . .80CMS FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . .53CMS FAULT . . . . . . . . . . . . . . . . . . . . . . . . . .80CREW WRN SYS FAULT . . . . . . . . . . . . . . . .53CVR (AFT or FWD) FAIL . . . . . . . . . . . . . . . .81DISPLAY CTRL FAIL . . . . . . . . . . . . . . . . . . .49DISPLAY CTRL FAULT . . . . . . . . . . . . . . . . .53EICAS FAULT . . . . . . . . . . . . . . . . . . . . . . . . .49EICAS OVHT . . . . . . . . . . . . . . . . . . . . . . . . .49EICAS Spurious Messages . . . . . . . . . . . . . . .76FD FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . .81FD FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . . .81FD LATERAL MODE OFF . . . . . . . . . . . . . . .11FD VERTICAL MODE OFF . . . . . . . . . . . . . .11FDR (AFT or FWD) FAIL . . . . . . . . . . . . . . . .82FMS (1 or 2) FAIL . . . . . . . . . . . . . . . . . . . . . .75FMS (1 or 2) GPS POS DISAG . . . . . . . . . . .82FMS POS DISAG . . . . . . . . . . . . . . . . . . . . . .82GND PROX FAIL . . . . . . . . . . . . . . . . . . . . . .54IRS (1 or 2) FAIL . . . . . . . . . . . . . . . . . . . . . . .49IRS (1 or 2) NAV MODE FAIL . . . . . . . . . . . .75IRS ALIGNING . . . . . . . . . . . . . . . . . . . . . . . .83IRS EXCESSIVE MOTION . . . . . . . . . . . . . . .49IRS PRES POS INVALID . . . . . . . . . . . . . . . .75MACH TRIM FAULT . . . . . . . . . . . . . . . . . . . .92MCDU (1 or 2) OVHT . . . . . . . . . . . . . . . . . . .53MFD (1 or 2) FAULT . . . . . . . . . . . . . . . . . . . .53MFD (1 or 2) OVHT . . . . . . . . . . . . . . . . . . . .53NAVCOM (1 or 2) FAIL . . . . . . . . . . . . . . . . . .49NAVCOM (1 or 2) OVHT . . . . . . . . . . . . . . . .54PFD (1 or 2) FAULT . . . . . . . . . . . . . . . . . . . .54PFD (1 or 2) OVHT . . . . . . . . . . . . . . . . . . . . .54RALT (1 or 2) FAIL . . . . . . . . . . . . . . . . . . . . .83SYS CONFIG FAIL . . . . . . . . . . . . . . . . . . . . .54

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TAT (1 or 2) FAIL . . . . . . . . . . . . . . . . . . . . . . 84TCAS FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . .84TERRAIN FAIL . . . . . . . . . . . . . . . . . . . . . . . .55

Auto Flight, Flight Instruments and Navigation (cont’d)TERRAIN NOT AVAILABLE . . . . . . . . . . . . . . 84VALIDATE CONFIG . . . . . . . . . . . . . . . . . . . .55VHF (1 or 2 or 3) OVHT . . . . . . . . . . . . . . . . . 54VHF 3 FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . .53WINDSHEAR FAIL . . . . . . . . . . . . . . . . . . . . .55XPDR (1 or 2) FAIL . . . . . . . . . . . . . . . . . . . .84YD FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . .84YD FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . .84YD OFF . . . . . . . . . . . . . . . . . . . . . . . . . . . . .84

DitchingDitching . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1Forced Landing . . . . . . . . . . . . . . . . . . . . . . . .2

Doors & WindowsDOOR (CENTER or FWD) EBAY OPEN . . . .3DOOR (PAX or SERV) (FWD or AFT) OPEN .4DOOR CRG (FWD or AFT) OPEN . . . . . . . . .3DOOR HYD OPEN . . . . . . . . . . . . . . . . . . . . .3Impaired or Cracked Windshield . . . . . . . . . . .5

ElectricalAC BUS 1 OFF . . . . . . . . . . . . . . . . . . . . . . . .14AC BUS 2 OFF . . . . . . . . . . . . . . . . . . . . . . . .14AC ESS BUS OFF . . . . . . . . . . . . . . . . . . . . .15AC STBY BUS OFF . . . . . . . . . . . . . . . . . . . .15APU GEN OFF BUS . . . . . . . . . . . . . . . . . . . .15BATT (1 or 2) DISCHARGING . . . . . . . . . . . . 15BATT (1 or 2) OVERTEMP . . . . . . . . . . . . . . viiBATT (1 or 2) TEMP SENS FAULT . . . . . . . . 80BATT 1 OFF . . . . . . . . . . . . . . . . . . . . . . . . . .14BATT 1-2 OFF . . . . . . . . . . . . . . . . . . . . . . . .12BATT 2 OFF . . . . . . . . . . . . . . . . . . . . . . . . . .16BATT DISCHARGING . . . . . . . . . . . . . . . . . . 12DC BUS 1 OFF . . . . . . . . . . . . . . . . . . . . . . . .16DC BUS 2 OFF . . . . . . . . . . . . . . . . . . . . . . . .17DC ESS BUS 1 OFF . . . . . . . . . . . . . . . . . . .18DC ESS BUS 2 OFF . . . . . . . . . . . . . . . . . . .19DC ESS BUS 3 OFF . . . . . . . . . . . . . . . . . . .20ELEC EMERGENCY . . . . . . . . . . . . . . . . . . .13EMER LT BATT FAULT . . . . . . . . . . . . . . . . . 12GPU CONNECTED . . . . . . . . . . . . . . . . . . . .12IDG (1 or 2) OFF BUS . . . . . . . . . . . . . . . . . . 20IDG (1 or 2) OIL . . . . . . . . . . . . . . . . . . . . . . .20INVERTER FAIL . . . . . . . . . . . . . . . . . . . . . . .83LOAD SHED . . . . . . . . . . . . . . . . . . . . . . . . . .83RAT FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . .83REMOTE CB TRIP . . . . . . . . . . . . . . . . . . . . .83SPDA FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . .84TRU (1 or 2) FAIL . . . . . . . . . . . . . . . . . . . . . .12TRU ESS FAIL . . . . . . . . . . . . . . . . . . . . . . . .12

Original 29AUG2005 ERJ-170 QRHxviii

Emergency LightsEMER LT NOT ARMED . . . . . . . . . . . . . . . . . .5EMER LT ON . . . . . . . . . . . . . . . . . . . . . . . . . .4

Engines

Driftdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . .29Dual Engine Failure . . . . . . . . . . . . . . . . . . . ivENG (1 or 2) CONTROL FAULT . . . . . . . . . .23ENG (1 or 2) FADEC FAULT . . . . . . . . . . . . .81ENG (1 or 2) FADEC OVERTEMP . . . . . . . . .23ENG (1 or 2) FAIL . . . . . . . . . . . . . . . . . . . . . .24ENG (1 or 2) FIRE,Severe Damage or

Separation . . . . . . . . . . . . . . . . . viENG (1 or 2) FUEL IMP BYPASS . . . . . . . . .26ENG (1 or 2) FUEL LO PRESS . . . . . . . . . . .26ENG (1 or 2) FUEL SOV FAIL . . . . . . . . . . . .28ENG (1 or 2) FUEL SW FAIL . . . . . . . . . . . . .81ENG (1 or 2) NO DISPATCH . . . . . . . . . . . . .30ENG (1 or 2) OIL IMP BYPASS . . . . . . . . . . .81ENG (1 or 2) OIL LO LEVEL . . . . . . . . . . . . . .30ENG (1 or 2) OIL LO PRESS . . . . . . . . . . . . .28ENG (1 or 2) OIL SW FAIL . . . . . . . . . . . . . . .81ENG (1 or 2) REV DEPLOYED . . . . . . . . . . .23ENG (1 or 2) REV FAIL . . . . . . . . . . . . . . . . .30ENG (1 or 2) REV INHIBIT . . . . . . . . . . . . . . .85ENG (1 or 2) REV PROT FAULT . . . . . . . . . .31ENG (1 or 2) REV TLA FAIL . . . . . . . . . . . . . .28ENG (1 or 2) SHORT DISPATCH . . . . . . . . . .81ENG (1 or 2) START VLV OPEN . . . . . . . . . .30ENG (1 or 2) T2 HEAT FAIL . . . . . . . . . . . . . .30ENG (1 or 2) TLA FAIL . . . . . . . . . . . . . . . . . .30ENG (1 or 2) TLA NOT IDLE . . . . . . . . . . . . .90ENG EXCEEDANCE . . . . . . . . . . . . . . . . . . .31ENG NO TAKEOFF DATA . . . . . . . . . . . . . . .31ENG REF A-I DISAG . . . . . . . . . . . . . . . . . . .31ENG REF ECS DISAG . . . . . . . . . . . . . . . . . .31ENG TDS REF A-I ALL . . . . . . . . . . . . . . . . . .85ENG TDS REF A-I ENG . . . . . . . . . . . . . . . . .85ENG THR RATING DISAG . . . . . . . . . . . . . . .31ENG TLA NOT TOGA . . . . . . . . . . . . . . . . . . .28ENG TLA TRIM FAIL . . . . . . . . . . . . . . . . . . .81Engine Abnormal Start . . . . . . . . . . . . . . . . . iiiEngine Abnormal Vibration . . . . . . . . . . . . . . .27Engine Airstart . . . . . . . . . . . . . . . . . . . . . . . .32Engine Airstart Envelope . . . . . . . . . . . . . . . .33Engine ITT Overtemperature . . . . . . . . . . . . .28Precautionary Engine Shutdown . . . . . . . . . .26

EvacuationEvacuation . . . . . . . . . . . . . . . . . . . . . . . . . . . . ii

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Fire ProtectionAPU FIRE DET FAIL . . . . . . . . . . . . . . . . . . .34APU FIREX BTL DISCH . . . . . . . . . . . . . . . . . 80APU FIREX FAIL . . . . . . . . . . . . . . . . . . . . . .34Cargo Compartment Fire . . . . . . . . . . . . . . . . 35CRG (FWD or AFT) FIRE SYS FAIL . . . . . . . 34CRG AFT FIREX (HI or LO) ARM . . . . . . . . . 80CRG FIRE PROT FAULT . . . . . . . . . . . . . . . . 81CRG FIREX (HI or LO) DISCH . . . . . . . . . . . . 85CRG FWD FIREX (HI or LO) ARM . . . . . . . . . 81ENG (1 or 2) FIRE DET FAIL . . . . . . . . . . . . . 34ENG (1 or 2) FIREX BTL (A or B) FAIL . . . . . 81ENG FIREX BTL (A or B) DISCH . . . . . . . . . . 81LAV SMOKE DET FAIL . . . . . . . . . . . . . . . . . 83RECIRC SMK DET FAIL . . . . . . . . . . . . . . . . .9

Flight Controls(FLAP or SLAT) FAIL . . . . . . . . . . . . . . . . . . .38(FLAP or SLAT) LO RATE . . . . . . . . . . . . . . . 75(ROLL or YAW) TRIM Runaway . . . . . . . . . . . 53AILERON (LH or RH) FAIL . . . . . . . . . . . . . . .74AOA LIMIT FAIL . . . . . . . . . . . . . . . . . . . . . . .36AUTO CONFIG TRIM FAIL . . . . . . . . . . . . . . 80ELEV NML MODE FAIL . . . . . . . . . . . . . . . . . 35ELEV THR COMP FAIL . . . . . . . . . . . . . . . . . 36ELEVATOR (LH or RH) FAIL . . . . . . . . . . . . . 37ELEVATOR FAULT . . . . . . . . . . . . . . . . . . . .36FLT CTRL ADS FAIL . . . . . . . . . . . . . . . . . . .82FLT CTRL NO DISPATCH . . . . . . . . . . . . . . .37FLT CTRL TEST FAILED . . . . . . . . . . . . . . . . 82FLT CTRL TEST IN PROG . . . . . . . . . . . . . . 82FLT CTRL TEST PASSED . . . . . . . . . . . . . . .82FTL CTRL FAULT . . . . . . . . . . . . . . . . . . . . .37GROUND SPOILERS FAIL . . . . . . . . . . . . . . 42Jammed Control Column - Pitch . . . . . . . . .xivJammed Control Wheel - Roll . . . . . . . . . . . xvJammed Rudder Pedals . . . . . . . . . . . . . . . . . 47NO TAKEOFF CONFIG . . . . . . . . . . . . . . . . . 48PITCH CONTROL DISC . . . . . . . . . . . . . . . . . 83PITCH TRIM BKUP FAIL . . . . . . . . . . . . . . . . 83PITCH TRIM FAIL . . . . . . . . . . . . . . . . . . . . .40PITCH TRIM Runaway . . . . . . . . . . . . . . . . .xviPITCH TRIM SW (1 or 2) FAIL . . . . . . . . . . . . 83ROLL CONTROL DISC . . . . . . . . . . . . . . . . . 84RUDDER FAIL . . . . . . . . . . . . . . . . . . . . . . . .41RUDDER FAULT . . . . . . . . . . . . . . . . . . . . . .40RUDDER LIMITER FAIL . . . . . . . . . . . . . . . . 41RUDDER NML MODE FAIL . . . . . . . . . . . . . . 36SHAKER (1 or 2) FAIL . . . . . . . . . . . . . . . . . . 84SHAKER ANTICIPATED . . . . . . . . . . . . . . . . 41SLAT-FLAP LVR DISAG . . . . . . . . . . . . . . . . 41SPDBRK LEVER DISAG . . . . . . . . . . . . . . . . 84SPOILER FAULT . . . . . . . . . . . . . . . . . . . . . .44SPOILER NML MODE FAIL . . . . . . . . . . . . . . 42STAB LOCK FAULT . . . . . . . . . . . . . . . . . . . .26STALL PROT FAIL . . . . . . . . . . . . . . . . . . . . .42STALL PROT FAULT . . . . . . . . . . . . . . . . . . .42STALL PROT ICE SPEED . . . . . . . . . . . . . . .76

Original 29AUG2005 ERJ-170 QRHxx

FuelDEFUEL SOV OPEN . . . . . . . . . . . . . . . . . . .81DOOR FUELING OPEN . . . . . . . . . . . . . . . . . .3ENG (1 or 2) FUEL SOV CLOSED . . . . . . . . .85FUEL (1 or 2) LO LEVEL . . . . . . . . . . . . . . . .55FUEL AC PUMP (1 or 2) FAIL . . . . . . . . . . . .55FUEL DC PUMP FAIL . . . . . . . . . . . . . . . . . .56FUEL EQUAL-XFEED OPEN . . . . . . . . . . . . .82FUEL FEED (1 or 2) FAULT . . . . . . . . . . . . . .82FUEL IMBALANCE . . . . . . . . . . . . . . . . . . . . .56FUEL KG-LB MISMATCH . . . . . . . . . . . . . . . .82Fuel Leak . . . . . . . . . . . . . . . . . . . . . . . . . . . .57FUEL TANK LO TEMP . . . . . . . . . . . . . . . . . .56FUEL XFEED FAIL . . . . . . . . . . . . . . . . . . . . .56FUEL XFEED SOV OPEN . . . . . . . . . . . . . . .85

HydraulicsHYD (1 or 2 or 3) LO QTY . . . . . . . . . . . . . . .82HYD (1 or 2) EDP FAIL . . . . . . . . . . . . . . . . . .82HYD (1 or 2) EDP NOT D-PRESS . . . . . . . . .65HYD (1 or 2) ELEC PUMP FAIL . . . . . . . . . . .75HYD (1 or 2) HI TEMP . . . . . . . . . . . . . . . . . .58HYD (1 or 2) LO PRESS . . . . . . . . . . . . . . . . .58HYD (1 or 2) OVERHEAT . . . . . . . . . . . . . . . .57HYD (1 or 2) SOV CLOSED . . . . . . . . . . . . . .85HYD (1 or 2) SOV FAIL . . . . . . . . . . . . . . . . .85HYD 3 ELEC PUMP A FAIL . . . . . . . . . . . . . .75HYD 3 ELEC PUMP B FAIL . . . . . . . . . . . . . .75HYD 3 HI TEMP . . . . . . . . . . . . . . . . . . . . . . .58HYD 3 LO PRESS . . . . . . . . . . . . . . . . . . . . .58HYD 3 OVERHEAT . . . . . . . . . . . . . . . . . . . .58HYD 3 PUMP A NOT ON . . . . . . . . . . . . . . . .82HYD 3 VLV FAIL . . . . . . . . . . . . . . . . . . . . . . .65HYD PTU FAIL . . . . . . . . . . . . . . . . . . . . . . . .57HYD PTU NOT AUTO . . . . . . . . . . . . . . . . . .82HYD PUMP NOT AUTO . . . . . . . . . . . . . . . . .82HYD TEMP SENS FAIL . . . . . . . . . . . . . . . . .58Loss of Hydraulic System 1 . . . . . . . . . . . . . .59Loss of Hydraulic System 2 . . . . . . . . . . . . . .60Loss of Hydraulic System 3 . . . . . . . . . . . . . .61Loss of Hydraulic Systems 1 and 2 . . . . . . . .62Loss of Hydraulic Systems 1 and 3 . . . . . . . .63Loss of Hydraulic Systems 2 and 3 . . . . . . . .64

Ice & Rain ProtectionA-I ENG (1 or 2) FAIL . . . . . . . . . . . . . . . . . . .65A-I ENG (1 or 2) FAULT . . . . . . . . . . . . . . . . .79A-I ENG (1 or 2) LEAK . . . . . . . . . . . . . . . . . .79A-I LO CAPACITY . . . . . . . . . . . . . . . . . . . . .66A-I MODE NOT AUTO . . . . . . . . . . . . . . . . . .79A-I SWITCH OFF . . . . . . . . . . . . . . . . . . . . . .79A-I WING (1 or 2) LEAK . . . . . . . . . . . . . . . . .66A-I WING FAIL . . . . . . . . . . . . . . . . . . . . . . . .66A-I WING NO DISPATCH . . . . . . . . . . . . . . . .66ICE CONDITION . . . . . . . . . . . . . . . . . . . . . . .83ICE DETECTOR (1 or 2) FAIL . . . . . . . . . . . .67WINDSHIELD (1 or 2) HTR FAIL . . . . . . . . . .67

ERJ-170 QRH Original 29AUG2005 xxxi

x

Landing GearAbnormal Landing Gear Extension . . . . . . . . . 69BRK (LH or RH) FAIL . . . . . . . . . . . . . . . . . . .43BRK (LH or RH) FAULT . . . . . . . . . . . . . . . . . 43BRK CONTROL FAULT . . . . . . . . . . . . . . . . . 43BRK OVERHEAT . . . . . . . . . . . . . . . . . . . . . .68BRK PEDL (LH or RH) SEAT FAIL . . . . . . . . 80EMER BRK FAIL . . . . . . . . . . . . . . . . . . . . . .68EMER BRK FAULT . . . . . . . . . . . . . . . . . . . .75Gear Lever Cannot Be Moved Up . . . . . . . . . 69LG LEVER DISAG . . . . . . . . . . . . . . . . . . . . .67LG NO DISPATCH . . . . . . . . . . . . . . . . . . . . .76LG NOSE DOOR OPEN . . . . . . . . . . . . . . . . . 68LG TEMP EXCEEDANCE . . . . . . . . . . . . . . . 83LG WOW SYS FAIL . . . . . . . . . . . . . . . . . . . .43Partial or Gear Up Landing . . . . . . . . . . . . . . .70STEER FAIL . . . . . . . . . . . . . . . . . . . . . . . . . .68STEER FAULT . . . . . . . . . . . . . . . . . . . . . . . .84STEER OFF . . . . . . . . . . . . . . . . . . . . . . . . . .85Steering Runaway . . . . . . . . . . . . . . . . . . . . xvii

Lightning StrikeLightning Strike . . . . . . . . . . . . . . . . . . . . . . . . 77

Ops DataApproach Minimums Determination . . . . . . . . 89

Holding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .87Minimum Brake Cooling Time . . . . . . . . . . . . 85RVSM Required Equipment . . . . . . . . . . . . . . 87Severe Weather/Windshear . . . . . . . . . . . . . . 91Takeoff Alternate . . . . . . . . . . . . . . . . . . . . . .88Takeoff Minimums . . . . . . . . . . . . . . . . . . . . .88Unfactored Landing Distance . . . . . . . . . . . . . 92Wind Component/Temp Conversion . . . . . . . 90

Overweight LandingOverweight Landing . . . . . . . . . . . . . . . . . . . .71

OxygenCREW OXY LO PRESS . . . . . . . . . . . . . . . . . 48OBSERVER OXY LO PRESS . . . . . . . . . . . . 76Oxygen Leakage . . . . . . . . . . . . . . . . . . . . . .69PAX OXY NOT DEPLOYED . . . . . . . . . . . . . . 48PAX OXY SW NOT AUTO . . . . . . . . . . . . . . .83

SmokeCRG (FWD or AFT) SMOKE . . . . . . . . . . . . . xiiLAV SMOKE . . . . . . . . . . . . . . . . . . . . . . . . . .73RECIRC SMOKE . . . . . . . . . . . . . . . . . . . . . .73 Air Condition Smoke . . . . . . . . . . . . . . . . . .viii

Original 29AUG2005 ERJ-170 QRHxxii

Electrical System Fire or Smoke . . . . . . . . . ixCargo Forward (Aft) Smoke . . . . . . . . . . . . . xiiSmoke Evacuation . . . . . . . . . . . . . . . . . . . . xiii

Volcanic AshVolcanic Ash Encounter . . . . . . . . . . . . . . . . .27

Non Normal Descent / Landing Checklists

PAGE

Aileron Failure Descent Checklist . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .74Aileron Failure Landing Checklist . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .74Dual Engine Failure Descent Checklist . . . . . . . . . . . . . . . . . . . . . . . . .22Dual Engine Failure Landing Checklist . . . . . . . . . . . . . . . . . . . . . . . . . .22Engine Out Descent Checklist . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .25Engine Out Landing Checklist . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .25FLAP/SLAT FAIL Descent Checklist . . . . . . . . . . . . . . . . . . . . . . . . . . .39FLAP/SLAT FAIL Landing Checklist . . . . . . . . . . . . . . . . . . . . . . . . . . . .39Flight Control/Brake Malfunction Descent Checklist . . . . . . . . . . . . . . . .45Flight Control/Brake Malfunction Landing Checklist . . . . . . . . . . . . . . . .45Jammed Rudder Pedals Descent Checklist . . . . . . . . . . . . . . . . . . . . . .47Jammed Rudder Pedals Landing Checklist . . . . . . . . . . . . . . . . . . . . . .47Loss of Hydraulic System 1 Descent Checklist . . . . . . . . . . . . . . . . . . .59Loss of Hydraulic System 1 Landing Checklist . . . . . . . . . . . . . . . . . . . .59Loss of Hydraulic System 2 Descent Checklist . . . . . . . . . . . . . . . . . . .60Loss of Hydraulic System 2 Landing Checklist . . . . . . . . . . . . . . . . . . . .60Loss of Hydraulic Systems 1 and 2 Descent Checklist . . . . . . . . . . . . . .62Loss of Hydraulic Systems 1 and 2 Landing Checklist . . . . . . . . . . . . . .62Loss of Hydraulic Systems 1 and 3 Descent Checklist . . . . . . . . . . . . . .63Loss of Hydraulic Systems 1 and 3 Landing Checklist . . . . . . . . . . . . . .63Loss of Hydraulic Systems 2 and 3 Descent Checklist . . . . . . . . . . . . . .64Loss of Hydraulic Systems 2 and 3 Landing Checklist . . . . . . . . . . . . . .64Pitch/Roll Malfunction Descent Checklist . . . . . . . . . . . . . . . . . . . . . . . .46Pitch/Roll Malfunction Landing Checklist . . . . . . . . . . . . . . . . . . . . . . . .46RAT Deployed Descent Checklist . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .21RAT Deployed Landing Checklist . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .21Smoke / Fumes Descent Checklist . . . . . . . . . . . . . . . . . . . . . . . . . . . . .72Smoke / Fumes Landing Checklist . . . . . . . . . . . . . . . . . . . . . . . . . . . . .72

ERJ-170 QRH Original 29AUG2005 xxxiii

x


Original 29AUG2005 ERJ-170 QRHxxiv

Ditching

Note: Accomplish the following procedure in lieu of the Normal Procedures Descent and Landing Checklist.

1. Distress Signal........................ Transmit “MAYDAY, MAYDAY, MAYDAY”a. Transmit present position, altitude, heading, speed, type of

aircraft, situation and intentions. Estimate time and position of intended touchdown and request intercept.

2. Transponder ....................................................................................77003. Cabin Crew.....................................................................................Notify4. Aural Warning Circuit Breakers (C7 and C31)................................PULL5. NO PED/FSTN BELTS ...................................................................... ON6. Landing Data ..................................................................................... Set7. Life Vests, Shoulder Harness & Seat Belts.........................................On8. ELT .................................................................................................... ON

At 10,000 ft. AGL:9. PRESSURIZATION DUMP....................................................... PUSH IN

10. Altimeters.................................................................................. __.__SetBelow 5,000 ft. AGL:11. PRESSURIZATION MODE .............................................................MAN12. CABIN ALT ..........................................................DOWN for 50 seconds13. Considerations:

• Plan touchdown on upwind side & parallel to waves and swells.• On final approach, level the wings and avoid skidding.• Touchdown with 5° nose up attitude, and at less than 200 ft./min.

descent ratio.• In a normal flotation condition the aircraft will rest with the fwd doors

above the waterline and aft doors below water line.• Review Ditching procedures below.• Transmit all pertinent information regarding final ditching position.

Final Approach:14. GND PROX TERR INHIB ......................................................... PUSH IN15. Landing Gear......................................................................................UP16. SLAT/FLAP...............................................................Maximum Available17. APU EMER STOP .................................................................... PUSH IN18. Airspeed ................................ 130 KIAS min. if engines are not running,19. Below 1,000 feet AGL.................................Advise on PA “Brace, brace”Ditching:20. Thrust Levers................................................................................... IDLE21. START/STOP ................................................................................ STOP22. Engine Fire Handles .................................................PULL and ROTATE23. Evacuation................................................................................... Initiate

[Initiate the evacuation by using the passenger address system. “Evacuate, Evacuate”.]

24. BATT 1 & BATT 2 .............................................................................OFF25. Ditching Checklist complete, and

* Establish and communicate a plan.

ERJ-170 QRH Original 29AUG2005 1

Forced Landing


1. Distress Signal ........................Transmit “MAYDAY, MAYDAY, MAYDAY”a. Transmit present position, altitude, heading, speed, type of

aircraft, situation and intentions. Estimate time and position of intended touchdown.

2. Transponder ................................................................................... 77003. Cabin Crew.....................................................................................Notify4. Aural Warning Circuit Breakers (C7 and C31) ............................... PULL5. NO PED/FSTN BELTS .......................................................................ON6. ELT .....................................................................................................ON

Below 10,000 ft. AGL:7. PRESSURIZATION DUMP ...................................................... PUSH IN8. Altimeters ..................................................................................__.__Set9. Considerations:

• Review “Evacuation” procedures on page ii.• Transmit all pertinent information regarding final landing position.

Final Approach:10. GND PROX TERR INHIB......................................................... PUSH IN11. Landing Gear................................................................................DOWN12. SLAT/FLAP...............................................................Maximum Available13. APU EMER STOP.................................................................... PUSH IN14. Airspeed ................................. 130 KIAS min. if engines are not running15. Below 1,000 feet AGL ................................Advise on PA “Brace, brace”16. Forced Landing Checklist complete, and

* Establish and communicate a plan.* After landing, accomplish “Evacuation” procedures on page ii.

Structural Damage

1. Airspeed .......................................................................... 200 KIAS MAX2. High Maneuvering Loads ............................................................... Avoid3. Land at the nearest suitable airport.4. If fuselage is damaged:

a. Altitude .................. 10,000 ft. or safe altitude (whichever is higher)When reaching 10,000 ft.:b. PRESSURIZATION DUMP .............................................. PUSH INc. Establish landing configuration early.d. Structural Damage Checklist complete, and

* Establish and communicate a plan.* This is an NTSB Reportable Event.

If fuselage is not damaged:a. Establish landing configuration early.b. Structural Damage Checklist complete, and


or

Original 29AUG2005 ERJ-170 QRH2

DOOR CRG (FWD or AFT) OPEN

[Condition: Associated baggage door open or not properly locked.]1. If pressurization is normal:

a. DOOR CRG (FWD or AFT) OPEN Checklist complete.If pressurization is not normal:a. Land at the nearest suitable airport.b. Altitude................... 10,000 ft. or safe altitude (whichever is higher)When reaching 10,000 ft.:c. PRESSURIZATION DUMP............................................... PUSH INd. DOOR CRG (FWD or AFT) OPEN Checklist complete, and


DOOR FUELING OPEN

[Condition: Fueling door open or not properly locked.]1. Monitor aircraft systems.2. DOOR FUELING OPEN Checklist complete.

DOOR (CENTER or FWD) EBAY OPEN

[Condition: Associated electronic bay door open or not properly locked.]1. If pressurization is normal:

a. DOOR (CENTER or FWD) EBAY OPEN Checklist complete.If pressurization is not normal:a. Altitude .................. 10,000 ft. or safe altitude (whichever is higher)b. DOOR (CENTER or FWD) EBAY OPEN Checklist complete, and


DOOR HYD OPEN

[Condition: Hydraulic System 3 access door open or not properly locked.]1. Airspeed ..........................................................................250 KIAS MAX2. DOOR HYD OPEN Checklist complete.

or

or


DOOR (PAX or SERV) (FWD or AFT) OPEN

[Condition: (Main passenger or service) door open or not properly locked either on the ground with an engine running or in flight.]

1. FSTN BELTS......................................................................................ON2. If pressurization is normal:

a. If a minimum of 2 door lock indicators are green:(1) DOOR (PAX or SERV) (FWD or AFT) OPEN Checklist

complete, and* Establish and communicate a plan.

If a minimum of 2 door lock indicators are not green:(1) Land at nearest suitable airport.(2) Altitude ......... 10,000 ft. or safe altitude (whichever is higher)When reaching 10,000 ft.:(3) PRESSURIZATION DUMP ..................................... PUSH IN(4) DOOR (PAX or SERV) (FWD or AFT) OPEN Checklist


If pressurization is not normal:a. Land at the nearest suitable airport.b. Altitude .................. 10,000 ft. or safe altitude (whichever is higher)When reaching 10,000 ft.:c. PRESSURIZATION DUMP .............................................. PUSH INd. DOOR (PAX or SERV) (FWD or AFT) OPEN Checklist complete,

and* Establish and communicate a plan.

EMER LT NOT ARMED

[Condition: Emergency lighting system not armed.]1. EMER LT .................................................................................... ARMED2. EMER LT NOT ARMED Checklist complete.

EMER LT ON

[Condition: Emergency lighting system ON.]1. EMER LT ................................................................... OFF then ARMED2. EMER LT ON Checklist complete.

or

or


Impaired or Cracked Windshield

1. Associated WINDSHIELD HEATING................................... PUSH OUT2. Cockpit Door................................................................................CLOSE

Note: There is a windshield heating wire between the middle and outer layers.

3. If the wire appears to have continuity (i.e., no gap), then the crack is in the outer layer:a. Continue normal operations.b. Impaired or Cracked Windshield Checklist complete.If the wire appears to have a discontinuity (i.e., gap), then the crack may be in the middle and/or inner layers:a. Airspeed ..................................................................220 KIAS MAXb. Altitude................... 10,000 ft. or safe altitude (whichever is higher)c. Land at the nearest suitable airport, and

* Establish and communicate a plan.While descending:d. PRESSURIZATION MODE .....................................................MANe. PRESSURIZATION CABIN ALT.................................................UPf. 10,000 ft. cabin altitude .........................maintain while descendingAt or below 10,000 ft.:g. PACK 1 ......................................................................... PUSH OUTh. PACK 2 ......................................................................... PUSH OUTi. If visibility is impaired on both sides:

(1) Airspeed .........................................................140 KIAS MAX(2) Direct Vision Window ...................................................OPEN(3) Impaired or Cracked Windshield Checklist complete.If visibility is impaired on only one side:(1) Pilot flying must be on the non-impaired side.(2) Impaired or Cracked Windshield Checklist complete.

AMS CTRL FAIL

[Condition: Both AMS controller channels failed.]1. Icing Conditions ..............................................................................Avoid2. Altitude........................... 10,000 ft. or safe altitude (whichever is higher)

At 10,000 ft.:3. PRESSURIZATION DUMP....................................................... PUSH IN4. Considerations:

• Assisted crossbleed start is not available.• Pneumatic assisted engine start APU is not available.

5. Land at the nearest suitable airport.6. AMS CTRL FAIL Checklist complete, and


or

or


CABIN DIFF PRESS FAIL

[Condition: Cabin differential pressure controller failed. Abnormal cabin indication.]

1. If cabin differential pressure red limit is reached:a. If cabin differential pressure value is negative:

(1) Aircraft descent rate...................................................Reduce(2) CABIN DIFF PRESS FAIL Checklist complete.If cabin differential pressure value is positive:(1) PACK 1 ............................................................... PUSH OUT(2) PACK 2 ............................................................... PUSH OUT(3) Altitude ...Max 10,000 ft or safe altitude (whichever is higher)(4) CABIN DIFF PRESS FAIL Checklist complete.

If cabin differential pressure red limit is not reached:a. CABIN DIFF PRESS FAIL Checklist complete.

BLEED APU LEAK

[Condition: An overheat detected in the APU bleed or both APU overheat detection system loops failed.]

1. APU BLEED ......................................................................... PUSH OUTWait 3 minutes.

2. If BLEED APU LEAK remains annunciated:a. APU EMER STOP............................................................ PUSH INb. APU MASTER..........................................................................OFFc. If BLEED APU LEAK still remains annunciated:

(1) BLEED 1 ............................................................. PUSH OUT(2) XBLEED.............................................................. PUSH OUT(3) BLEED 1 OFF .................................................... Annunciated(4) XBLEED SW OFF.............................................. Annunciated(5) BLEED APU LEAK Checklist complete.If BLEED APU LEAK does not remain annunciated:(1) BLEED APU LEAK Checklist complete.

If BLEED APU LEAK does not remain annunciated:a. Resume normal operations.b. BLEED APU LEAK Checklist complete.

BLEED (1 or 2) FAIL

[Condition: A bleed failure detected. Bleed no longer available.]1. Associated BLEED............................................................... PUSH OUT

Wait 1 minute.2. If BLEED (1 or 2) remains annunciated:

a. Altitude ..................................................................... 31,000 ft. maxb. BLEED (1 or 2) FAIL Checklist complete.If BLEED (1 or 2) does not remain annunciated:a. Associated BLEED........................................................... PUSH INb. BLEED (1 or 2) FAIL Checklist complete.

or

or

or

or

or


PACK (1 or 2) FAIL

[Condition: Associated Pack no longer available.]1. CKPT or PAX CABIN................................................. 12 o’clock position2. Associated PACK ................................................................ PUSH OUT

Wait 1 minute.3. Associated PACK .................................................................... PUSH IN4. If PACK (1 or 2) remains annunciated:

a. Associated PACK ......................................................... PUSH OUTb. Altitude...................................................................... 31,000 ft. maxc. PACK (1 or 2) FAIL Checklist complete.If PACK (1 or 2) does not remain annunciated:After one (1) minute:a. CKPT or PAX CABIN........................................... Operate normallyb. PACK (1 or 2) FAIL Checklist complete.

PRESN AUTO FAIL

[Condition: Both pressurization controller channels automatic mode failed. Abnormal cabin indication (amber dashes) may be presented.]

1. PRESSURIZATION MODE ..........................................MAN then AUTO2. If PRESN AUTO FAIL remains annunciated:

a. PRESSURIZATION MODE .....................................................MANb. CABIN ALT .................................................................Set Pressure

See “AIRCRAFT/CABIN ALTITUDE CONVERSION TABLE” on page 8..

At 5,000 ft.:c. CABIN ALT .................................................Hold up for 50 secondsd. PRESN AUTO FAIL Checklist complete.If PRESN AUTO FAIL does not remain annunciated:a. Proceed with the flight and monitor pressurization.b. PRESN AUTO FAIL Checklist complete.

PRESN MAN FAIL

[Condition: Both pressurization controller channels automatic mode failed.]1. Altitude........................... 10,000 ft. or safe altitude (whichever is higher)

At 25,000 ft.:2. PACK 1 ................................................................................. PUSH OUT

At 10,000 ft.:3. PACK 2 ................................................................................. PUSH OUT4. PRESN MAN FAIL Checklist complete.

or

or


Loss of Pressurization Indication

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

AIRCRAFT/CABIN ALTITUDE CONVERSION TABLE

AIRCRAFT ALTITUDE (ft.)

CABIN ALTITUDE (ft.)

DIFFERENTIALPRESSURE

(PSID)10000 600 4.311000 700 4.612000 800 4.913000 1000 5.214000 1100 5.515000 1300 5.716000 1500 6.017000 1600 6.218000 1800 6.419000 2000 6.620000 2200 6.821000 2500 6.922000 2700 7.123000 2900 7.324000 3100 7.425000 3400 7.526000 3700 7.627000 3900 7.728000 4200 7.829000 4400 7.930000 4700 8.031000 5000 8.132000 5300 8.133000 5600 8.234000 5900 8.235000 6200 8.236000 6500 8.337000 6800 8.338000 7100 8.339000 7400 8.340000 7700 8.341000 8000 8.3


RECIRC SMK DET FAIL

[Condition: Smoke detector failed.]1. RECIRC FAN........................................................................ PUSH OUT2. RECIRC SMK DET FAIL Checklist complete.

BLEED (1 or 2) LEAK

[Condition: An overheat detected at the associated bleed system/pack. An amber stripe bar illuminated inside the affected bleed switch.]

1. Associated BLEED ............................................................... PUSH OUT2. APU BLEED (if applicable) ................................................... PUSH OUT3. XBLEED ............................................................................... PUSH OUT4. Icing Conditions ..............................................................................Avoid5. Altitude.............................................................................. 31,000 ft. max

Wait 3 minutes.6. If BLEED (1 or 2) LEAK remains annunciated:

a. If BLEED (1 or 2) OFF is annunciated:Note: Consider the possibility of leakage in the opposite side.(1) Opposite side BLEED ......................................... PUSH OUT(2) APU BLEED ....................................................................OFF(3) Altitude ......... 10,000 ft. or safe altitude (whichever is higher)At 10,000 ft.:(4) PRESSURIZATION DUMP ..................................... PUSH IN(5) BLEED (1 or 2) LEAK Checklist complete.If BLEED (1 or 2) OFF is not annunciated:(1) Associated Thrust Lever ................................................IDLE(2) BLEED (1 or 2) LEAK Checklist complete, and

* Accomplish “Engine Out Descent Checklist”, page 25.If BLEED (1 or 2) LEAK does not remain annunciated:a. BLEED (1 or 2) LEAK Checklist complete.

CENTER EBAY FANS FAIL

1. Land at the nearest suitable airport.2. CENTER EBAY FANS FAIL Checklist complete, and


FWD EBAY FANS FAIL

[Condition: Forward ebay fans failed.]1. If TRU (1 or 2) is annunciated:

a. Land at the nearest suitable airport.b. FWD EBAY FANS FAIL Checklist complete, and

* Establish and communicate a plan.If TRU (1 or 2) is not annunciated:a. FWD EBAY FANS FAIL Checklist complete.

or

or

or


CRG FWD VENT FAIL

1. Land at the nearest suitable airport.2. CRG FWD VENT FAIL Checklist complete, and


APU FAIL

[Condition: APU FAIL with automatic shutdown. APU cannot be restarted.]1. If APU FAIL is annunciated during start:

a. APU can be restarted according to APU starter limitations.b. APU FAIL Checklist complete.If APU FAIL is not annunciated during start:a. APU CONTROL MASTER .......................................................OFFb. APU........................................................................... Do not restartc. APU FAIL Checklist compete.

APU FUEL SOV FAIL

[Condition: Shutoff valve not in the commanded position.]1. APU. ......................................................................................Do not start2. APU FUEL SOV FAIL Checklist complete.

APU OIL HI TEMP

[Condition: Oil temperature operating limit exceeded.]1. APU OIL HI TEMP Checklist complete, and

* Accomplish “APU FAULT” checklist, page 10.

APU OIL LO PRESS

[Condition: Oil pressure is below the minimum operating limit.]1. APU OIL LO PRESS Checklist complete, and

* Accomplish “APU FAULT” checklist, page 10.

APU FAULT

[Condition: Abnormal EICAS APU EGT indication may be displayed.]1. If abnormal EGT indication is displayed:

a. APU BLEED ................................................................. PUSH OUTWait 1 minute.b. If abnormal indication remains:

(1) APU EMER STOP .................................................. PUSH IN(2) APU CONTROL MASTER ..............................................OFF(3) APU FAULT Checklist complete.If abnormal indication does not remain:(1) APU..................................................Turn OFF if not required(2) APU FAULT Checklist complete.

If abnormal EGT indication is not displayed:a. APU...........................................................Turn OFF if not requiredb. APU FAULT Checklist complete.

or

oror


AP PITCH MISTRIM

[Condition: Pitch trim and autopilot commanding pitch trim, control in opposite directions.]

1. Control Wheel........................................................................Hold Firmly2. AP/TRIM DISC ...............................................................................Press3. Pitch Trim............................................................................. As Required4. Autopilot............................................................................... As Required5. AP PITCH MISTRIM Checklist complete.

AP PITCH TRIM FAIL

[Condition: Autopilot stabilizer trim no longer operative.]1. Control Wheel........................................................................Hold Firmly2. AP/TRIM DISC ...............................................................................Press3. Pitch Trim............................................................................. As Required4. AP PITCH TRIM FAIL Checklist complete.

AP ROLL MISTRIM

[Condition: Roll trim and autopilot commanding roll trim, control in opposite directions.]

1. Roll Trim ..............................................................................As Required2. AP ROLL MISTRIM Checklist complete.

AP FAIL

[Condition: Autopilot no longer operative.]1. Fly aircraft manually. 2. AP FAIL Checklist complete.

FD LATERAL MODE OFF

[Condition: Disconnection of the lateral mode due to invalid conditions.]1. Flight Director Lateral Mode ..........................................................Select2. FD LATERAL MODE OFF Checklist complete.

FD VERTICAL MODE OFF

[Condition: Disconnection of the vertical mode due to invalid conditions.]1. Flight Director Vertical Mode .........................................................Select2. FD VERTICAL MODE OFF Checklist complete.

AT FAIL

[Condition: Both autothrottles failed. Selected autothrottle not available.]1. Operate thrust levers manually.2. AT FAIL Checklist complete.


BATT DISCHARGING

[Condition: Batteries are discharging in an electrical emergency with no RAT assistance, or on ground when the battery is the only power source supplying the aircraft.]

1. Land at the nearest suitable airport.2. BATT DISCHARGING Checklist complete, and


BATT 1-2 OFF

[Condition: Battery #1 and #2 isolated from the electrical network.]1. Land at the nearest suitable airport.2. Consideration:

• APU start is not available.3. BATT 1-2 OFF Checklist complete, and


EMER LT BATT FAULT

[Condition: Emergency Light Battery fault detected.]1. Do not takeoff.

GPU CONNECTED

[Condition: AC or DC GPU connected and parking brake released.]Before taxi:

1. GPU....................................................................................... Disconnect2. GPU CONNECTED Checklist complete.

TRU (1 or 2) FAIL

[Condition: TRU failure detected.]1. Associated TRU ............................................................OFF then AUTO2. If TRU (1 or 2) FAIL remains annunciated:

a. Associated TRU .......................................................................OFFb. TRU (1 or 2) FAIL Checklist complete.If TRU (1 or 2) FAIL does not remain annunciated:a. TRU (1 or 2) FAIL Checklist complete.

TRU ESS FAIL

[Condition: TRU failure detected.]1. TRU ESS..........................................................................................OFF2. TRU ESS FAIL Checklist complete.

or


ELEC EMERGENCY

[Condition: AC main buses de-energized.]1. Airspeed ........................................................................... 130 KIAS MIN2. APU ............................................................................................. START3. IDG 1 ............................................................ Rotate to OFF then AUTO4. IDG 2 ............................................................. Rotate to OFF then AUTO5. EMER LT ..........................................................................................OFF6. If ELEC EMERGENCY remains annunciated:

a. If BATT DISCHARGING is displayed:(1) RAT Manual Deploy Lever ............................................PULL(2) TRU 1...................................................................Select OFF(3) TRU 2...................................................................Select OFF

* Proceed to step 7.If BATT DISCHARGING is not displayed:

* Proceed to step 7.If ELEC EMERGENCY does not remain annunciated:a. FLIGHT CONTROLS MODE (all) .....................PUSH IN then OUT

(ELEVATORS, RUDDER, SPOILERS)b. Go to step 10.

7. Icing Conditions ..............................................................................Avoid8. Altitude........................... 10,000 ft. or safe altitude (whichever is higher)9. The following components are inoperative:

10. ELEC EMERGENCY Checklist complete, and* Land at the nearest suitable airport.* Establish and communicate a plan.* Accomplish “RAT Deployed Descent Checklist” and “RAT

Deployed Landing Checklist,” page 21.

ADS 1 & 2 AOA Limit FunctionAutopilot CCD 2Autothrottles Flight Director 1 & 2Engine 1 & Engine 2 Reversers FMS 1Fuel AC Pump 1 Ground Spoilers L1, R1, L2, R2GPS 1 IRS 2Ice Detectors 1 & 2 Nosewheel SteeringMCDU 1 PFD 1MFD 2 Radio Altimeters 1 & 2MFS L3, R3, L4, R4, L5, R5 TAT 1 & 2NAVCOM 2 Windshield Wipers 1 & 2Pack 1 & 2 Windshield Heaters 1 & 2Speedbrake WX RadarTCAS Yaw DamperWindshear Detection

oror


AC BUS 1 OFF

[Condition: AC BUS 1 de-energized.]

1. The following components are inoperative:

2. Considerations:• Fuel XFEED LOW 2 is not available. • SLATS will operate at low rate (half speed).

3. If flying in icing conditions:a. ICE PROTECTION MODE.........................................................ONTwo (2) minutes after exiting icing conditions:b. ICE PROTECTION MODE.................................................... AUTOc. AC BUS 1 OFF Checklist complete.If not flying in icing conditions:a. AC BUS 1 OFF Checklist complete.

AC BUS 2 OFF

[Condition: AC BUS 2 de-energized.]


2. Consideration:• FLAPS will operate at low rate (half speed).

3. If flying in icing conditions:a. ICE PROTECTION MODE.........................................................ONTwo (2) minutes after exiting icing conditions:b. ICE PROTECTION MODE.................................................... AUTOc. AC BUS 2 OFF Checklist complete.If not flying in icing conditions:a. AC BUS 2 OFF Checklist complete.

BATT 1 OFF

[Condition: BATT 1 isolated from electrical system.]1. BATT 1 ...............................................................................................ON2. Consideration:

• If BATT 1 is off, APU start is not available.3. BATT 1 OFF Checklist complete.

AC Fuel Pump 1 Windshield Heater 2Ice Detector 1 Windshield Wiper 2Hydraulic System 2 Electric Pump

Hydraulic System 1 Electric Pump Ice Detector 2Hydraulic System 3 Electric Pump B Windshield Heater 1Windshield Wiper 1

or

or


AC ESS BUS OFF

[Condition: AC ESS BUS de-energized.]1. TRU ESS ..........................................................................................OFF2. The following components are inoperative:

3. Considerations:• Fuel XFEED LOW 1 is not available.• SLATS/FLAPS will operate at low rate (half speed).

4. AC ESS BUS OFF Checklist complete.

AC STBY BUS OFF

[Condition: AC STBY BUS de-energized.]1. Electrical Systems .......................................................................Monitor2. The following components are inoperative:

3. Consideration:• Engine start with batteries only is not available.

4. AC STBY BUS OFF Checklist complete.

APU GEN OFF BUS

[Condition: APU generator failure or APU GEN switch pushed out.]1. APU GEN .................................................................PUSH OUT then IN2. If APU GEN OFF BUS remains annunciated:

a. APU GEN ..................................................................... PUSH OUTb. APU GEN OFF BUS Checklist complete.If APU GEN OFF BUS does not remain annunciated:a. APU GEN OFF BUS Checklist complete.

BATT (1 or 2) DISCHARGING

[Condition: Associated battery discharging due to EPGDS (Electrical Power Generation and Distribution System) automation failure, or the battery is the only source supplying the system.]

1. Associated TRU.............................................................OFF then AUTO2. If BATT (1 or 2) DISCHARGING remains annunciated:

a. TRU (1 or 2)..............................................................................OFFb. BATT (1 or 2) DISCHARGING Checklist complete.If BATT (1 or 2) DISCHARGING does not remain annunciated:a. BATT (1 or 2) DISCHARGING Checklist complete.

AC Fuel Pump 2 Hydraulic System 3 Electric Pump A

Ignitions 1A & 2A

or

or


BATT 2 OFF

[Condition: BATT 2 isolated from the electrical system.]1. BATT 2 .......................................................................................... AUTO2. BATT 2 OFF Checklist complete.

DC BUS 1 OFF

[Condition: DC BUS 1 isolated from the electrical system.]1. Autothrottles ...........................................................................Disengage2. EMER LT ..........................................................................................OFF3. Altitude ............................................................................. 31,000 ft. max4. The following components are inoperative:

5. Considerations:• SLATS/FLAPS will operate at low rate (half speed).• Perform a Flaps FULL landing.• Arm the EMER LT on final.• Multiply the Unfactored Landing Distance on page 92 by 1.15.

6. DC BUS 1 OFF Checklist complete.

Hydraulic System 2 Electric Pump PTUThrust Reverser 1 Windshield Heater 2Engine 1 Autothrottle Weather RadarPack 1 Windshield Wiper 2ADS 1 AutopilotMFD 2 PFD 1CCD 2 MCDU 1MFS L5 + R5 Radio Altimeter 1


DC BUS 2 OFF

[Condition: DC BUS 2 de-energized.]1. Autothrottles ...........................................................................Disengage2. Altitude.............................................................................. 31,000 ft. max3. The following components are inoperative:

4. Considerations:• Perform a Flaps FULL landing.• Steer the aircraft on the ground using differential braking and rudder.• Multiply the Unfactored Landing Distance on page 92 by 1.20.

5. DC BUS 2 OFF Checklist complete.

PFD 2 ADS 2Transponder 2 NAVCOM 2Engine Vibration Indications Pedal Adjustment SwitchTCAS Radio Altimeter 2Engine 2 Thrust Reverser SpeedbrakesHydraulic System 1 Electric Pump Roll TrimHydraulic System 3 Electric Pump B Nosewheel SteeringWindshield Wiper 1 Autothrottle 2Windshield Heater 1 Pack 2Multi Function Spoilers L3, L4, R3, R4


DC ESS BUS 1 OFF

[Condition: DC ESS BUS 1 de-energized.]1. Icing Conditions.............................................................................. Avoid2. BATT 1 .............................................................................................OFF3. Land at the nearest suitable airport.4. The following components are inoperative:

5. SPOILER FAULT Checklist ....................................... Do not accomplish6. Considerations:

• Compass internal light will be inoperative.• FADEC will set flight idle on the ground.• FLAPS will operate at low rate (half speed).• Engine 2 windmill start is not available.• Thrust reversers, ground spoilers, wing anti-ice and ground idle may not

be available.• Expect lower (slower) roll rates and speedbrake efficiency.• Perform a Flaps FULL landing.• Multiply the Unfactored Landing Distance on page 92 by 1.70.• Apply the emergency/parking monitoring the parking brake light. When

the emergency/parking light is on, maintain steady pressure since anti-skid protection is not available.

7. DC ESS BUS 1 OFF Checklist complete, and* Establish and communicate a plan.

NAV/COM 1 Fwd. LAV Smoke DetectionDAP 1 Ignition 1A & 2AEICAS ADS 1Master Caution 1 Start Valve 1Transponder 1 MFS Panel L5, R5Hydraulic System 2 Depress. Valve Outboard BrakesRAT Automatic Deployment APUOil Pressure Indicator 1 Fuel Quantity Indicator 1Hydraulic System 3 Electric Pump A


DC ESS BUS 2 OFF

[Condition: DC ESS BUS 2 de-energized.]1. Icing Conditions ..............................................................................Avoid2. BATT 2..............................................................................................OFF3. Land at the nearest suitable airport.4. The following components are inoperative:

5. SPOILER FAULT Checklist ....................................... Do not accomplish6. APU MASTER ..................................................................................OFF7. Considerations:

• FADEC will set flight idle on the ground. • SLATS will operate at low rate (half speed).• Engine 1 windmill start is not available.• Perform a Flaps FULL landing.• Multiply the Unfactored Landing Distance on page 92 by 1.80.• Apply the emergency/parking monitoring the parking brake light. When

the emergency/parking light is on, maintain steady pressure since anti-skid protection is not available.

• On ground, use differential braking and rudder to steer the aircraft. Thrust reversers, steering, ground spoilers, wing anti-ice and ground idle may not be available.

8. DC ESS BUS 2 OFF Checklist complete, and* Establish and communicate a plan.

DAP 2 Inboard BrakesMFD 1 CCD 1ELT Master Warning/Caution 2ADS 3 & ADS Standby Aural Warning 2Hydraulic System 1 Depress. Valve Fuel Quantity 2AFT LAV Smoke Detection DC Fuel PumpAPU Fire Detection Thrust Reversers 1 & 2APU Fire Extinguishing ENG 2 Oil Pressure IndicationAPU Fuel SOV IESSENG 2 Start Valve Fuel Xfeed OperationMFS Panel L3, R3, L4, R4 TCASMCDU 2


DC ESS BUS 3 OFF

[Condition: DC ESS BUS 3 de-energized.]1. TRU ESS..........................................................................................OFF2. If DC ESS BUS 3 OFF remains annunciated:

a. The following components are inoperative:

b. Consideration:• FLAPS will operate at low rate (half speed).

c. APU MASTER..........................................................................OFFd. DC ESS BUS 3 OFF Checklist complete.If DC ESS BUS 3 OFF does not remain annunciated:a. DC ESS BUS 3 OFF Checklist complete.

IDG (1 or 2) OFF BUS

[Condition: IDG (1 or 2) failure or IDG (1 or 2) in OFF position.]1. Associated IDG .............................................................OFF then AUTO2. If IDG (1 or 2) OFF BUS remains annunciated:

a. Associated IDG ........................................................................OFFb. APU............................................................................. As Requiredc. IDG (1 or 2) OFF BUS Checklist complete.If IDG (1 or 2) OFF BUS does not remain annunciated:a. IDG (1 or 2) OFF BUS Checklist complete.

IDG (1 or 2) OIL

[Condition: High oil temperature or low oil pressure detected. Affected IDG light becomes amber.]

1. IDG #___........................Confirm ................................................... DISC

2. IDG (1 or 2) OIL Checklist complete.

Radio Altimeter 3 Fuel Crossfeed ValvePassenger Address Cargo Compartments Fire BottlesADS 2 Internal Lights of all SwitchesRudder Trim Landing Gear Override SwitchFIREX Switches Cockpit Dome Lights

or

or

Once disconnected, the IDG cannot be reset in flight.


RAT Deployed Descent Checklist

1. Approach considerations:• Plan on a Flap 3 landing.• Multiply the Unfactored Landing Distance on page 92 by 2.10.

2. GND PROX FLAP OVRD ......................................................... PUSH IN3. Shoulder Harness...................... Verify...............................................On4. FSTN BELTS ..................................................................................... ON5. Altimeters................................... Verify..................................... __.__Set6. Landing Data ............................. Verify.............................................. Set

a. Set VREF FULL + 20 KIAS or 130 KIAS (whichever is higher).7. EICAS........................................................................................Checked8. Approach Briefing .................................................................... Complete9. RAT Deployed Descent Checklist complete.

RAT Deployed Landing Checklist

1. EICAS........................................................................................Checked2. EMER LT ....................................................................................ARMED3. Landing Gear............................. Verify............................Down, 3 Green

4. Flaps.......................................... Verify..................................................35. RAT Deployed Landing Checklist complete.

* This is an NTSB Reportable Event.


Dual Engine Failure Descent Checklist

1. Approach consideration:• Plan on a Flap 3 landing.

2. Flight Attendants ............................................................................Notify3. ATC ................................................................................................Notify4. Transponder .................................................................................... 77005. Aural Warning CBs (C7 and C31) .................................................. PULL6. GND PROX FLAP OVRD......................................................... PUSH IN7. Shoulder Harness.......................Verify .............................................. On8. FSTN BELTS......................................................................................ON9. Altimeters ...................................Verify .....................................__.__Set

10. Landing Data ............................. Verify...............................................Seta. Set VREF FULL + 20 KIAS or 130 KIAS (whichever is higher).

11. Approach Briefing.....................................................................Complete12. Landing consideration:

• For a ditching, plan on gear up.

At 10,000 ft. and below:13. PRESSURIZATION DUMP .................................................. PUSH OUT14. If depressurized and ditching is required:

a. PRESSURIZATION MODE ..................................................... MANb. CABIN ALT................................................DOWN (for 50 seconds)c. Dual Engine Failure Descent Checklist complete.If depressurized and ditching is not required:a. Dual Engine Failure Descent Checklist complete.

Dual Engine Failure Landing Checklist

1. EMER LT .................................................................................... ARMED2. Landing Gear..............................Verify .......................Down, 3 Green or

Up (if ditching)Note: Alternate gear extension may be required.

3. Flaps..................................................................................Max Available4. Airspeed ........................................................................... 130 KIAS MIN5. APU EMER STOP.................................................................... PUSH IN6. Dual Engine Failure Landing Checklist complete, and

* Below 1,000 feet AGL, advise on PA “Brace, brace.”* When required, accomplish “Evacuation,” page ii.* This is an NTSB Reportable Event.

or


ENG (1 or 2) REV DEPLOYED

[Condition: Thrust reverser deployed unexpectedly or not stowed when commanded to stow. Reverse position undetermined. REV icon displayed above the associated ITT indicator.]

1. Autothrottles ...........................................................................Disengage2. #__Thrust Lever ........................ Confirm ........................................ IDLE3. If buffeting is noticed:

a. #__START/STOP ........................... Confirm ......................... STOPb. APU (if available)................................................................. STARTc. Fuel.....................................................................................Balanced. Land at the nearest suitable airport.e. ENG (1 or 2) REV DEPLOYED Checklist complete, and

* Establish and communicate a plan.* Accomplish “Engine Out Descent Checklist” and “Engine Out

Landing Checklist”, page 25.If buffeting is not noticed:a. Land at the nearest suitable airport.b. ENG (1 or 2) REV DEPLOYED Checklist complete, and


Landing Checklist”, page 25.

ENG (1 or 2) CONTROL FAULT

[Condition: Pilot unable to modulate thrust, OBV (Operability Bleed Valve) failed open or engine responds slowly.]

1. Autothrottles ...........................................................................Disengage2. If engine thrust is controllable:

a. ENG (1 or 2) CONTROL FAULT Checklist complete.If engine thrust is not controllable:a. ENG (1 or 2) CONTROL FAULT Checklist complete, and

* Accomplish “Precautionary Engine Shutdown” procedure, page 26.

ENG (1 or 2) FADEC OVERTEMP

[Condition: FADEC overtemperature detected.]1. If engine parameters are normal:

a. ENG (1 or 2) FADEC OVERTEMP Checklist complete.If engine parameters are not normala. ENG (1 or 2) FADEC OVERTEMP Checklist complete, and

* Accomplish “Precautionary Engine Shutdown” procedure, page 26.

or

Avoid thrust reverser use, rapid thrust lever movement and high thrust operation.

or

or


ENG (1 or 2) FAIL

[Condition: Unexpected engine shutdown occurred. EICAS: FAIL icon in center of the N1 gauge. Oil pressure indication displaying red.]

1. Autothrottles ...........................................................................Disengage2. #__Thrust Lever .........................Confirm....................................... IDLE3. If engine did autorelight:

a. Monitor engine parameters.Note: After an engine airstart, if flight conditions permit, operate

the engine at idle for 2 minutes prior to high thrust operation.

b. ENG (1 or 2) FAIL Checklist complete, and* Establish and communicate a plan.

If engine did not autorelight:a. #__START/STOP ........................... Confirm......................... STOPb. APU (if available) .................................................................STARTc. Fuel .................................................................................... Balanced. If fuel leak is suspected:

(1) FUEL XFEED..................................................................OFF(2) If leak is on the RH tank:

(a) APU.......................................................................OFF(b) Go to Step 4.If leak is not on the RH tank:(a) APU.......................................................... As Required(b) Go to Step 4.

If fuel leak is not suspected:(1) Go to Step 4.

4. If engine airstart is required or considered:a. ENG (1 or 2) FAIL Checklist complete, and

* Establish and communicate a plan.* Accomplish “Engine Airstart” procedure, page 32.

If engine airstart is not required or considered:a. ENG (1 or 2) FAIL Checklist complete, and


Landing Checklist”, page 25.* If required, accomplish “Driftdown”, page 29.

or

oror

or


Engine Out Descent Checklist

1. Approach considerations:• Multiply the Unfactored Landing Distance on page 92 by 1.50.• Use SLAT/FLAP 5 for landing; Set VREF FULL + 20 KIAS.• If RAT deployed use SLAT/FLAP 3 only; Set VREF FULL + 20 KIAS.

2. Shoulder Harness...................... Verify...............................................On3. FSTN BELTS ..................................................................................... ON4. Altimeters................................... Verify.................................... .__.__Set5. Landing Data ............................. Verify.............................................. Set6. EICAS........................................................................................Checked7. Approach Briefing .................................................................... Complete8. Go Around Considerations:

• Simultaneously press TOGA and ensure thrust lever in TOGA detent and verify thrust setting.

• Rotate to FD commands and/or go around attitude of 8° nose up. • Select FLAPS 2, Positive Rate, Gear UP, maintain VAC and limit bank

angle to 15°.• Climb straight ahead to 500 ft. AGL or follow “Engine Failure - Missed

Approach” procedure if published.• Above 400 ft. select HDG or FMS NAV.• Climbing through engine out acceleration altitude select FLCH, VFS.• Retract flaps on flap retraction schedule.

9. Engine Out Descent Checklist complete.

Engine Out Landing Checklist

1. Landing consideration:• During landing only operative engine thrust reverser is available.

2. EICAS........................................................................................Checked3. Landing Gear.............................Verify ........................DOWN, 3 GREEN

4. FLAPS......................................Verify ....................................................53 (if RAT deployed)

5. FUEL XFEED ...................................................................................OFF6. Engine Out Landing Checklist complete.


Precautionary Engine Shutdown

1. Autothrottles ...........................................................................Disengage2. #__Thrust Lever .........................Confirm........................................ IDLE3. #__START/STOP .......................Confirm...................................... STOP

4. Engine Thrust (remaining engine) ....................................... As Required5. APU (if available)..........................................................................START6. Fuel Balance ....................................................................... As Required7. Land at the nearest suitable airport.8. Precautionary Engine Shutdown Checklist complete, and


Landing Checklist”, page 25.* If required, accomplish “Driftdown”, page 29.

ENG (1 or 2) FUEL IMP BYPASS

[Condition: Fuel filter impending bypass.]1. If both engines are affected:

a. Land at the nearest suitable airport.b. ENG (1 or 2) FUEL IMP BYPASS Checklist complete.

* Establish and communicate a plan.If one engine affected:a. Monitor engine and fuel systems.b. ENG (1 or 2) FUEL IMP BYPASS Checklist complete.

ENG (1 or 2) FUEL LO PRESS

[Condition: Fuel pressure low. Backup fuel pump activated.]1. FUEL XFEED ...................................................................................OFF2. Autothrottles ...........................................................................Disengage3. #__Thrust Lever .........................Confirm........................................ IDLE4. Altitude ............................................................................. 25,000 ft. max5. Consideration:

• If thrust lever is set above idle, ENG (1 or 2) FUEL LO PRESS message may return.

6. If fuel leak is suspected:a. ENG (1 or 2) FUEL LO PRESS Checklist complete, and

* Accomplish “Fuel Leak” procedure, page 57..If fuel leak is not suspected:a. ENG (1 or 2) FUEL LO PRESS Checklist complete.

If the engine does not shutdown, PULL do not rotate the associated FIRE EXTINGUISHING HANDLE.

or

or


Engine Abnormal Vibration

[Condition: Engine vibration indication becomes amber.]1. Autothrottles ...........................................................................Disengage2. If vibration is due to ice accumulation:

a. #__Thrust Lever ............................. Confirm ........................... IDLEthen advance to 70% N1 min.

Wait 30 seconds.b. #__Thrust Lever .......................................................... As Requiredc. Engine Abnormal Vibration Checklist complete.If vibration is not due to ice accumulation:a. #__Thrust Lever ................................................................. Reduceb. If able to maintain vibration and/or engine parameters within

operating limits:(1) Engine Abnormal Vibration Checklist complete.If not able to maintain vibration and/or engine parameters within operating limits:(1) Engine Abnormal Vibration Checklist complete, and

* Establish and communicate a plan.* Accomplish “Precautionary Engine Shutdown”

procedure, page 26.

Volcanic Ash Encounter

Accomplish the following while making a 180° turn:1. ATC.................................................................................................Notify2. Autothrottles ...........................................................................Disengage3. Thrust (altitude permitting)............................................. Reduce to IDLE

[This reduces ash ingestion, maximizes engine surge margin and lowers engine turbine temperature.]

4. Oxygen Masks......................................................................... ON/100%5. Cabin Crew.....................................................................................Notify6. Passenger Oxygen ..............................................................As Required7. ICE PROTECTION MODE ................................................................ ON8. APU ............................................................................................. START9. ENGINE PARAMETERS .............................................................Monitor

10. Airspeed Indications ....................................................................Monitor11. Volcanic Ash Encounter Checklist complete, and


or

or


ENG (1 or 2) FUEL SOV FAIL

[Condition: Associated shutoff valve not in commanded position.]1. If Fire Handle is pulled:

a. Associated FUEL AC PUMP ....................................................OFFb. FUEL XFEED ...........................................................................OFFc. ENG (1 or 2) FUEL SOV FAIL Checklist complete.If Fire Handle is not pulled:a. ENG (1 or 2) FUEL SOV FAIL Checklist complete.

Engine ITT Overtemperature

[Condition: ITT pointer and digits flashing red.]1. Autothrottles ...........................................................................Disengage2. #__Thrust Lever .........................Confirm....................................Reduce3. If able to maintain ITT within limits with reduced thrust:

a. Engine ITT Overtemperature Checklist complete.If not able to maintain ITT within limits with reduced thrust:b. Engine ITT Overtemperature Checklist complete, and

* Establish and communicate a plan.* Accomplish “Precautionary Engine Shutdown” procedure,

page 26.

ENG (1 or 2) OIL LO PRESS

[Condition: Low oil pressure detected. Amber oil pressure indication.]1. Oil Pressure Indication ..................................................................Check2. If oil pressure indication is normal:

a. Engine Indications............................................................... Monitorb. ENG (1 or 2) OIL LO PRESS Checklist complete.If oil pressure indication is not normal:a. ENG (1 or 2) OIL LO PRESS Checklist complete, and


page 26.

ENG (1 or 2) REV TLA FAIL

[Condition: Associated thrust reverser solenoid protection failed.]1. Do not move thrust levers below idle.2. Consideration:

• Thrust reverser (affected engine) is not available.3. ENG (1 or 2) REV TLA FAIL Checklist complete.

ENG TLA NOT TOGA

[Condition: TLA not at TOGA position during takeoff and/or go-around.]1. Thrust Levers ...................................................................TOGA position2. ENG TLA NOT TOGA Checklist complete.

or

or

or


Driftdown

[Condition: Engine failure during cruise when descent to lower altitude becomes necessary.]

CRUISE ALTITUDE - CONFIGURATION - CLEAN

1. Autothrottles .....................................................................................OFF2. Max. ContinuoUs Thrust.................................................................... Set3. SPD on GP .................................................. Set SPD from Tables below

a. Enter the weight row (Start Driftdown) and proceed to the appropriate speed (Initial Driftdown Speed).

4. ALT SEL ....................... Set Gross Level-Off Altitude from Tables belowa. Enter the weight row (Start of Driftdown) and proceed to the

appropriate ISA deviation column to determine the Gross Level-Off Altitude.

5. FLCH ............................................................................................Select

6. Driftdown Checklist complete.

o

oLRC CRUISE

TERRAIN CRITICAL

DRIFTDOWN SPEED

LEVEL OFF

ENGINE LOSSMAX CONT THRUST

DRIFTDOWN TABLE

EMBRAER 170 – CF34-8E5 ENGINES – FAA CERTIFICATION

BLEEDS ON/ENGINE & WING ANTI-ICE OFF

WEIGHT (lb) INITIAL GROSS LEVEL OFF ALTITUDE - FT

DRIFTDOWN (NET LEVEL OFF ALTITUDE - FT)

START SPEED ISA+10°C

DRIFTDOWN LEVEL OFF (KIAS) & BELOW

ISA +15°C ISA+20°C

20000 19600 18600 79000 75400 199

(15100) (14400) (13000)

21300 21000 20200 75000 72000 194

(17000) (16400) (15100)

22700 22400 21900 71000 68400 188

(18600) (18200) (17000)

24100 24000 23400 67000 64600 183

(20100) (19900) (19000)

25700 25600 25000 63000 60900 178

(21700) (21500) (20900)

27300 27200 26700 59000 57100 172

(23300) (23200) (22700)

28900 28900 28400 55000 53300 166

(25100) (25000) (24600)

30700 30700 30300 51000 49500 160

(26900) (26900) (26500)

DRIFTDOWN TABLE

EMBRAER 170 – CF34-8E5 ENGINES – FAA CERTIFICATION

BLEEDS ON/ENGINE & WING ANTI-ICE ON

WEIGHT (lb) INITIAL GROSS LEVEL OFF ALTITUDE - FT

DRIFTDOWN (NET LEVEL OFF ALTITUDE - FT)

START SPEED ISA-8°C

DRIFTDOWN LEVEL OFF (KIAS) & BELOW

ISA ISA+10°C

19700 19600 18000 79000 75400 198

(14900) (14700) (12600)

20900 20800 19400 75000 72200 194

(16800) (16600) (14700)

22200 22200 20800 71000 68500 188

(18400) (18200) (16500)

23600 23600 22300 67000 64700 183

(19800) (19700) (18200)

25100 25000 23800 63000 61000 178

(21300) (21300) (19900)

26600 26300 25300 59000 57100 172

(22900) (22900) (21600)

28300 27500 26500 55000 53400 166

(24600) (24600) (23400)

30100 29000 27800 51000 49600 160

(26300) (26100) (25100)


ENG (1 or 2) START VLV OPEN

[Condition: Start valve not closed while engine running.]1. XBLEED ............................................................................... PUSH OUT2. Associated BLEED............................................................... PUSH OUT3. If during start:

a. If ENG 1 START VLV OPEN is annunciated:(1) APU BLEED (if applicable) ................................. PUSH OUT(2) #1 Thrust Lever.............................................................. IDLE(3) #1 START/STOP.......................................................... STOP(4) ENG (1 or 2) START VLV OPEN Checklist complete.If ENG 2 START VLV OPEN is annunciated:(1) Engine start ground cart............................................Remove(2) #2 Thrust Lever.............................................................. IDLE(3) #2 START/STOP.......................................................... STOP(4) ENG (1 or 2) START VLV OPEN Checklist complete.

If during flight:a. APU BLEED ................................................................. PUSH OUTb. Icing Conditions...................................................................... Avoidc. Altitude .....................................Max. 31,000 ft. or min safe altituded. Consideration:

• Inflight assisted starts are not possible for the affected engine.e. ENG (1 or 2) START VLV OPEN Checklist complete.

ENG (1 or 2) TLA FAIL

[Condition: Associated engine thrust control lost.]1. Thrust Rating...................................................Set to IDLE automatically2. ENG (1 or 2) TLA FAIL Checklist complete, and


Landing Checklist” procedure, page 25.

ENG (1 or 2) T2 HEAT FAIL

[Condition: Associated T2 heater failed.]1. Icing Conditions.............................................................................. Avoid2. ENG (1 or 2) T2 HEAT FAIL Checklist complete.

ENG (1 OR 2) NO DISPATCH

1. Do not takeoff.

ENG (1 OR 2) OIL LO LEVEL

1. Do not takeoff.

ENG 1 (2) REV FAIL

1. Do not takeoff.

or

or


ENG 1 (2) REV PROT FAULT

1. Do not takeoff.

ENG EXCEEDANCE

1. Do not takeoff.

ENG THR RATING DISAG

1. Do not takeoff.

ENG NO TAKEOFF DATA

[Condition: Takeoff data not entered successfully. Discrepancy between information entered in FMS for engine 1 and 2 detected.]

1. Takeoff Data Setting ..................................................... Enter or Reenter2. ENG NO TAKEOFF DATA Checklist complete.

ENG REF A-I DISAG

[Condition: Ice protection mode selector set to the ON position with OFF or ENG in the takeoff data set (TDS) menu.]

1. If takeoff data correct:a. Reconfigure the aircraft.b. ENG REF A-I DISAG Checklist complete.If aircraft configuration correct:a. Re-enter the takeoff data.b. ENG REF A-I DISAG Checklist complete.

ENG REF ECS DISAG

[Condition: Discrepancy between REF ECS input and actual ECS bleed configuration.]

Note: This message will always be displayed when the following conditions apply simultaneously:

• the REF ECS is set to ON,• the APU is running, and• the engine thrust levers are set to idle.

1. If takeoff data correct:a. Reconfigure the aircraft.b. ENG REF A-I DISAG Checklist complete.If aircraft configuration correct:a. Re-enter the takeoff data.b. ENG REF ECS DISAG Checklist complete.

or

or


Engine Airstart

1. Considerations:• Windmilling starts accomplished with residual ITT below 90°C are more

reliable. Start attempts outside of the airstart envelope are not assured. • After an engine airstart, if flight conditions permit, operate the engine at

idle for 2 min. prior to high thrust operations.2. Autothrottles ...........................................................................Disengage3. Airstart Envelope ..........................................................................Check

See “Engine Airstart Envelope” on page 33.4. If doing a windmilling airstart:

a. XBLEED ....................................................................... PUSH OUTb. APU BLEED (if engine 1 is affected)............................ PUSH OUTc. Inoperative engine N2 ...................................................... 7.2% mind. Inoperative engine IGNITION................................................OVRDe. Inoperative START/STOP ...................................START then RUN

(1) If windmilling airstart is successful:After engine stabilizes at idle:(a) XBLEED ........................................................ PUSH IN(b) IGNITION ........................................................... AUTO(c) FUEL ............................................................... Balance(d) Engine Airstart Checklist complete.Windmilling airstart not successful:(a) XBLEED ........................................................ PUSH IN(b) #__START/STOP ............Confirm...................... STOP(c) IGNITION ........................................................... AUTO(d) FUEL ............................................................... Balance(e) Engine Airstart Checklist complete, and

* Accomplish “Engine Out Descent Checklist” and “Engine Out Landing Checklist”, page 25.

If doing an assisted airstart:a. Operative Engine N2 ......................................................... 80% minb. Inoperative engine IGNITION................................................OVRDc. Inoperative START/STOP ...................................START then RUN

(1) If assisted airstart is successful:After engine stabilizes at idle:(a) IGNITION ........................................................... AUTO(b) Engine Airstart Checklist complete.If assisted airstart is not successful:(a) #__START/STOP ............Confirm...................... STOP(b) IGNITION ........................................................... AUTO(c) FUEL ............................................................... Balance(d) Engine Airstart Checklist complete, and

* Accomplish “Engine Out Descent Checklist” and “Engine Out Landing Checklist”, page 25.

or

or

or


Engine Airstart Envelope


APU FIRE DET FAIL

[Condition: APU fire detection system failed.]1. APU MASTER..................................................................................OFFNote: The message APU FIRE DET FAIL may appear just before the

message APU FIRE. 2. APU FIRE DET FAIL Checklist complete, and

* Accomplish “APU FIRE Checklist”, page vii if APU FIRE annunciates.

APU FIREX FAIL

[Condition: APU fire extinguisher failed.]1. APU MASTER .................................................................................OFF2. APU FIREX FAIL Checklist complete.

CRG (FWD or AFT) FIRE SYS FAIL

[Condition: All smoke detectors failed in the associated compartment, or pressure in any extinguisher bottle is low and the cartridges are intact, or any of the cartridge circuits are opened.]

1. If cargo compartment is empty:a. CRG (FWD or AFT) FIRE SYS FAIL Checklist complete.If cargo compartment is not empty:a. Land at the nearest suitable airport.b. CRG (FWD or AFT) FIRE SYS FAIL Checklist complete, and


ENG (1 OR 2) FIRE DET FAIL

[Condition: Engine fire detection system failed.]1. If fire is suspected:

a. ENG (1 or 2) FIRE DET FAIL Checklist complete, and* Accomplish “Engine Fire, Severe Damage, or Separation

Checklist”, page vi.If fire is not suspected:a. Engine Parameters ............................................................. Monitorb. ENG (1 or 2) FIRE DET FAIL Checklist complete.

or

or


Cargo Compartment Fire

[Condition: Fire in the cargo compartment with no EICAS warning message.]

Associated Cargo Compartment (FWD or AFT):1. Associated CARGO SMOKE.........................................................PUSH

After CRG (FWD or AFT) FIREX HI ARMED is annunciated and associated CARGO SMOKE Light illuminates:

2. Associated CARGO SMOKE............................................... PUSH again3. Associated CARGO SMOKE Light ..................................... Extinguishes4. CRG (FWD or AFT) FIREX LO ARM...................................Annunciates5. CRG (FWD or AFT) FIREX HI ARMED....Does not remain annunciated

Note: The low rate fire extinguishing bottle does not automatically discharge on the ground, unless the pilot pushes the associated CARGO SMOKE once again.

Wait 1 minute.6. CRG (FWD or AFT) FIREX LO ARM........Does not remain annunciated7. Associated CARGO SMOKE Light ..................................... Extinguishes8. Land at the nearest suitable airport.9. Cargo Compartment Fire Checklist complete, and


ELEV NML MODE FAIL

[Condition: Elevator system normal mode inoperative.]1. FLIGHT CONTROL MODE ELEVATOR................................... PUSH IN2. ELEVATOR FAULT Procedure .................................. Do not accomplish3. The following components are inoperative:

4. Considerations:• Avoid side slipping the aircraft.• The stick shaker remains operative.

5. ELEV NML MODE FAIL Checklist complete.* This is an NTSB Reportable Event.

AOA Limit Auto Configuration TrimAutopilot Elevator Thrust Compensation


RUDDER NML MODE FAIL

[Condition: Rudder system normal mode inoperative.]1. FLIGHT CONTROL MODE RUDDER...................................... PUSH IN2. RUDDER FAULT Procedure ..................................... Do not accomplish3. The following components are inoperative:

4. RUDDER NML MODE FAIL Checklist complete.* This is an NTSB Reportable Event.

AOA LIMIT FAIL

[Condition: One or more sensors required to perform AOA Limiting function failed and function no longer available.]

1. Considerations:• Avoid side slipping the aircraft.• The stick shaker remains operative.

2. AOA LIMIT FAIL Checklist complete.

ELEV THR COMP FAIL

[Condition: One or more sensors required to perform Elevator Thrust Compensation function failed and function no longer available.]

1. Compensate manually any pitch tendency following thrust variations.2. ELEV THR COMP FAIL Checklist complete.

ELEVATOR FAULT

[Condition: Left and Right elevator system reverted to direct mode.]Note: If the SPOILER FAULT message is also displayed, accomplish the

Spoiler Fault procedure prior to this procedure.1. FLIGHT CONTROLS MODE ELEVATORS........PUSH IN, WAIT 10

SECONDS, then OUT2. If ELEVATOR FAULT remains annunciated:


b. Considerations:• Avoid side slipping the aircraft.• The stick shaker remains operative.

c. ELEVATOR FAULT Checklist complete.If ELEVATOR FAULT does not remain annunciated:a. Resume normal flight operations and report to maintenance.b. ELEVATOR FAULT Checklist complete.

Yaw Damper Turn Coordination

Auto Configuration Trim AOA LimitAutopilot Elevator Thrust Compensation

or


ELEVATOR (LH or RH) FAIL

[Condition: The associated elevator panel jammed. Remaining elevator forced in direct mode.]

1. Airspeed .................................................................................As follows:

2. ELEVATOR (LH or RH) FAIL Checklist complete, and* Establish and communicate a plan.* Accomplish “Pitch/Roll Malfunction Descent Checklist” and “Pitch/

Roll Malfunction Landing Checklist”, page 46.

FLT CTRL NO DISPATCH

1. Do not takeoff.

FLT CTRL FAULT

1. Do not takeoff.

If the failure occurs ___ 175 KIAS... Then maximum airspeed is...above the current airspeed

at or below 175 KIAS


(FLAP or SLAT) FAIL

[Condition: Flap or Slat malfunction.]1. Airspeed ..........................................Maintain for appropriate flap setting2. Flaps..................................................................Cycle (up to 3 attempts)

The objectives of the following steps are to determine:• what has failed (i.e., FLAP, SLAT or both)• when the failure occurs• what is the most FLAP and SLAT extension possible

Read steps a. through c. below entirely before accomplishing.a. Return the Flap lever to the previously selected position.b. Reselect desired Flap position.c. Determine the most extended SLAT or FLAP position prior to a

failure occurring.For example:

3. If (FLAP or SLAT) FAIL does not remain annunciated:a. (FLAP or SLAT) FAIL Checklist complete.If (FLAP or SLAT) FAIL remains annunciated:a. Consideration:

• Limit bank angle to 20° maximum.b. Using the last normal FLAP/SLAT position prior to a failure

occurring, determine the most extended FLAP/SLAT setting from the following table:For example:• If a SLAT FAIL occurs at 1, then

— the most extended SLAT setting is 0.By reading down the SLAT 0 column:

— the most extended FLAP setting is 2.— the Flap lever is set to 2.— the Max Speed (KIAS) is 215 KIAS.— the VREF (KIAS) IS VREF FULL + 40.— the Ldg Coef is 1.82.

• If a FLAP FAIL occurs at 2, then

— the most extended FLAP setting is 1.By reading across the FLAP 1 row:

— the most extended SLAT setting is FULL.— the Flap lever is set to FULL.— the Max Speed (KIAS) is 180 KIAS.— the VREF (KIAS) IS VREF FULL + 35.— the Ldg Coef is 2.00.

Cont’d

When selecting the flap lever to 1, if a ___ failure occurs...

then the most extended...

FLAP FLAP position is 0.SLAT SLAT position is 0.

or


c. (FLAP or SLAT) FAIL Checklist complete, and* Establish and communicate a plan.* Accomplish “FLAP/SLAT FAIL Descent Checklist” and “FLAP/

SLAT FAIL Landing Checklist”, page 39.

FLAP/SLAT FAIL Descent Checklist

1. Approach Considerations:• Extend pattern to ensure a long, straight final approach.• Establish landing configuration early.

2. Determine the landing distance by multiplying the Unfactored Landing Distance on page 92 by the appropriate Ldg. Coef. from the table above.

3. Shoulder Harness...................... Verify...............................................On4. FSTN BELTS ..................................................................................... ON5. Altimeters................................... Verify..................................... __.__Set6. Landing Data ............................. Verify........ Applicable VREF (KIAS) Set

from the table above7. EICAS........................................................................................Checked8. GND PROX FLAP OVRD ...................................PUSH IN (if applicable)9. Approach Briefing .................................................................... Complete

10. FLAP/SLAT FAIL Descent Checklist complete.

FLAP/SLAT FAIL Landing Checklist

1. EICAS........................................................................................Checked2. Landing Gear............................. Verify............................Down, 3 Green

3. Flaps.......................................... Verify..... ___ (Max extension possible)4. FLAP/SLAT FAIL Landing Checklist complete.

SLAT

FLAP 0 1, 2, 3 4, 5, FULL

0 Max Speed (KIAS)VREF (KIAS)

Ldg Coef

VMO/MMOVREF FULL+ 60

2.41

230 KIASVREF FULL+ 65

2.48


2.49


Ldg Coef


2.12


1.97


2.00


Ldg Coef


1.82


1.55


1.57


Ldg Coef

Notusable


1.42


1.43

4, 5 Max Speed (KIAS)VREF (KIAS)

Ldg Coef


1.31


1.29

FULL Max Speed (KIAS)VREF (KIAS)

Ldg Coef


1.22

165 KIASVREF FULL

NOT APPLICABLE


PITCH TRIM FAIL

[Condition: Both HS-ACE (Horizontal Stabilizer Actuator Control Electronics) channels inoperative and pitch trim function no longer available.


2. PITCH TRIM 1 and PITCH TRIM 2 CUTOUT ..........PUSH IN then OUT3. PITCH TRIM................................................................................Actuate4. If Pitch Trim is normal:

a. Continue normal operations and report to maintenance.b. PITCH TRIM FAIL Checklist complete.If Pitch Trim is not normal:a. PITCH TRIM SYS 1 and 2 CUTOUT................................ PUSH IN

Additional pitch trim is not available.b. PITCH TRIM FAIL Checklist complete, and

* Establish and communicate a plan.* Accomplish “Pitch/Roll Malfunction Descent Checklist” and

“Pitch/Roll Malfunction Landing Checklist”, page 46.

RUDDER FAULT

[Condition: Rudder control system reverted to direct mode.]Note: If the SPOILER FAULT message is also displayed, accomplish the

Spoiler Fault procedure prior to this procedure.1. FLIGHT CONTROLS MODE RUDDER...... ..............PUSH IN, WAIT 10

SECONDS, then OUT2. If RUDDER FAULT remains annunciated:


b. RUDDER FAULT Checklist complete.If RUDDER FAULT does not remain annunciated:a. Continue normal operations and report to maintenance.b. RUDDER FAULT Checklist complete.c. This is an NTSB Reportable Event.



Yaw Damper Turn Coordination

or

or


RUDDER FAIL

[Condition: Active/standby rudder channels failed or rudder jammed.


2. Land at the nearest suitable airport.3. Considerations:

• Perform a Flaps FULL landing. • Avoid landing with a crosswind above 10 kts.• If a go around is required, proceed as a normal go around limiting the

approach climb speed to 175 KIAS.• Asymmetric thrust may be required.• Maximum thrust on both engines may not be possible.


5. RUDDER FAIL Checklist complete, and* Establish and communicate a plan.* This is an NTSB Reportable Event.

RUDDER LIMITER FAIL

[Condition: Rudder authority (30°) retained in flight.]1. Abrupt rudder pedal and/or full rudder deflection ................Do not apply2. RUDDER LIMITER FAIL Checklist complete.

SHAKER ANTICIPATED

[Condition: Stall warning function inoperative.]1. Side slipping the aircraft .................................................................Avoid2. Airspeed ........................................................................ 0.5 MACH MAX

Use the lower previously selected SLAT/FLAP setting in relation to the current position as a reference to select the VREF minimum speed on final approach and the landing coefficient presented in the SLAT/FLAP FAIL procedure table on page 38.

3. SHAKER ANTICIPATED Checklist complete.

SLAT- FLAP LVR DISAG

[Condition: SLAT/FLAP surfaces not extending due to excessive airspeed. Flaps were commanded above VFE, RAT is only electrical source, FLAP/SLAT surface interlock occurred.]

1. FLAP Lever................................................... Return to previous position2. SLAT - FLAP LVR DISAG Checklist complete.



Yaw Damper Yaw TrimTurn Coordination


STALL PROT FAIL

[Condition: Stall Warning/Protection, Stick Shaker & AOA Limiting inoperative.]

1. Side slipping the aircraft ................................................................. Avoid2. STALL PROT FAIL Checklist complete, and

* Establish and communicate a plan.* Accomplish “Pitch/Roll Malfunction Descent Checklist” and “Pitch/

Roll Malfunction Landing Checklist”, page 46.

STALL PROT FAULT

1. Do not takeoff.

STAB LOCK FAULT

[Condition: Horizontal stabilizer may have a drift rate of up to 0.5 degrees per minute nose up or nose down.]

1. PITCH TRIM........................................................................ As Required2. Any PITCH TRIM System Cutout ........................................Do not press3. Land at the nearest suitable airport.4. STAB LOCK FAULT Checklist complete, and


SPOILER NML MODE FAIL

[Condition: Spoiler system normal mode inoperative.]1. SPD BRK.....................................................................................CLOSE2. FLIGHT CONTROLS MODE SPOILERS................................. PUSH IN3. SPOILER FAULT Procedure ..................................... Do not accomplish4. The following components are inoperative:

5. SPOILER NML MODE FAIL Checklist complete, and* Accomplish “Flight Control/Brake Malfunction Descent Checklist”

and “Flight Control/Brake Malfunction Landing Checklist”, page 45.

GROUND SPOILERS FAIL

[Condition: One or more ground spoilers extended inadvertently or failed to extend when commanded.]

1. Speed Brake................................................................................CLOSE2. GROUND SPOILERS FAIL Checklist complete, and

* Accomplish “Flight Control/Brake Malfunction Descent Checklist” and “Flight Control/Brake Malfunction Landing Checklist”, page 45.

Ground Spoilers Speedbrake


BRK (LH or RH) FAIL

[Condition: Main landing gear inboard/outboard normal brakes inoperative.]1. BRK (LH or RH) FAIL Checklist complete, and

* Establish and communicate a plan* Accomplish “Flight Control/Brake Malfunction Descent Checklist”


LG WOW SYS FAIL

[Condition: PSEM failure or failure of the proximity sensors.]1. Icing Conditions .............................................................................Avoid2. Land at the nearest suitable airport.3. Consideration:

• Thrust reversers, steering, ground spoilers and wing anti-ice may not be available.

4. LG WOW SYS FAIL Checklist complete, and* Establish and communicate a plan.* Accomplish “Flight Control/Brake Malfunction Descent Checklist”


BRK CONTROL FAULT

[Condition: Failure in a single wheel brake resulting in a degraded brake performance.]

1. BRK CONTROL FAULT Checklist complete, and* Establish and communicate a plan.* Accomplish “Flight Control/Brake Malfunction Descent Checklist”


BRK (LH or RH) FAULT

[Condition: Inboard or outboard wheel brake inoperative.]1. BRK (LH or RH) FAULT Checklist complete, and

* Establish and communicate a plan.* Accomplish “Flight Control/Brake Malfunction Descent Checklist”



SPOILER FAULT

[Condition: One or more of the multi-function spoilers panels reverted to Direct Mode, extended inadvertently or failed to extend.]

1. SPD BRK.....................................................................................CLOSE2. FLIGHT CONTROLS MODE SPOILERS..................PUSH IN, WAIT 10

SECONDS, then OUT3. If SPOILER FAULT is not annunciated:

a. SPOILER FAULT Checklist complete.If SPOILER FAULT is annunciated:a. The following components are inoperative:

b. If any spoiler panel has failed open or is not possible to determine position:(1) SPOILER FAULT Checklist complete, and

* Accomplish “Pitch/Roll Malfunction Descent Checklist” and “Pitch/Roll Malfunction Landing Checklist”, page 46.

If all spoiler panels are closed:(1) SPOILER FAULT Checklist complete, and

* Accomplish “Flight Control/Brake Malfunction Descent Checklist” and “Flight Control/Brake Malfunction Landing Checklist”, page 45.

SPOILER FAULT (ON THE GROUND)

[Condition: While on the ground, one or more of the multi-function spoilers panels reverted to Direct Mode, extended inadvertently or failed to extend.]

1. Control Wheels...............................................................Neutral Position2. FLIGHT CONTROLS MODE SPOILERS.................PUSH IN then OUT3. Contact Maintenance.4. SPOILER FAULT (ON THE GROUND) Checklist complete.

Ground spoilers (partially or fully lost)

Speedbrake (partially or fully lost)

or

or


Flight Control/Brake Malfunction Descent Checklist

1. Approach Considerations:• Plan on a Flap FULL landing.• Establish landing configuration early.

2. Landing Distance.................................................................... Determine

3. Shoulder Harness...................... Verify...............................................On4. FSTN BELTS ..................................................................................... ON5. Altimeters................................... Verify..................................... __.__Set6. Landing Data ............................. Verify............................. VREF FULL Set7. EICAS........................................................................................Checked8. Approach Briefing .................................................................... Complete9. Landing Considerations (for brake malfunction):

• Apply brakes normally.• If necessary, apply the Emergency/Parking Brake monitoring the

Emergency/Parking Brake light. When the light is on, maintain steady pressure since the anti-skid protection is not available.

10. Flight Control/Brake Malfunction Descent Checklist complete.

Flight Control/Brake Malfunction Landing Checklist


3. Flaps.......................................... Verify........................................... FULL4. Flight Control/Brake Malfunction Landing Checklist complete.


For the following EICAS messages:

Multiply the Unfactored Landing Distance on page 92 by:

AVNX MAU 1A FAIL 1.70AVNX MAU 1B FAIL 1.15AVNX MAU 2B FAIL 1.65AVNX MAU 3A FAIL 1.20AVNX MAU 3B FAIL

BRK CONTROL FAULTBRK (LH or RH) FAIL

BRK (LH or RH) FAULT1.65

GROUND SPOILERS FAIL 1.30LG WOW SYS FAIL

SPOILER FAULT 1.45SPOILER NML MODE FAIL


Pitch/Roll Malfunction Descent Checklist

1. Approach Considerations:• Plan on a Flap 5 landing.• Establish landing configuration early.• Avoid crosswinds greater than 10 kts. for a roll malfunction.

2. Landing Distance.................................................................... Determine

3. Shoulder Harness.......................Verify .............................................. On4. FSTN BELTS......................................................................................ON5. Altimeters ...................................Verify .....................................__.__Set6. Landing Data ..............................Verify .....................VREF FULL + 15 Set7. EICAS........................................................................................Checked8. Approach Briefing.....................................................................Complete9. Landing Consideration:

• Expect less elevator control authority and slower response during landing flare.

10. Pitch/Roll Malfunction Descent Checklist complete.

Pitch/Roll Malfunction Landing Checklist

1. EICAS........................................................................................Checked2. Landing Gear..............................Verify ...........................Down, 3 Green

3. Flaps...........................................Verify ................................................. 54. Go Around Consideration:

• Maintain airspeed of VREF FULL + 15 KIAS (limited to 175 KIAS).

5. Pitch/Roll Malfunction Landing Checklist complete.* This is an NTSB Reportable Event.

For the following: Multiply the Unfactored Landing Distance on page 92 by:

ELEVATOR (LH or RH) FAIL1.40Jammed Control Column - Pitch

Jammed Control Wheel - RollPITCH TRIM FAIL 1.40SPOILER FAULT 1.78

STALL PROT FAIL 1.40


Jammed Rudder Pedals


2. The following component is inoperative:

3. Jammed Rudder Pedals Checklist complete, and* Establish and communicate a plan.* Use asymmetrical thrust for directional control.* Accomplish “Jammed Rudder Pedals Descent Checklist” and

“Jammed Rudder Pedals Landing Checklist”, page 47.

Jammed Rudder Pedals Descent Checklist

1. Approach Considerations:• Plan on a Flap FULL landing.• Avoid crosswinds greater than 10 kts.• Use asymmetrical thrust for directional control.• Due to possible inadvertent flight control inputs, consider first officer to

accomplish approach and landing.2. Shoulder Harness...................... Verify...............................................On3. FSTN BELTS ..................................................................................... ON4. Altimeters................................... Verify..................................... __.__Set5. Landing Data ............................. Verify............................. VREF FULL Set6. EICAS........................................................................................Checked7. Approach Briefing .................................................................... Complete8. Landing Considerations:

• Determine who will accomplish the landing.• First Officer holds the Yoke Steering Disengage Switch until the captain

engages the Nosewheel Steering Handle upon nosewheel touchdown.• Use asymmetric thrust/braking as necessary.• Do not release the Nosewheel Steering Handle until aircraft is

completely stopped.9. Jammed Rudder Pedals Descent Checklist complete.

Jammed Rudder Pedals Landing Checklist


3. Flaps.......................................... Verify........................................... FULL4. Yoke Steer Disc ............................................................................... Hold5. Go Around Consideration:

• Maintain airspeed of VREF FULL + 15 KIAS (limited to 175 KIAS).

6. Jammed Rudder Pedals Landing Checklist complete.* This is an NTSB Reportable Event.



Yaw Trim


AT NOT IN HOLD

[Condition: Autothrottle not in takeoff HOLD.]1. Autothrottles ...........................................................................Disengage2. AT NOT IN HOLD Checklist complete.

AURAL WRN SYS FAIL

1. Visual Indications ........................................................................ Monitor2. The following components are inoperative:

3. Consideration:• TCAS aural will be operative.

4. AURAL WRN SYS FAIL Checklist complete.

CREW OXY LO PRESS

[Condition: Oxygen cylinder pressure below limits or pressure sensor failure.]1. Altitude .......................... 10,000 ft. or safe altitude (whichever is higher)2. CREW OXY LO PRESS Checklist complete.

PAX OXY NOT DEPLOYED

[Condition: Cabin altitude above 14,200 ft. with masks not deployed.]1. PASSENGER OXYGEN MASKS DEPLOY............... OVRD (if required)2. PAX OXY NOT DEPLOYED Checklist complete.

NO TAKEOFF CONFIG

[Condition: Aircraft not in a valid takeoff configuration.]1. Aircraft .....................................................................Configure for takeoff2. Considerations:

• Flaps not in takeoff position.• Parking brakes are applied.• Pitch trim out of green range.• Any spoiler panel is deployed.

3. NO TAKEOFF CONFIG Checklist complete.

ADS PROBE 1 (2, 3, 4) FAIL

1. Do not takeoff.

ADS (1 or 2) FAIL

[Condition: Associated ADS failed.]1. Automatic Revision......................................................................... Verify2. Associated Revisionary Panel ADS ...................... PUSH (if necessary)3. ADS (1 or 2) FAIL Checklist complete.

Aural Warnings, including EGPWS callouts


ADS 3 FAIL

[Condition: ADS #3 failed.]1. Reversion ............................................................................ As Required2. ADS 3 FAIL Checklist complete.

NAVCOM (1 or 2) FAIL

[Condition: All functions hosted in MRC (1 or 2) unavailable.]1. Select and use the remaining NAVCOM.2. NAVCOM (1 or 2) FAIL Checklist complete.

DISPLAY CTRL FAIL

[Condition: The loss of all display controller function.]1. IESS Altitude Indication ................................................. Use (if required)2. DISPLAY CTRL (1 or 2) FAIL Checklist complete.

EICAS FAULT

1. EICAS Information...............................Check and revert (as necessary)2. EICAS FAULT Checklist complete.

EICAS OVHT

1. Circuit Breaker B11.........................................................................PULL2. Reversionary Selector ..................................................................EICAS3. EICAS OVHT Checklist complete.

IRS EXCESSIVE MOTION

[Condition: Excessive aircraft motion disturbing IRS aligning sequence.]1. Aircraft ........................................................................................... STOP2. IRS will restart the alignment after the motion is stopped.3. IRS EXCESSIVE MOTION Checklist complete.

IRS (1 or 2) FAIL

[Condition: Associated IRS failed.]1. Reversionary IRS Selector ............................................................PUSH2. IRS (1 or 2) FAIL Checklist complete.

APM FAIL

1. Do not takeoff.

APM MISCOMP

1. Do not takeoff.


AVNX ASCB FAULT

1. Do not takeoff.

AVNX MAU 1 (2) (3) FAN FAIL

1. Do not takeoff.

AVNX MAU 1A FAIL

[Condition: Avionics MAU 1A channel failed.]1. Land at the nearest suitable airport.2. Icing Conditions.............................................................................. Avoid3. The following components are inoperative:

4. AVNX MAU 1A FAIL Checklist complete, and* Establish and communicate a plan.* Accomplish “Flight Control/Brake Malfunction Descent Checklist”


AVNX MAU 1B FAIL


2. AVNX MAU 1B FAIL Checklist complete, and* Establish and communicate a plan.* Accomplish “Flight Control/Brake Malfunction Descent Checklist”


AVNX MAU 2A FAIL

[Condition: Avionics MAU 2A channel failed.]


2. Consideration:a. Steer the aircraft with rudder and differential braking.

3. AVNX MAU 2A FAIL Checklist complete.

Outboard Brakes Left Aileron IndicationWeather Radar ACARSPitch Trim Indication Autopilot 1 MCDU 1 (except circuit breakers page)

Multi-function Spoiler L5, R5

GPS 1 Multi-function Spoilers L5, R5Pitch Trim Indication

FMS 1 Nosewheel Steering


AVNX MAU 2B FAIL


2. AVNX MAU 2B FAIL Checklist complete, and* Establish and communicate a plan.* Accomplish “Flight Control/Brake Malfunction Descent Checklist”


AVNX MAU 3A FAIL

[Condition: Avionics MAU 3A channel failed.]1. Land at the nearest suitable airport.2. Icing Conditions ..............................................................................Avoid3. The following components are inoperative:

4. AVNX MAU 3A FAIL Checklist complete, and* Establish and communicate a plan.* Accomplish “Flight Control/Brake Malfunction Descent Checklist”


AVNX MAU 3B FAIL


2. AVNX MAU 3B FAIL Checklist complete, and* Accomplish “Flight Control/Brake Malfunction Descent Checklist”


Inboard Brakes Autopilot 1MCDU 2 (except circuit breakers page)

IESS- Localizer & Glideslope Indication

Right Side WX Radar Control NAV/COM 2EPGWS Transponder 2

Multi-function Spoiler L3, L4, R3, R4 Autopilot 2Right Aileron Indication APUFMS 2 ADS 3Ground Spoilers GPS 2Speedbrakes

MFS L3, L4, R3, R4 Pitch Trim IndicationEngine Vibration Indication


AVNX MAU (1A or 1B) OVHT

[Condition: Associated Avionics MAU channel unavailable.]1. If AVNX MAU 1A OVHT is annunciated:

a. Circuit Breakers B6 and B7.................................................... PULLb. AVNX MAU (1A or 1B) OVHT Checklist complete, and

* Accomplish “AVNX MAU 1A FAIL” procedure, page 50..If AVNX MAU 1B OVHT is annunciated:a. Circuit Breaker B15 ................................................................ PULLb. AVNX MAU (1A or 1B) OVHT Checklist complete, and

* Accomplish “AVNX MAU 1B FAIL” procedure, page 50..



a. Circuit Breaker B25 ................................................................ PULLb. AVNX MAU (2A or 2B) OVHT Checklist complete, and

* Accomplish “AVNX MAU 2A FAIL” procedure, page 50..If AVNX MAU 2B OVHT is annunciated:a. Circuit Breaker B26 and B35.................................................. PULLb. AVNX MAU (2A or 2B) OVHT Checklist complete, and




a. Circuit Breaker B34 ................................................................ PULLb. AVNX MAU (3A or 3B) OVHT Checklist complete, and

* Accomplish “AVNX MAU 3A FAIL” procedure, page 51..If AVNX MAU 3B OVHT is annunciated:a. Circuit Breaker B27 ................................................................ PULLb. AVNX MAU (3A or 3B) OVHT Checklist complete, and


CHECK EICAS

1. EICAS Information................................................................ Crosscheck2. CHECK EICAS Checklist complete

CHECK MFD (1 or 2)

1. Crosscheck the associated display information with the standby instruments or with the other displays.

2. CHECK MFD (1 or 2) Checklist complete.

CHECK PFD (1 or 2)

1. Crosscheck the associated display information with the standby instruments or with the other displays.

2. CHECK PFD (1 or 2) Checklist complete.

or

or

or


CMS FAIL

1. Do not takeoff.

CREW WRN SYS FAULT

1. Do not takeoff.

DISPLAY CTRL FAULT

1. Do not takeoff.

VHF 3 FAIL

1. Select another VHF.2. VHF 3 FAIL Checklist complete.

MCDU (1 or 2) OVHT

[Condition: MCDU overtemperature.]1. If MCDU 1 OVHT is annunciated:

a. Circuit Breaker B16 ................................................................PULLb. MCDU (1 or 2) OVHT Checklist complete.If MCDU 2 OVHT is annunciated:a. Circuit Breaker B31 ................................................................PULLb. MCDU (1 or 2) OVHT Checklist complete.

MFD (1 or 2) FAULT

[Condition: Fault detected or misleading information displayed on MFD.]1. Crosscheck the affected MFD display information with the opposite side

MFD display information and revert if necessary.2. MFD (1 or 2) FAULT Checklist complete.

MFD (1 or 2) OVHT

[Condition: Overheat condition detected in the associated MFD.]1. If MFD 1 OVHT is annunciated:

a. Circuit Breaker B29 ................................................................PULLb. Reversion .................................................................... As Requiredc. MFD (1 or 2) OVHT Checklist complete.If MFD 2 OVHT is annunciated:a. Circuit Breaker B20 ................................................................PULLb. Reversion .................................................................... As Requiredc. MFD (1 or 2) OVHT Checklist complete.

or

or


NAVCOM (1 or 2) OVHT

[Condition: MRC NIM over temperature condition.]1. If NAVCOM 1 OVHT is annunciated:

a. Circuit Breaker C10................................................................ PULLb. NAVCOM (1 or 2) OVHT Checklist complete.If NAVCOM 2 OVHT is annunciated:a. Electronic Circuit Breaker MRC2 ........................................... PULLb. NAVCOM (1 or 2) OVHT Checklist complete.

PFD (1 or 2) FAULT

[Condition: Fault detected or misleading information displayed.]1. Crosscheck the affected PFD display information with the opposite side

PFD display information.2. PFD ........................................................................Revert (if necessary)3. PFD (1 or 2) FAULT Checklist complete.

PFD (1 or 2) OVHT

[Condition: Overheat condition detected on associated PFD.]1. If PFD 1 OVHT is annunciated:

a. Circuit Breaker B19 ................................................................ PULLb. Reversion .................................................................... As Requiredc. PFD (1 or 2) OVHT Checklist complete.If PFD 2 OVHT is annunciated:a. Circuit Breaker B21 ................................................................ PULLb. Reversion .................................................................... As Requiredc. PFD (1 or 2) OVHT Checklist complete.

VHF (1 or 2 or 3) OVHT

[Condition: VHF COM detected an overheat condition.]1. If VHF 1 OVHT is annunciated:

a. Circuit Breaker C11 ................................................................ PULLb. VHF (1 or 2 or 3) OVHT Checklist complete.If VHF 2 OVHT is annunciated:a. Electronic Circuit Breaker VHF2 ............................................ PULLb. VHF (1 or 2 or 3) OVHT Checklist complete.If VHF 3 OVHT is annunciated:a. Electronic Circuit Breaker VHF3 ............................................ PULLb. VHF (1 or 2 or 3) OVHT Checklist complete.

GND PROX FAIL

1. Increase awareness in relation to ground proximity.

SYS CONFIG FAIL

1. Do not takeoff.

or

or

or

or


TERRAIN FAIL

1. Increase awareness in relation to terrain proximity.

VALIDATE CONFIG

1. Do not takeoff.

WINDSHEAR FAIL

1. Increase awareness in relation to weather, wind and speed variations.

FUEL (1 or 2) LO LEVEL

[Condition: Low level sensors indicate 660 lbs (300kg) of fuel remain in the respective tank. Fuel quantity indication displayed red.]

1. If fuel leak is suspected:a. FUEL (1 or 2) LO LEVEL Checklist complete, and

* Accomplish “Fuel Leak”, page 57.If fuel leak is not suspected:a. FUEL XFEED ..............................................................As Requiredb. Land at the nearest suitable airport.c. Attitudes in excess of 15° nose up or down ...........................Avoidd. Uncoordinated maneuvers and negative G’s .........................Avoide. Considerations:

• Maintain a clean configuration as long as possible during the descent and approach to conserve fuel. However, initiate configuration change early enough to provide a smooth, slow deceleration to final approach speed to prevent fuel running forward in the tanks.

• Runway conditions permitting, avoid heavy braking and high levels of reverse thrust to prevent uncovering all fuel pumps and possible engine flameout during landing roll.

• For a go around, apply thrust slowly and smoothly, maintain minimum nose-up attitude required for safe climb gradient and avoid rapid acceleration.

• If any wing tank fuel pump low pressure message is displayed, do not turn fuel pump off.

f. FUEL (1 or 2) LO LEVEL Checklist complete.

FUEL AC PUMP (1 or 2) FAIL

[Condition: Discrepancy between commanded/actual pump states.]1. If FUEL AC PUMP 1 FAIL is annunciated:

a. FUEL XFEED .......................................................................LOW 1b. FUEL AC PUMP (1 or 2) FAIL Checklist complete.If FUEL AC PUMP 2 FAIL is annunciated:a. FUEL XFEED .......................................................................LOW 2b. FUEL AC PUMP (1 or 2) FAIL Checklist complete.

or

or


FUEL DC PUMP FAIL

[Condition: Discrepancy between commanded/actual pump states.]1. FUEL DC PUMP...............................................................................OFF2. FUEL DC PUMP FAIL Checklist complete.

FUEL TANK LO TEMP

[Condition: Fuel temperature less than or equal to -40°C.]1. Airspeed ......................Accelerate as much as possible up to VMO/MMO

Wait 3 minutes.2. If FUEL TANK LO TEMP remains annunciated:

a. Altitude ..............................................................................Descendb. Engine Indications............................................................... Monitorc. FUEL TANK LO TEMP Checklist complete.If FUEL TANK LO TEMP does not remain annunciated:a. FUEL TANK LO TEMP Checklist complete.

FUEL IMBALANCE

[Condition: Fuel imbalance 800 lbs or more.]1. If a fuel leak is suspected:

a. FUEL IMBALANCE Checklist complete, and* Accomplish “Fuel Leak”, page 57.

If fuel leak is not suspected:a. FUEL XFEED .............................................................. As Requiredb. FUEL IMBALANCE Checklist complete.

FUEL XFEED FAIL

[Condition: Discrepancy between cockpit control position and either valve position or affected pump status.]

1. If FUEL XFEED is OFF:a. FUEL XFEED FAIL Checklist complete.If FUEL XFEED is not OFF:a. Associated FUEL AC PUMP (higher quantity tank) ...................ONb. If fuel is balancing:

When appropriate:(1) FUEL XFEED..................................................................OFF(2) FUEL AC PUMP (higher quantity tank)........................ AUTO(3) FUEL XFEED FAIL Checklist complete.If fuel is not balancing:(1) FUEL XFEED..................................................................OFF(2) FUEL AC PUMP (higher quantity tank)........................ AUTO(3) Asymmetric thrust .............................................. As Required(4) FUEL XFEED FAIL Checklist complete.

or

or

or

or


Fuel Leak

A fuel leak may be evidenced by one or more of the following:

• Visual observation of fuel spray from the strut/engine.• Excessive engine fuel flow.• Total fuel quantity decreasing at an abnormal rate.• Fuel imbalance.• Unexpected total fuel quantity difference between EICAS and FMS

Performance Init page.1. FUEL XFEED ...................................................................................OFF2. Affected Fuel Tank....................................................................... Identify3. If leak is on the RH tank:

a. APU ..........................................................................................OFFb. Land at the nearest suitable airport.c. Inflight Fuel Leak Checklist complete, and

* Establish and communicate a plan.If leak is not on the RH tank:a. APU ............................................................................. As Requiredb. Land at the nearest suitable airport.c. Inflight Fuel Leak Checklist complete, and


HYD PTU FAIL

[Condition: PTU not supplying hydraulic power to System 2 or PTU automatic operation compromised.]

1. PTU ................................................................................................... ON2. HYD PTU FAIL Checklist complete.

HYD (1 or 2) OVERHEAT

[Condition: System (1 or 2) temperature exceeded caution range.]1. Associated HYDRAULIC ELEC PUMP ............................................OFF2. Associated ENG PUMP SHUTOFF.......................................... PUSH IN3. If HYD (1 or 2) SOV FAIL is annunciated:

a. Land at the nearest suitable airport.b. HYD (1 or 2) OVERHEAT Checklist complete, and


page 26..If HYD (1 or 2) SOV FAIL is not annunciated:a. HYD (1 or 2) OVERHEAT Checklist complete, and

* Establish and communicate a plan.* Accomplish as appropriate:

— “Loss of Hydraulic System 1”, page 59 or— “Loss of Hydraulic System 2”, page 60 or— “Loss of Hydraulic Systems 1 and 2”, page 62.

or

or


HYD 3 OVERHEAT

[Condition: System 3 temperature exceeded caution range.]1. HYDRAULIC SYS 3 ELEC PUMP A ................................................OFF2. HYDRAULIC SYS 3 ELEC PUMP B ................................................OFF3. HYD 3 OVERHEAT Checklist complete, and

* Accomplish “Loss of Hydraulic System 3”, page 61.

HYD (1 or 2) HI TEMP

[Condition: System (1 or 2) temperature exceeded the normal range.]1. Associated HYDRAULIC ELEC PUMP ............................................OFF2. HYD (1 or 2) HI TEMP Checklist complete.

HYD 3 HI TEMP

[Condition: System 3 temperature exceeded the normal range.]1. HYDRAULIC SYS 3 ELEC PUMP A ............................................... OFF2. HYD 3 HI TEMP Checklist complete.

HYD TEMP SENS FAIL

1. Do not takeoff.

HYD (1 or 2) LO PRESS

[Condition: System (1 or 2) pressure low.]1. Associated HYDRAULIC ELEC PUMP ..............................................ON2. If HYD (1 or 2) LO PRESS remains annunciated:

a. Associated HYDRAULIC ELEC PUMP ....................................OFFb. HYD (1 or 2) LO PRESS Checklist complete, and

* Accomplish as appropriate:— “Loss of Hydraulic System 1”, page 59 or— “Loss of Hydraulic System 2”, page 60 or— “Loss of Hydraulic Systems 1 and 2”, page 62.

If HYD (1 or 2) LO PRESS does not remain annunciated:a. HYD (1 or 2) LO PRESS Checklist complete.

HYD 3 LO PRESS

[Condition: System 3 pressure low.]1. HYDRAULIC SYS 3 ELEC PUMP B ..................................................ON2. HYDRAULIC SYS 3 ELEC PUMP A ................................................OFF3. If HYD 3 LO PRESS remains annunciated:

a. HYDRAULIC SYS 3 ELEC PUMP B ........................................OFFb. HYD 3 LO PRESS Checklist complete, and

* Accomplish “Loss of Hydraulic System 3” checklist, page 61.If HYD 3 LO PRESS does not remain annunciated:a. HYD 3 LO PRESS Checklist complete.

or

or


Loss of Hydraulic System 1


2. Loss of Hydraulic System 1 Checklist complete, and* Establish and communicate a plan.* If required, accomplish applicable After Takeoff Checklist items.* Accomplish “Loss of Hydraulic System 1 Descent Checklist” and

“Loss of Hydraulic System 1 Landing Checklist”, page 59.

Loss of Hydraulic System 1 Descent Checklist

1. Approach Considerations:• Expect lower roll rates.• Plan a long final approach.• Plan a Flap FULL landing.

2. Determine landing distance by multiplying the Unfactored Landing Distance on page 93 by 1.90.

3. Shoulder Harness...................... Verify...............................................On4. FSTN BELTS ..................................................................................... ON5. Altimeters................................... Verify..................................... __.__Set6. Landing Data ............................. Verify............................. VREF FULL Set7. EICAS........................................................................................Checked8. Approach Briefing .................................................................... Complete9. Landing Consideration:

• Stopping effectiveness degraded due to inoperative components.10. Loss of Hydraulic System 1 Descent Checklist complete.

Loss of Hydraulic System 1 Landing Checklist


3. Flaps.......................................... Verify........................................... FULL4. Loss of Hydraulic System 1 Landing Checklist complete.

MFS L3, R3, L4, R4 Engine 1 ReverserGround Spoiler L2, R2 Outboard Brakes

Autopilot



1. SPOILER FAULT Procedure ..................................... Do not accomplish2. The following components are inoperative:

3. Loss of Hydraulic System 2 Checklist complete, and* Establish and communicate a plan.* If required, accomplish applicable After Takeoff Checklist items. * Accomplish “Loss of Hydraulic System 2 Descent Checklist” and

“Loss of Hydraulic System 2 Landing Checklist”, page 60.

Loss of Hydraulic System 2 Descent Checklist

1. Approach Considerations:• Expect lower roll rates.• Plan a long final approach.• Plan a Flap FULL landing.


3. Shoulder Harness.......................Verify .............................................. On4. FSTN BELTS......................................................................................ON5. Altimeters ...................................Verify .....................................__.__Set6. Landing Data ..............................Verify .............................VREF FULL Set7. EICAS........................................................................................Checked8. Approach Briefing.....................................................................Complete9. Landing Considerations:

• Stopping effectiveness degraded due to inoperative components.• Use asymmetric thrust/braking as necessary due to nosewheel steering

inoperative.10. Go Around Consideration:

* Landing gear cannot be retracted.11. Loss of Hydraulic System 2 Descent Checklist complete.

Loss of Hydraulic System 2 Landing Checklist

1. Landing Gear Lever......................................................................DOWN2. Alternate Gear Extension ...........Confirm....................................... PULL3. EICAS........................................................................................Checked4. Landing Gear..............................Verify ...........................Down, 3 Green

5. Flaps...........................................Verify .......................................... FULL6. Loss of Hydraulic System 2 Landing Checklist complete.

Engine 2 Reverser Inboard BrakesMFS L5, R5 Ground Spoiler L1, R1

Landing Gear Retraction and NormalExtension

Nosewheel Steering




2. Loss of Hydraulic System 3 Checklist complete.

Right Outboard Elevator ActuatorBoth Outboard Aileron Actuators

Lower Rudder Actuator


Loss of Hydraulic Systems 1 and 2

1. Land at the nearest suitable airport.2. ELEVATOR FAULT Procedure .................................. Do not accomplish3. SPOILER FAULT Procedure ..................................... Do not accomplish4. The following components are inoperative:

5. Loss of Hydraulic Systems 1 and 2 Checklist complete, and* Establish and communicate a plan.* If required, accomplish applicable After Takeoff Checklist items. * Accomplish “Loss of Hydraulic Systems 1 and 2 Descent Checklist”

and “Loss of Hydraulic Systems 1 and 2 Landing Checklist”, page 62.

Loss of Hydraulic Systems 1 and 2 Descent Checklist

1. Approach Considerations:• Expect slower than normal roll and pitch rates.• Plan a long final approach.• Plan a Flaps 5 landing.


3. Shoulder Harness.......................Verify .............................................. On4. FSTN BELTS......................................................................................ON5. Altimeters ...................................Verify .....................................__.__Set6. Landing Data ..............................Verify .....................VREF FULL + 10 Set7. EICAS........................................................................................Checked8. Approach Briefing.....................................................................Complete9. Landing Considerations:

• Stopping effectiveness degraded due to inoperative components.• Apply brakes normally.• If necessary, apply the Emergency/Parking Brake monitoring the

Emergency/Parking Brake light. When the light is on, maintain steady pressure since the anti-skid protection is not available.

10. Loss of Hydraulic Systems 1 and 2 Descent Checklist complete.

Loss of Hydraulic Systems 1 and 2 Landing Checklist


5. Flaps...........................................Verify ................................................. 56. Loss of Hydraulic Systems 1 and 2 Landing Checklist complete.


Landing Gear Retraction and Normal Extension

MFS Spoilers L3, R3, L4, R4, L5, R5

Left Elevator Ground Spoilers L1, R1, L2, R2Speedbrake Engine 1 and 2 Reverser

Outboard and Inboard Brakes AutopilotNosewheel Steering



1. Land at the nearest suitable airport.2. SPOILER FAULT Procedure ..................................... Do not accomplish3. The following components are inoperative:

4. Loss of Hydraulic Systems 1 and 3 Checklist complete, and* Establish and communicate a plan.* If required, accomplish applicable After Takeoff Checklist items. * Accomplish “Loss of Hydraulic Systems 1 and 3 Descent Checklist”



1. Approach Considerations:• Expect slower than normal roll and pitch rates.• Plan a long final approach.• Plan a Flaps 5 landing.• Avoid crosswinds greater than 10 kts.


3. Shoulder Harness...................... Verify...............................................On4. FSTN BELTS ..................................................................................... ON5. Altimeters................................... Verify..................................... __.__Set6. Landing Data ............................. Verify..................... VREF FULL + 10 Set7. EICAS........................................................................................Checked8. Approach Briefing .................................................................... Complete9. Landing Consideration:

• Stopping effectiveness degraded due to inoperative components.10. Loss of Hydraulic Systems 1 and 3 Descent Checklist complete.



3. Flaps.......................................... Verify..................................................54. Loss of Hydraulic Systems 1 and 3 Landing Checklist complete.


Rudder Ground Spoiler L2, R2Engine 1 Reverser MFS Panel L3, R3, L4, R4Outboard Brakes Autopilot



1. Land at the nearest suitable airport.2. ELEVATOR FAULT Procedure .................................. Do not accomplish3. SPOILER FAULT Procedure .................................... Do not accomplish4. The following components are inoperative:

5. Loss of Hydraulic System 2 and 3 Checklist complete, and* Establish and communicate a plan.* If required, accomplish applicable After Takeoff Checklist items. * Accomplish “Loss of Hydraulic Systems 2 and 3 Descent Checklist”



1. Approach Considerations:• Expect slower than normal roll and pitch rates.• Plan a long final approach.• Plan a Flaps 5 landing.• Avoid crosswinds greater than 10 kts.


3. Shoulder Harness.......................Verify .............................................. On4. FSTN BELTS......................................................................................ON5. Altimeters ...................................Verify .....................................__.__Set6. Landing Data ..............................Verify .....................VREF FULL + 10 Set7. EICAS........................................................................................Checked8. Approach Briefing.....................................................................Complete9. Landing Consideration:

• Stopping effectiveness degraded due to inoperative components.10. Loss of Hydraulic Systems 2 and 3 Descent Checklist complete.



5. Flaps...........................................Verify ................................................. 56. Loss of Hydraulic Systems 2 and 3 Landing Checklist complete.


Right Elevator Ground Spoiler L1, R1Ailerons Inboard Brakes

Engine 2 Reverser MFS Spoiler L5, R5Nosewheel Steering Landing Gear Retraction and

Normal Extension


HYD 3 VLV FAIL

[Condition: Hydraulic system 3 valve failed.]1. Airspeed ................................................................... 130 KIAS minimum2. HYD 3 VLV FAIL Checklist complete.

HYD (1 or 2) EDP NOT D-PRESS

[Condition: Depressurization of associated engine-driven pump failed.]1. Consideration:

• Engine windmill restart will not be available.2. HYD (1 or 2) EDP NOT D-PRESS Checklist complete.

ADS (1 or 2 or 3) HTR FAIL

[Condition: Associated heater failed.]1. Associated ADS............................................................................ Revert2. ADS (1 or 2 or 3) HTR FAIL Checklist complete.

ADS 4 HTR FAIL

[Condition: ADS 4 heater failed.]1. IESS Airspeed and Altitude Indications ................................... Disregard2. ADS 4 HTR FAIL Checklist complete.

A-I ENG (1 or 2) FAIL

[Condition: Associated engine anti-ice bleed valve closed when commanded open, or duct failure detected.]

1. Associated ICE PROTECTION ENGINE (1 or 2) .....PUSH OUT then IN2. If A-I ENG (1 or 2) FAIL remains annunciated:

a. ICE PROTECTION MODE ....................................................... ONb. If A-I ENG (1 or 2) FAIL remains annunciated:

(1) Icing Conditions.............................................................Avoid(2) Engine Vibration .........................................................Monitor(3) If engine vibration increases:

(a) A-I ENG (1 or 2) FAIL Checklist complete, and* Accomplish “Engine Abnormal Vibration” checklist,

page 27.If engine vibration does not increase:After exiting icing conditions:(a) ICE PROTECTION MODE .................................AUTO(b) A-I ENG (1 or 2) FAIL Checklist complete.

If A-I ENG FAIL does not remain annunciated:After exiting icing conditions:(1) ICE PROTECTION MODE...........................................AUTO(2) A-I ENG (1 or 2) FAIL Checklist complete.

If A-I ENG FAIL does not remain annunciated:a. A-I ENG (1 or 2) FAIL Checklist complete.

or

oror


A-I LO CAPACITY

[Condition: Wing anti-ice bleed air pressure and temperature capacity low.]1. Thrust Levers ............................................................................ Advance2. A-I LO CAPACITY Checklist complete.

A-I WING FAIL

[Condition: Wing anti-ice system failure detected.]1. ICE PROTECTION WING........................................PUSH OUT then IN2. If A-I WING FAIL remains annunciated:

a. ICE PROTECTION MODE.........................................................ONb. If A-I WING FAIL still remains annunciated:

(1) ICE PROTECTION MODE........................................... AUTO(2) ICE PROTECTION WING................................... PUSH OUT(3) Icing Conditions ............................................................ Avoid(4) A-I WING FAIL Checklist complete.If A-I WING FAIL does not remain annunciated:After exiting icing conditions:(1) ICE PROTECTION MODE........................................... AUTO(2) A-I WING FAIL Checklist complete.

If A-I WING FAIL does not remain annunciated:a. A-I WING FAIL Checklist complete.

A-I WING NO DISPATCH

[Condition: Wing anti-ice bleed valve failed open.]1. Inflight Assisted Engine Airstart....................................... Do not perform2. A-I WING NO DISPATCH Checklist complete.

A-I WING (1 or 2) LEAK

[Condition: Overheating/leakage detected.]1. ICE PROTECTION WING.................................................... PUSH OUT2. Icing Conditions.............................................................................. Avoid3. If A-I WING (1 or 2) LEAK remains annunciated:

a. If BLEED 1 is affected:(1) BLEED 1 ............................................................. PUSH OUT(2) XBLEED.............................................................. PUSH OUT(3) Altitude ......... 31,000 ft. or safe altitude (whichever is higher)(4) APU BLEED........................................................ PUSH OUT(5) A-I WING (1 or 2) LEAK Checklist complete.If BLEED 2 is affected:(1) BLEED 2 ............................................................. PUSH OUT(2) XBLEED.............................................................. PUSH OUT(3) Altitude ......... 31,000 ft. or safe altitude (whichever is higher)(4) A-I WING (1 or 2) LEAK Checklist complete.

If A-I WING (1 or 2) LEAK does not remain annunciated:a. A-I WING (1 or 2) LEAK Checklist complete.

or

or

oror


ICE DETECTOR (1 or 2) FAIL

[Condition: Associated ice detector failed.]In icing conditions:

1. ICE PROTECTION MODE ............................................................... .ONTwo minutes after exiting icing conditions:

2. ICE PROTECTION MODE ............................................................AUTO3. ICE DETECTOR (1 or 2) FAIL Checklist complete.

WINDSHIELD (1 or 2) HTR FAIL

[Condition: Associated windshield heating system failed/overheated.]1. Associated WINDSHIELD HEATING........................PUSH OUT then IN2. If WINDSHIELD (1 or 2) HTR FAIL remains annunciated:

a. Associated WINDSHIELD HEATING............................ PUSH OUTb. WINDSHIELD (1 or 2) HTR FAIL Checklist complete.If WINDSHIELD (1 or 2) HTR FAIL does not remain annunciated:a. WINDSHIELD (1 or 2) HTR FAIL Checklist complete.

LG LEVER DISAG

[Condition: EICAS Indication: Landing gear lever and at least one landing gear discrepancy.]

1. Landing Gear Lever........................................................................Cycle2. If LG LEVER DISAG remains annunciated:

a. If following extension:(1) LG LEVER DISAG Checklist complete, and

* Accomplish “Abnormal Landing Gear Extension” checklist, page 69.

If following retraction:(1) Icing Conditions.............................................................Avoid(2) Landing Gear ............................................................ DOWN(3) LG LEVER DISAG Checklist complete.

If LG LEVER DISAG is not annunciated:a. LG LEVER DISAG Checklist complete.

or

oror


BRK OVERHEAT

[Condition: Brake temperature exceeded the normal operating range.]1. In flight:

a. Landing Gear .......................................................................DOWNb. If BRK OVERHEAT remains annunciated:

Wait 5 minutes after BRK OVERHEAT extinguishes.(1) Landing Gear ............................................................. Retract(2) BRK OVERHEAT Checklist complete.If BRK OVERHEAT does not remain annunciated:(1) Landing Gear .................................................................... UP(2) BRK OVERHEAT Checklist complete.

On ground:a. Stop the aircraft as soon as possible, but avoid hard braking

actuation.b. Chocks ........................................................................................ INc. Emergency/Parking Brake .......................................................OFFd. BRK OVERHEAT Checklist complete.

EMER BRK FAIL

[Condition: Both brake accumulator pressures low and hydraulic systems 1 & 2 low pressure.]

1. Considerations:• Emergency/Parking Brake is inoperative.• When parking, use wheel chocks.

2. EMER BRK FAIL Checklist complete.

LG NOSE DOOR OPEN

[Condition: Nose landing gear up and locked and gear door open.]1. Airspeed .......................................................................... 250 KIAS MAX

CautionLeave the gear lever down unless climb performance is

required to clear obstacles.

2. LG NOSE DOOR OPEN Checklist complete.

STEER FAIL

[Condition: Steering system failure.]1. Steer the aircraft using differential braking and rudder.2. STEER FAIL Checklist complete.

or

or


Oxygen Leakage

[Condition: Oxygen leakage through the crew masks, mask hose, flow indicator (blinker), or oxygen lines.]

1. NO PED............................................................................................. ON2. Oxygen Test/Reset Switch...........................................................Actuate3. Altitude................................................................................. As Required4. Oxygen Leakage Checklist complete.

Abnormal Landing Gear Extension

1. Airspeed ..........................................................................250 KIAS MAX2. Landing Gear Lever..................................................................... DOWN3. Gear ELECTRICAL OVERRIDE....................................... GEAR DOWN4. Landing Gear Indication ................................................................Check

a. If gear is down:(1) Abnormal Landing Gear Extension Checklist complete, and

* Establish and communicate a plan.If gear is not down:(1) Alternate Gear Extension Lever ...Pull UP to latched position(2) Landing Gear Indication ...............................................Check

(a) If gear is down:i) Abnormal Landing Gear Extension Checklist


If gear is still not down:i) Abnormal Landing Gear Extension Checklist

complete, and* Accomplish “Partial or Gear Up Landing”

checklist, page 70.

Gear Lever Cannot Be Moved Up

[Condition: LG WOW SYS FAIL message displayed.]1. Landing Gear Lever..................................................................... DOWN2. If obstacle clearance is required:

a. Downlock Override .................................................................Pressb. Gear Lever Cannot Be Moved Up Checklist complete, and

* Accomplish “LG WOW SYS FAIL”, page 43.If obstacle clearance is not required:a. Gear Lever Cannot Be Moved Up Checklist complete, and

* Accomplish “LG WOW SYS FAIL”, page 43.

or

or

or


Partial or Gear Up Landing


1. Fuel .......................................................... Burn to reduce landing speed2. Cabin Crew.....................................................................................Notify3. Aural Warning Circuit Breakers (C7 and C31) ............................... PULL4. NO PED/FSTN BELTS .......................................................................ON5. APU................................................................................OFF (if running)

Below 10,000 ft. AGL:6. PRESSURIZATION DUMP ...................................................... PUSH IN7. Altimeters ..................................................................................__.__Set8. Considerations:

• Review “Evacuation” procedures on page ii.• Plan a long final approach.• Plan a Flap FULL landing.

Final Approach:9. GND PROX TERR INHIB......................................................... PUSH IN10. Landing Gear................................................................................DOWN

Plan to land on available gear.11. SLAT/FLAP..................................................................................... FULL12. JBelow 1,000 feet AGL...............................Advise on PA “Brace, brace”13. Partial or Gear Up Landing Checklist complete, and

* Establish and communicate a plan.* After landing, accomplish “Evacuation” procedures on page ii.* This is an NTSB Reportable Event.


Overweight Landing

[Condition: Perform overweight landing when condition dictates it to be safer to land overweight than to continue flight.

1. Overweight landings are at captain’s discretion.2. Overweight landing data tables ...................................................Review

• Tables are based on anti-skid and ground spoiler system working.• The Minimum Landing Distance Table list the minimum required FAA

landing distance vs. gross weight for dry and wet runway conditions and airport elevations, based on normal touchdown point.

1 Data based on A/C Packs ON.

• The Approach Climb Weight Table ensures FAA required engine-out gradient requirements are satisfied.

3. Considerations:• Sink rate at touchdown should be 120 to 180 FPM (same as normal

touchdown) but must never exceed 300 FPM.• Upon touchdown use maximum available reverse thrust and brakes as

required to stop in the available runway.4. Overweight Landing Checklist complete.

* Make an “overweight landing” logbook entry after landing.

ERJ-170 FULL Flap Minimum Landing Distance Table

Landing Field Length1 Corrections

Landing Weight (1000 LB)

Dry Wet FT per 1000 FT

Pressure Altitude Dry Wet

FT per 10 KT

Tailwind Dry Wet

75 6910 7950 +180 +129080 7130 8200 +185 +130085 7330 8860 +190 +1320

Temp (°C)/

Altitude (ft)-1000 SL 2000 4000 6000 8000

10 85980 85980 85980 83787 78529 72578

15 85980 85980 85980 83595 77786 71692

20 85980 85980 85980 83176 76256 70550

25 85980 85980 85980 81117 73919 68063

30 85980 85980 84475 77003 70733 65098

35 85980 85980 79287 72936 67532 -

40 83864 80963 74468 68952 - -

45 78520 76485 70032 - - -

50 73445 72488 - - - -

Temp (°C)/

Altitude (ft)-1000 SL 2000 4000 6000 8000

10 85980 85980 85980 83225 76362 70473

5 85980 85980 85980 83507 77909 71663

0 85980 85980 85980 83712 78403 72448

-5 85980 85980 85980 83857 78668 72834

-10 85980 85980 85980 84001 78881 73222

-15 85980 85980 85980 84012 78974 73341

-20 85980 85980 85980 83833 78910 73407

-25 85980 85980 85980 83745 78888 73473

-30 85980 85980 85980 83789 78889 73540

-35 85980 85980 85980 83833 78930 73606

-40 85980 85980 85980 85980 78961 73672

EMBRAER 170 - CF34-8E5 ENGINES - FAA CERTIFICATION - BLEEDS OFF -

ENGINE & WING ANTI-ICE ON - LANDING FLAPS FULL - APPROACH FLAPS 4

APPROACH CLIMB LIMIT WEIGHT (lbs.)

APPROACH CLIMB LIMIT WEIGHT (lbs.)

EMBRAER 170 - CF34-8E5 ENGINES - FAA CERTIFICATION - BLEEDS OFF -

ENGINE & WING ANTI-ICE OFF - LANDING FLAPS FULL - APPROACH FLAPS 4


Smoke / Fumes Descent Checklist

1. Approach considerations:• Plan on a Flap 3 landing.• Flaps/Slats may operate at low rate.• Multiply the Unfactored Landing Distance on page 92 by 1.80.

2. GND PROX FLAP OVRD......................................................... PUSH IN3. Shoulder Harness.......................Verify .............................................. On4. FSTN BELTS......................................................................................ON5. Altimeters ...................................Verify .....................................__.__Set6. Landing Data ..............................Verify ..............................................Set

a. Set VREF FULL + 20 KIAS or 130 KIAS (whichever is higher).7. EICAS........................................................................................Checked8. Approach Briefing.....................................................................Complete9. Landing considerations:

• Thrust reversers may not be available.• Apply brakes normally.• If necessary, use EMER/Parking Brake and maintain steady pressure

since anti-skid protection is not available.10. Smoke / Fumes Descent Checklist complete.

Smoke / Fumes Landing Checklist

1. EICAS........................................................................................Checked2. EMER LT .................................................................................... ARMED3. Landing Gear..............................Verify ...........................Down, 3 Green

4. Flaps...........................................Verify ................................................. 35. Smoke / Fumes Landing Checklist complete.


LAV SMOKEEstablish contact with the cabin crew and consider an emergency descent if necessary.

RECIRC SMOKE

1. RECIRC FAN....................................................................... .PUSH OUT2. RECIRC SMOKE Checklist complete.


AILERON (LH or RH) FAIL

[Condition: (Left or Right) aileron inoperative.]1. Abrupt and Large Aileron Inputs..................................................... Avoid2. Bank Angle ............................................................................. 25° or less3. AILERON (LH or RH) FAIL Checklist complete, and

* Establish and communicate a plan.* Accomplish “Aileron Failure Descent Checklist” and “Aileron

Failure Landing Checklist”, page 74.

Aileron Failure Descent Checklist

1. Approach Considerations:• Plan on a Flap 5 landing.• Establish landing configuration early.• Avoid crosswinds greater than 10 kts. for a roll malfunction.


3. Shoulder Harness.......................Verify .............................................. On4. FSTN BELTS......................................................................................ON5. Altimeters ...................................Verify .....................................__.__Set6. Landing Data ..............................Verify .....................VREF FULL + 10 Set7. EICAS........................................................................................Checked8. Approach Briefing.....................................................................Complete9. Aileron Failure Descent Checklist complete.

Aileron Failure Landing Checklist

1. EICAS........................................................................................Checked2. Landing Gear..............................Verify ...........................Down, 3 Green

3. Flaps...........................................Verify ................................................. 54. Aileron Failure Landing Checklist complete.


BLEED (1 or 2) OFF

[Condition: Associated bleed off.]1. Altitude ............................................................................. 31,000 ft. max2. BLEED (1 or 2) OFF Checklist complete.

XBLEED FAIL

[Condition: Bleed isolation valve failed closed.]1. Considerations:

* Assisted crossbleed start is not available. * Engine 2 starting assisted by the APU is not available.

2. XBLEED FAIL Checklist complete.


EMER BRK FAULT

[Condition: Emergency/Parking brake degraded.]When parking:

1. Wheel Chocks ..................................................................................... IN2. Power Down ......................................................................... Accomplish3. Emergency Parking Brake.......................................... Cycle 2 to 3 times4. Accumulator Pressure ...................................................................Green

• On the status page, verify accumulator pressure returns to or remains green (normal operating range).

5. EMER BRK FAULT Checklist complete.

(FLAP or SLAT) LO RATE

[Condition: Flap/Slat system operating at low rate.]1. Consideration:

• Anticipate a slower (half speed) SLAT/FLAP actuation.2. (FLAP or SLAT) LO RATE Checklist complete.

FMS (1 or 2) FAIL

1. Navigation Data .........Select remaining FMS or V/L navigation raw data2. FMS (1 or 2) FAIL Checklist complete.

HYD (1 or 2) ELEC PUMP FAIL

1. Associated HYDRAULIC ELEC PUMP ............................................. ON2. HYD (1 or 2) ELEC PUMP FAIL Checklist complete.

HYD 3 ELEC PUMP A FAIL

[Condition: Associated hydraulic pump inoperative.]1. HYDRAULIC SYS 3 ELEC PUMP A ................................................OFF2. HYD 3 ELEC PUMP A FAIL Checklist complete.

HYD 3 ELEC PUMP B FAIL

1. HYDRAULIC SYS 3 ELEC PUMP B ................................................. ON2. HYD 3 ELEC PUMP B FAIL Checklist complete.

IRS PRES POS INVALID

1. FMS Present Position................................................... Enter or Reenter2. IRS PRES POS INVALID Checklist complete.

IRS (1 or 2) NAV MODE FAIL

1. Associated Reversionary Panel IRS Button ................................. PUSH2. IRS (1 or 2) NAV MODE FAIL Checklist complete.


OBSERVER OXY LO PRESS

1. If observer seat occupied:a. Altitude .................. 10,000 ft. or safe altitude (whichever is higher)b. OBSERVER OXY LO PRESS Checklist complete.If observer seat not occupied:a. OBSERVER OXY LO PRESS Checklist complete.

PACK (1 or 2) OFF

[Condition: Associated pack off in flight.]1. Associated PACK ..........................................................................Check2. Altitude ............................................................................. 31,000 ft. max3. PACK (1 or 2) OFF Checklist complete.

STALL PROT ICE SPEED

For approach, landing, and go-around:1. Airspeed ...................................................... Use ICE additive (+10 kts.)2. STALL PROT ICE SPEED Checklist complete.

LG NO DISPATCH

1. Power Down..........................................................................Accomplish2. Wait 30 seconds minimum.3. Power Up...............................................................................Accomplish4. Contact Maintenance.5. LG NO DISPATCH Checklist complete.

EICAS Spurious Messages

[Condition: After a normal power up procedure, some messages may be spuriously presented on the EICAS.]

1. Power Down..........................................................................Accomplish2. Wait 30 seconds minimum.3. Power Up...............................................................................Accomplish4. Ensure no spurious EICAS messages are displayed.

a. If still remaining, repeat steps 1. through 3.5. Contact Maintenance.6. Spurious EICAS Messages Checklist complete.

The following messages are considered normal when HYD SYS 1, 2, & 3 are nor pressurized:

FLT CTRL NO DISPATCH, BRK LH FAIL, BRK RH FAIL, AILERON LH FAIL, AILERON FAIL, ELEVATOR LH FAIL, ELEVATOR RH FAIL, RUDDER FAIL.

7. Spurious EICAS Messages Checklist complete.

or


Lightning Strike

If Lightning Strike Is Suspected To OccurAn imminent lightning strike event may be indicated to flight crews by the buildup of static discharge which causes interference on ADF indicators or noise in communication receivers. Another indication is St. Elmo’s Fire, which is visible at night as small electrical discharges running across the windshields and sparking on the wings.

Consider wearing sunglasses to protect your eyes from the flash or have one pilot keep eyes downward.

1. All Cockpit Lights ..........................................ON/FULL BRIGHTNESS

If The Airplane Has Been Hit By LightningIf situation is under control after a lightning strike, apply the following procedure to ascertain whether the flight may be proceed.

1. Circuit Breakers........................................................................CHECK2. Compass/Heading System ...................................................... CHECK

a. Check magnetic compass and heading system for normal indication.

3. Engine Indication...................................................................... CHECKa. Check engine for normal indication and apply associated

procedure if any failure arises after strike attachment.b. In case of engine shutdown, the flight crew shall analyze the

circumstances of the event and consider an engine airstart.4. Pressurization........................................................................... CHECK

a. Check pressurization system for normal indication.5. Flight Controls .......................................................................... CHECK

a. Check all flight controls for freedom of movement. Verify that slats/flaps and speed brakes are working properly (refer to slats/flaps and speed brakes operating limits).

6. Fuel System .............................................................................. CHECKa. Check fuel system for normal operation. Monitor fuel remaining

and fuel consumption to ascertain that no fuel leak exists.7. Altitude ................................................................................. MAINTAIN

a. Never climb the airplane after a lightning strike, unless required by performance (cl imb or obstacle clearance) or operat ion contingencies. If any structural damage is suspected, apply EMERGENCY DESCENT procedure.

8. All Other Airplane Systems ..................................................... CHECKa. Check all airplane instrument following a panel scan sequence to

ascertain that flight safety prevails.b. Apply the associated emergency/abnormal procedure if any failure

arises after lightning strike. Consider discontinuing the flight and land at the nearest suitable airport if any unsafe condition is revealed after checking systems operation.

Cont’d


On GroundApproaching and landing an airplane during a thunderstorm is strongly not recommended. The human body may provide the grounding that is otherwise lacking. If you are in the cockpit, do not attempt to communicate with ground through a wire handset, and stay inside the airplane until the storm has passed.

1. If The Airplane Has Been Hit By Lightning perform an External safety inspection:

a. Check for holes, punctures, discoloration and de-lamination throughout the whole airframe.

b. Verify for loose, melted or missing rivets.c. Check that all static dischargers are in place or in accordance with

the CDL.d. Verify the integrity of the lights installed on tail, wing, fuselage ande. landing gear.f. Verify all antennas, ice detectors, smart probes, TAT probes and

pressurization static ports for condition.2. Write up the lightning strike in the Flight/Maintenance Log and

report to maintenance personnel.3. Make sure that the maintenance performed before flying the

airplane again.4. Fill out a LIGHTNING STRIKE REPORT form.5. Lightning Strike Checklist ....................................................Complete

Original 29AUG2005 ERJ-170 QRH78 September 23, 2005 QRH-05-01

The following EICAS messages are crew awareness.

ADS (1 or 2) HTR FAULT

ADS 3 SLIPCOMP FAIL

ADS 4 SLIPCOMP FAIL

AFCS FAULT

AFCS PANEL FAIL

AFCS PANEL FAULT

A-I ENG (1 or 2) FAULT

A-I ENG (1 or 2) LEAK

A-I MODE NOT AUTO

A-I SWITCH OFF

AMS CTRL FAULT

AP FAULT

AP PITCH TRIM FAULT

APM FAULT

APPR 2 NOT AVAIL



APU FIREX BTL DISCH

AT FAULT

AURAL WRN SYS FAULT

AUTO CONFIG TRIM FAIL

AVNX DB MODULE FAIL

AVNX MAU (1A or 1B) FAULT



BATT (1 or 2) TEMP SENS FAULT

BRK PEDL (LH or RH) SEAT FAIL

CCD (1 or 2) FAULT

CMC FAIL

CMF (1 or 2) FAIL

CMS FAULT

CRG AFT FIREX (HI or LO) ARM



CRG FWD FIREX (HI or LO) ARM

CRG FIRE PROT FAULT

CVR (AFT or FWD) FAIL

DEFUEL SOV OPEN

ENG (1 or 2) FADEC FAULT

ENG (1 or 2) FIREX BTL (A or B) FAIL

ENG (1 or 2) FUEL SW FAIL

ENG (1 or 2) OIL IMP BYPASS

ENG (1 or 2) OIL SW FAIL

ENG (1 or 2) SHORT DISPATCH

ENG FIREX BTL (A or B) DISCH

ENG TLA TRIM FAIL

FD FAIL

FD FAULT



FDR (AFT or FWD) FAIL

FLT CTRL ADS FAIL

FLT CTRL TEST FAILED

FLT CTRL TEST IN PROG

FLT CTRL TEST PASSED

FMS (1 or 2) GPS POS DISAG

FMS POS DISAG

FUEL EQUAL-XFEED OPEN

FUEL FEED (1 or 2) FAULT

FUEL KG-LB MISMATCH

HYD (1 or 2) EDP FAIL

HYD (1 or 2 or 3) LO QTY

HYD 3 PUMP A NOT ON

HYD PTU NOT AUTO

HYD PUMP NOT AUTO



ICE CONDITION

INVERTER FAIL

IRS ALIGNING

LAV SMOKE DET FAIL

LG TEMP EXCEEDANCE

LOAD SHED

PAX OXY SW NOT AUTO

PITCH CONTROL DISC

PITCH TRIM BKUP FAIL

PITCH TRIM SW (1 or 2) FAIL

PRESN AUTO FAULT

RALT (1 or 2) FAIL

RAM AIR FAULT

RAT FAIL

REMOTE CB TRIP



ROLL CONTROL DISC

SHAKER (1 or 2) FAIL

SPDA FAIL

SPDBRK LEVER DISAG

STEER FAULT

TAT (1 or 2) FAIL

TCAS FAIL

TERRAIN NOT AVAILABLE

XBLEED SW OFF

XPDR (1 or 2) FAIL

YD FAIL

YD FAULT

YD OFF


The following EICAS messages are system status messages.

A-I ENG (1 or 2) VLV OPEN

A-I WING VLV OPEN

APU FUEL SOV CLOSED

APU SHUTTING DOWN

BLEED APU VLV OPEN

CRG FIREX (HI or LO) DISCH

ENG (1 or 2) FUEL SOV CLOSED

ENG (1 or 2) REV INHIBIT

ENG (1 or2) TLA NOT IDLE

ENG TDS REF A-I ALL

ENG TDS REF A-I ENG

FUEL XFEED SOV OPEN

HYD (1 or 2) SOV CLOSED

HYD (1 or 2) SOV FAIL

STEER OFF


Minimum Flight Crew Oxygen Pressure

The following tables define the minimum oxygen system pressure beforedeparture. The indicated pressure ensures enough oxygen to perform anemergency descent from 41,000 ft. in 10 min., followed by 110 min. of cruiseat 10,000 ft.

The pressure indicated on the MFD Status page is temperature corrected and reflects the large (77 cuft) oxygen bottle.

Minimum Brake Cooling Time

[Condition: Amber brake temperature indication on Status page.]

Any amber indication of the brake temperature indication on the MFD Status page do not takeoff.

Holding

RVSM Required Equipment

Minimum Flight Crew Oxygen Pressure (PSI)2 crew 842

2 crew + Obs 1150

Altitude (ft) Maximum Airspeed (KIAS)SL < 6,000 200

> 6,000 < 14,000 230 (210 where published)> 14,000 265

TimingSL < 14,000 1 minute

> 14,000 1 minute 30 seconds

Equipment Prior to EntryAutopilot (1) Must be operationalAltitude Alerting System Must be operationalAltitude Reporting Transponder (2) One (1) must be operationalAir Data Computers (3) Two (2) must be operational


Takeoff Alternate/Takeoff Minimums

Takeoff AlternateIf the departure airport is below CAT I landing minimums for the runway(s) in use, ensure a takeoff alternate is designated.

Takeoff Minimums[See Low Time First Officer in FOM, if applicable.][The standard for aircraft with two engines is RVR 5000 or 1 mile.]

1. Refer to the Jeppesen Airport page, Takeoff Block for appropriate runway RVR/Visibility requirement.

2. Comply with IFR Departure Procedure (if applicable).3. Use table below to confirm operable RVR and Runway Lighting/Marking

requirements.

1 Takeoff allowed without these, as long as other runway markings or lighting provide sufficient visual reference to identify the takeoff surface and maintain directional control throughout takeoff roll.

2 At airports with only TDZ and RO RVR, both are required and con-trolling. At airports with TDZ, MID, RO RVR, if any RVR out, the other two are required and controlling.

3 If Mid RVR is OTS, TDZ and RO are required and controlling.

TDZ MID RO Lighting/Markings

Uni

ted

Stat

es

Vis or RVV 1/4 sm (no RVR reported) HIRL or CL or RCLM1

RC1600 S A HIRL or CL or RCLM1

RC1200 S RC

1000 CL

RC2

600RC2

600RC2

600CL, RCLM

Can

ada

RC1200

(1/4 sm)S A HIRL or CL or RCLM

RC3

600RC3

600 A3 HIRL, CL, RCLM

C: Controlling visibility; R: Required; S: May substitute for controlling visibility if “C” is not available; A: Advisory, if operational


Approach Minimums

[See High Minimums Captains or Low Time First Officers in FOM, if applicable.]Approach minimums shall be as published or as depicted in table below, whichever is higher. RVR in feet; visibility in statute miles; when either RVR or Visibility may be used, they are depicted as “RVR-Vis” (e.g. 1800-1/2).

Approach MinimumsMin. Alt. TDZ MID RO Remarks

Circling1,000 ft. HAA or MDA(whichever is higher) 3 sm Min ceiling

1,000 ft.

Non-Precision

MDA/DA RC2400-1/2 A A Use MID if TDZ

inop

CAT I ILS

DA RC1800-1/2 A A Use MID if TDZ

inopC: Controlling R: Required A: Advisory if reported.


WIND COMP/CONT RUNWAY/TEMP CONV

WIND COMPONENTSTower/ATIS wind = Magnetic METAR/TAF wind = True

U.S. Contaminated Runway T/O & Landing Guidelines

ICAO Contaminated Runway T/O & Landing Guidelines

Temperature Conversion (°C to °F)

Kts ↓ Crosswind (Degrees off Nose/Tail) ↓0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 02 0 0 0 1 1 1 1 1 1 1 2 2 2 2 2 2 2 2 24 0 0 1 1 1 2 2 2 3 3 3 3 3 4 4 4 4 4 46 0 1 1 2 2 3 3 3 4 4 5 5 5 5 6 6 6 6 68 0 1 1 2 3 3 4 5 5 6 6 7 7 7 8 8 8 8 8

10 0 1 2 3 3 4 5 6 6 7 8 8 9 9 9 10 10 10 1012 0 1 2 3 4 5 6 7 8 8 9 10 10 11 11 12 12 12 1214 0 1 2 4 5 6 7 8 9 10 11 11 12 13 13 14 14 14 1416 0 1 3 4 5 7 8 9 10 11 12 13 14 15 15 15 16 16 1618 0 2 3 5 6 8 9 10 12 13 14 15 16 16 17 17 18 18 1820 0 2 3 5 7 8 10 11 13 14 15 16 17 18 19 19 20 20 2022 0 2 4 6 8 9 11 13 14 16 17 18 19 20 21 21 22 22 2224 0 2 4 6 8 10 12 14 15 17 18 20 21 22 23 23 24 24 2426 0 2 5 7 9 11 13 15 17 18 20 21 23 24 24 25 26 26 2628 0 2 5 7 10 12 14 16 18 20 21 23 24 25 26 27 28 28 2830 0 3 5 8 10 13 15 17 19 21 23 25 26 27 28 29 30 30 3032 0 3 6 8 11 14 16 18 21 23 25 26 28 29 30 31 32 32 3234 0 3 6 9 12 14 17 20 22 24 26 28 29 31 32 33 33 34 3436 0 3 6 9 12 15 18 21 23 25 28 29 31 33 34 35 35 36 3638 0 3 7 10 13 16 19 22 24 27 29 31 33 34 36 37 37 38 3840 0 3 7 10 14 17 20 23 26 28 31 33 35 36 38 39 39 40 40

Kts 90 95 100 105 110 115 120 125 130 135 140 145 150 155 160 165 170 175 180 ↑ Tailwind (Degrees Off Nose) ↑

90 85 80 75 70 65 60 55 50 45 40 35 30 25 20 15 10 5 0 ↑ Headwind (Degrees Off Nose) ↑

°C °F °C °F °C °F °C °F °C °F °C °F44 111 30 86 16 61 2 36 -12 10 -26 -1542 108 28 82 14 57 0 32 -14 7 -28 -18

40 104 26 79 12 54 -2 28 -16 3 -30 -2238 100 24 75 10 50 -4 25 -18 0 -32 -2636 97 22 72 8 46 -6 21 -20 -4 -34 -2934 93 20 68 6 43 -8 18 -22 -8 -36 -3332 90 18 64 4 39 -10 14 -24 -11 -38 -36

0 10 20 30 40Mu

Cross ≤ 10 kt Cross ≤ 15 kt Cross ≤ 29Tail < 5 kt Tail ≤ 5 kt Tail ≤ 10 kt

Nil Poor Fair Good(Limits) See FOM

(Guidelines) (Guidelines) (Limits)

Cross ≤ 10 kt Cross ≤ 15 kt Cross ≤ 29Tail < 5 kt Tail ≤ 5 kt Tail ≤ 10 kt

Poor Poor Medium Good(Limits)

See FOM Nil

(Guidelines) (Guidelines) (Limits)

0 .10 .20 .30 .40CRFI / Mu


Severe Weather/Windshear

Takeoff•Use longest suitable runway•When possible, use flaps 2•Use maximum takeoff thrust

Evaluate the WeatherDo not takeoff or land until conditions improve. Average windshear lasts only 10-15 minutes

Any sign of hazardous convective weather within 15 miles of airport? (H=high/M=medium/L=low)

Convective weather and... •≥Moderate turbulence (M)

•Rwy specific alert (H) •Temp/Dewpoint spread >16°C (M)

•Localized strong winds (H) •Dewpoint > 10°C (M)

•≥red return/heavy precip (H)

•Rain showers (M)

•LLWAS≥20kt change (H) •Lightning (M)

Has Microburst Alert been issued for takeoff/landing runway?

Can you maintain at least 3 nm horizontal separation from severe weather when aircraft is ≤1,000 feet AGL?•ATC report of VIP level 5 or greater•Steep and/or asymmetrical radar gradients•Notches, hooks, fingers, or scalloped radar edges•Heavy rain with convective activity•Radar echo with a shadow behind it or a magenta radar return

Do you judge it safe to continue?

Apply Windshear Precautions

Follow Standard Operating Procedures•Takeoff: minimize pitch attitude reductions•Approach: avoid large thrust reductions•Know normal attitude and performance•PNF monitor flight path instruments and call out deviations

Accomplish Windshear Recovery if Windshear Encountered

Report Encounter

No

Yes

Yes

Yes

Landing•Use longest suitable runway•Use ILS or VASI for glidepath monitoring•Use flaps 5•Consider using increased approach

speed, up to 20 knots•Establish a stabilized approach no later

than 1,000 feet AFE•Minimize thrust reductions•Monitor flight director, autopilot, and

autothrottles

Yes

No

No

No


Unfactored Landing Distance

The table reflects the actual landing distance required. Plan accordingly. Chose a runway that provides the largest safety margin possible.

The published distances are based on the following: • Touchdown within 1,000 feet from the approach end of the runway.• Application of maximum manual braking.

Cont’d

NO

TE This information is for in-flight emergency use

only. These distances reflect the required landing distance only. The FAA additional runway margin is not included.

UNFACTORED LANDING DISTANCE TABLE ALL ENGINE TYPES – FAA – FLAPS 5ISA CONDITIONS – ANTI ICE OFF – AUTO BRAKES OFF

ALTITUDE

0 ft 1000 ft

WIND

Weight(lb)

-10 Kt 0 Kt 10 Kt 20 Kt -10 Kt 0 Kt 10 Kt 20 Kt

52000 2599 2198 2076 1960 2638 2230 2105 1985 56000 2716 2303 2177 2057 2758 2339 2210 2087 60000 2835 2410 2280 2156 2882 2450 2317 2190 64000 2957 2520 2385 2257 3008 2564 2427 2295 68000 3083 2628 2490 2357 3142 2676 2535 2400 72000 3222 2741 2598 2461 3286 2794 2648 2508 76000 3366 2863 2710 2566 3435 2923 2766 2617

ALTITUDE

2000 ft 3000 ft

WIND

Weight(lb)


52000 2685 2275 2150 2030 2728 2311 2183 2077 56000 2809 2387 2258 2134 2856 2428 2296 2169 60000 2936 2502 2368 2241 2988 2547 2410 2280 64000 3066 2619 2481 2349 3124 2668 2527 2393 68000 3207 2735 2593 2457 3272 2789 2644 2505 72000 3357 2860 2709 2569 3427 2920 2765 2621 76000 3517 2998 2839 2688 3605 3074 2912 2756

ALTITUDE

4000 ft 5000 ft

WIND

Weight(lb)


52000 2779 2360 2231 2108 2830 2410 2281 2157 56000 2911 2480 2347 2220 2962 2524 2389 2259 60000 3047 2602 2466 2334 3102 2651 2511 2377 64000 3190 2728 2586 2451 3253 2780 2637 2498 68000 3343 2852 2707 2566 3413 2912 2762 2619 72000 3512 2998 2841 2692 3599 3074 2913 2759 76000 3700 3160 2996 2839 3795 3243 3075 2913

NOTE: Landing distance in ft.


Unfactored Landing Distance (Cont.)

UNFACTORED LANDING DISTANCE TABLE ALL ENGINE TYPES – FAA – FLAPS FULL ISA CONDITIONS – ANTI ICE OFF – AUTO BRAKES OFF

ALTITUDE

0 ft 1000 ft

WIND

Weight(lb)


52000 2429 2041 1923 1812 2463 2068 1947 1832 56000 2529 2131 2009 1893 2567 2161 2037 1918 60000 2632 2222 2097 1977 2674 2257 2129 2021 64000 2734 2313 2183 2060 2783 2360 2230 2106 68000 2838 2405 2272 2145 2891 2455 2321 2193 72000 2943 2498 2361 2229 3001 2550 2413 2280 76000 3055 2593 2454 2320 3113 2640 2498 2362

ALTITUDE

2000 ft 3000 ft

WIND

Weight(lb)


52000 2505 2109 1988 1872 2550 2152 2030 1915 56000 2612 2205 2080 1960 2659 2250 2124 2005 60000 2721 2302 2174 2050 2772 2350 2221 2097 64000 2829 2399 2266 2139 2883 2450 2316 2188 68000 2940 2498 2361 2230 2997 2551 2414 2282 72000 3057 2597 2456 2333 3120 2653 2511 2376 76000 3177 2697 2554 2417 3240 2749 2603 2463

ALTITUDE

4000 ft 5000 ft

WIND

Weight(lb)


52000 2589 2184 2060 1941 2635 2229 2104 1985 56000 2703 2286 2158 2035 2752 2333 2204 2081 60000 2819 2390 2258 2131 2871 2440 2308 2180 64000 2933 2493 2357 2227 2989 2546 2410 2278 68000 3052 2599 2459 2324 3114 2655 2514 2378 72000 3185 2712 2569 2432 3248 2764 2618 2479 76000 3309 2813 2664 2522 3377 2871 2717 2573

NOTE: Landing distance in ft.


Evacuation Duties

[Procedure continued from Immediate Action item page ii]

Captain:1. Take a portable fire extinguisher and proceed to main cabin.2. Assess exit and evacuation conditions, assessing left hand of

aircraft first.3. Assess conditions in cabin.4. Open forward exits, if exit is still closed, (priority is the main cabin

door - 1L).5. Assist passengers in exiting the aircraft.6. Captain is last to exit. Exit only after ensuring everyone has exited,

or own life is in danger.7. If a flight attendant is incapacitated, take him/her with you.8. Take charge of all passengers and crewmembers. Keep people

together, away from aircraft.9. Do not allow smoking.10.Do not allow anyone to re-enter the aircraft.11.Supervise provision of first aid and shelter.

First Officer:1. Assess exit and evacuation conditions, assessing right hand of

aircraft first.2. The First Officer's duty is to get outside the aircraft as quickly as

possible in order to assist passengers.3. First Officer may exit out the crew emergency exit or through a

forward exit depending on the nature of the emergency, passenger load, conditions outside the aircraft, landing gear position, etc.

4. When possible, the First Officer's exit path should be briefed prior to landing.

5. Open forward exits, if exit is still closed.6. Circle the aircraft and enlist the aid of others.7. Help direct passengers to an assembly point.8. Assist the flight attendants and Captain.


Quick Reference Handbook - Aviation For All · ERJ-170 QRH Original 29AUG2005 i ERJ-170 ERJ-170 QRH...

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Transcript of Quick Reference Handbook - Aviation For All · ERJ-170 QRH Original 29AUG2005 i ERJ-170 ERJ-170 QRH...