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REVISION INFO
B767, REV INFO Date 22.03.00
REVISION: 4 DATE: 22.03.00 CHANGES: revised EFRAS-description: ESC-key description deleted; The additional information was for programmers only. Cockpit/Cabin reports and signals changed. NP 20.29 changed.
REVISION INFO
B767, REV INFO Date 16.02.00
REVISION: 3 DATE: 16.02.00 CHANGES: revised EFRAS-description Item 4 new details
B767 Workbook
B767 W o r k b o o k
PUBLISHED BY
FLEET-MANAGER B767
FOR REQUESTS CONTACT
B767 4 PUBLICATIONS
LAUDA-AIR Luftfahrt Aktiengesellschaft
P.O.Box 56 A-1300 Vienna Airport - Austria
Tel.: (0043-1) 7007-3158 Fax.: (0043-1) 7007-5628
SITA: VIEDONG
FIRST ISSUED:
30.08.1996
COPYRIGHT LAUDA AIR
B767 Workbook Introduction
B767 WKB INT , Rev.1 Date 30.08.96 , Page 1
INTRODUCTION The LAUDA AIR B767 WORKBOOK is designed to provide flight crews with readily accessible information for daily operation. The LAUDA AIR B767 WORKBOOK is structured as follows: PREFACE: TABLE OF CONTENTS, RECORD OF REVISION, RECORD OF EFFECTIVE PAGES CHAPTER 1: PROCEDURES CHAPTER 2: SUPPLEMENTARY PROCEDURES CHAPTER 3: SUPPLEMENTARY INFORMATION CHAPTER 4: ROUTE AND AERODROME INSTRUCTIONS AND INFORMATION INFORMATION APPENDIX: FLEET-INFO
B767 Workbook Introduction
Page 2 , Date 30.08.96 B767 WKB INT , Rev.1
PAGE NUMBERING AND ORGANIZATION OF THE CHAPTERS: Each chapter is subdivided into sections, categorized by the subject or type of material presented. Sections are identified by a three-letter-code.
Example:
B767 1 SOP , Rev.1 Date 30.08.96 , Page 2 B767 Workbook Chapter (B767 1), Section identifier for Standard Operating Procedures (SOP), Revision Status (Rev.1), Revision date (30.08.96), Pagenumber.
REVISION SYSTEM: Revision to this workbook will be issued when necessary and are numbered consecutively. Each revision should be inserted immediately and entered in the Record of Revision. Alterations to former pages will be identified by a vertical line, except when a whole chapter or section is revised.
TABLE OF CONTENTS: The Preface Chapter consists of a complete Table of Contents, a Record of Revision Sheets and the List of Effective Pages. For quick reference, each section also has a detailed Table of Contents.
CAUTION: Lauda Air makes no express or implied warranty and disclaims any liability with respect to the design, adequacy, accuracy, reliability, safety or conformance with government standards or regulations and approved Airplane Flight Manual. The user of this workbook has to verify the presented data by appropriate means and never rely solely on this workbook.
Any questions with regard to the use of this workbook and the information contained within should be directed to the
B767 FLEETOFFICE.
B767 Workbook Preface
B767 WKB PRF, Rev. 4 Date 13.12.99 , Page 1
TABLE OF CONTENTS
B767 WORKBOOK
Title Page
Introduction INT
PREFACE PRF
Table of Contents PRF
Revision Record PRF
List of Effective Pages PRF
CHAPTER 1 ( PROCEDURES )
Normal Procedures (Boeing-layout) NP
Non Normal Procedures NNP
CHAPTER 2 ( SUPPLEMENTARY PROCEDURES )
Take Off Performance TOP
Landing Performance LDP
NAT RVSM Operation NAT
B767 Workbook Preface
Page 2 , Date 13.12.99 B767 WKB PRF, Rev.3
TABLE OF CONTENTS
CHAPTER 3 ( SUPPLEMENTARY INFORMATION)
B767-Limitations LIM
B767-Differences DIF
B767-EFRAS ERS
CHAPTER 4 ( Route and Aerodrome Instructions and Information )
Route and Aerodrome Qualification RAQ
Special Aerodrome Briefings SAB
Route & Aerodrome Information RAI
INFORMATION APPENDIX INF APP
Introduction
FLEET-INFO
B767 Workbook Preface
B767 WKB PRF, Rev. 4 Date 13.12.99 , Page 3
RECORD OF REVISION
REVISION
NUMBER
CHAPTER REVISION DATE
INITIALS SIGNATURE
5 PREFACE 10.01.2000
2 EFRAS 10.01.2000
Note: It is the responsibility of the workbook holder to keep it up to date.
B767 Workbook Preface
Page 4 , Date 16.11.99 B767 WKB PRF, Rev.3
I N T E N T I O N A L L Y
L E F T
B L A N K
L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Operations Manual
Normal Procedures Chapter NP Table of Contents Section 0
January 01, 1998 NP.0.1
lntroduction............................................................................................................NP.10.1
General...............................................................................................................NP.10.1
Deviations from Normal Procedures .......................................................NP.10.1
Normal Procedures ...........................................................................................NP.10.1
Autopilot Flight Director System and Flight
Management System Monitoring ...........................................................NP.10.2
CDU Operation...........................................................................................NP.10.3
Radio Procedure.........................................................................................NP.10.3
ATC Procedure ..........................................................................................NP.10.3
Altimeter Procedures.................................................................................NP.10.4
Decision height reference indicator setting...........................................NP.10.4
Reference altitude marker (RAM) setting ..............................................NP.10.4
EHSI MAP Mode Procedure....................................................................NP.10.5
Instrument Approach Procedures General ............................................NP.10.5
Final Approach Procedures General.......................................................NP.10.6
Area of Responsibility and Panel Scan.........................................................NP.10.7
Amplified Procedures .............................................................................................NP.20.1
Preflight..............................................................................................................NP.20.1
Exterior Inspection.....................................................................................NP.20.1
Cockpit Preparation...................................................................................NP.20.1
Cockpit Preparation First Officer (electrical power
established) ................................................................................................NP.20.1
Cockpit Preparation First Officer (electrical power not
established) ................................................................................................NP.20.2
Cockpit Preparation Captain ...............................................................NP.20.11
Cockpit Preparation Final....................................................................NP.20.15
Engine Start .....................................................................................................NP.20.18
Engine Start Procedure ...........................................................................NP.20.18
Normal Procedures L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Table of Contents Operations Manual
NP.0.2 January 01, 1998
After Start Procedure ..............................................................................NP.20.19
Taxi-out and Takeoff......................................................................................NP.20.21
Before Takeoff Procedure......................................................................NP.20.21
Takeoff Procedure ..................................................................................NP.20.22
Climb and Cruise.............................................................................................NP.20.24
Climb Procedure .......................................................................................NP.20.24
Cruise Procedure......................................................................................NP.20.25
Approach and Landing .................................................................................NP.20.26
Descent Procedure ..................................................................................NP.20.26
Landing Procedure ..................................................................................NP.20.28
Go - Around Procedure...........................................................................NP.20.30
Landing Roll Procedure ..........................................................................NP.20.31
Taxi-in and Park ..............................................................................................NP.20.32
After Landing Procedure ........................................................................NP.20.32
Shutdown Procedure...............................................................................NP.20.33
Secure Procedure .....................................................................................NP.20.35
Flight Patterns .........................................................................................................NP.30.1
Takeoff...............................................................................................................NP.30.1
ILS Approach....................................................................................................NP.30.2
Non-Precision Approach ................................................................................NP.30.3
Circling...............................................................................................................NP.30.4
Circling Approach Plan View..........................................................................NP.30.5
Visual Traffic Pattem........................................................................................NP.30.6
Standard Callouts ....................................................................................................NP.40.1
Standard Callouts .............................................................................................NP.40.1
Standard Callouts Summary............................................................................NP.40.2
Standard Phraseology .....................................................................................NP.40.3
Cockpit/Cabin Reports and Signals .....................................................................NP.50.1
Cockpit/Cabin Reports and Signals ...............................................................NP.50.1
L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Operations Manual
Normal Procedures Chapter NP Introduction Section 10
January 13, 2000 Rev.3 NP.10.1
General This chapter contains two tabbed sections titled Normal Procedures and Supplementary Normal Procedures. The first section incorporates routine normal procedures and associated flight patterns. The second section incorporates normal procedures and flight patterns that are accomplished as required rather than routinely performed on every flight.
Deviations from Normal Procedures If any deviations from procedures are required, the term NONSTANDARD shall be used.
Normal Procedures Normal procedures are used by the trained flight crew to ensure the airplane condition is acceptable for flight and that the cockpit is correctly configured for each phase of flight. These procedures assume that all systems are operating normally and that automated features are fully utilized.
Normal procedures are performed from recall and follow a panel scan pattern. These procedures are designed to minimize crew workload and are consistent with new flight deck technology. All procedural information is task orienteted.
Before engine start, when possible, individual system lights and indications are used to verify system status when the system is activated or configured for flight. After engine start, EICAS is used as the primary indication of a non-normal system condition or improper configuration.
If an improper indication is noted during accomplishment of procedures, first verify the proper control position. Then, if necessary, check the appropriate circuit breaker(s) and test the related system light(s).
Exterior lighting used during periods of darkness, cockpit lighting and personal comfort items such as sidewall heaters are systems that are assumed to have obvious procedural requirements and are not addressed in this section.
Flight crewmember duties have been organized in accordance with an area of responsibility concept. Each crewmember is assigned a cockpit area where the crewmember can initiate action for required procedures. The panel illustration followed on next page describes the crewmember's area of responsibility and scan flow pattern for each panel. A normal scan flow is encouraged; however, certain items may be handled in the most logical sequence for existing conditions (e.g., air
Normal Procedures L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Introduction Operations Manual
NP.10.2 Rev.3 January 13, 2000
conditioning, flight plan loading, etc.). Actions outside the crewmembers area of responsibility are initiated at the direction of the Captain.
General phaseofflight responsibilities are as follows:
Pilot flying:
flight path and airspeed control.
airplane configuration.
navigation.
Pilot not flying:
checklist reading.
communications.
tasks requested by PF.
Phase of flight duties beginning with engine starting and ending with the after landing procedure, are presented in table form in the appropriate procedures section.
The first officer, when flying the aircraft, performs the duties listed under pilot flying and the captain performs those duties listed under pilot not flying.
Note: Although the mode control panel is designated as the pilot flyings responsibility, the pilot not flying should operate the controls on the mode control panel at direction of the pilot flying when the airplane is being flown manually.
The Captain, however, retains final authority for all actions directed and performed.
Autopilot Flight Director System and Flight Management System When the autopilot, flight director, or autothrottle are in use and a mode change is selected or is scheduled to occur, the annunciation must be verified on the autopilot flight director system (AFDS). Airplane course, vertical path, and speed must always be monitored.
Similarly, when a thrust reference mode change is selected or is scheduled to occur, the annunciation must be verified on the EICAS.
In LNAV and VNAV, all airplane course, vertical path, thrust, and speed changes must be verified.
L a u d a A i r B O E I N G 7 6 7 L a u d a A i r B O E I N G 7 6 7 Normal Procedures Operations Manual Introduction
January 13, 2000 Rev.3 NP.10.3
CDU Operation On the ground Control Display Unit (CDU) manipulations are normally performed by the First Officer and verified by the Captain. In automatic flight, CDU entries are accomplished by the pilot flying and verified by the pilot not flying prior to execution. However, during high workload periods such as departure, approach or holding, CDU entries shall be accomplished by the pilot not flying on command of the pilot flying. In manual flight, CDU entries are accomplished by the pilot not flying and verfied by the pilot flying prior execution.
CDU manipulations should be accomplished prior to high workload periods such as departure, arrival or holding. During high workload periods, using autopilot modes such as heading select, flight level change, and the speed intervention feature along with the HSI MAP Switches may be more efficient than making complex CDU changes.
Radio Procedure The L VHF shall be used for ATC communication. The R VHF shall be used for company communication, weather broadcast or 121.5 Mhz listening watch. The C VHF shall be used for DATA communication.
ATC Procedure
ATC heading and/or altitude clearances must be checked by both pilots. On the ground, the first officer reads back heading and/or altitude clearances to ATC and sets the heading/altitude in the heading/altitude window on the MCP. The captain calls "Heading ____" , "____" feet, FL "____ , checked". In manual flight, the pilot not flying reads back heading and/or altitude clearances to ATC and sets the heading/altitude in the heading/altitude window on the MCP. The pilot flying calls "Heading____" , "____" feet, FL "____ , checked. In automatic flight, the pilot not flying reads back heading and/or altitude clearances to ATC. The pilot flying sets the heading/altitude in the heading/altitude window on the MCP. The pilot not flying calls "Heading ____" , "____" feet, FL "____, checked.
Normal Procedures L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Introduction Operations Manual
NP.10.4 Rev.3 January 13, 2000
Altimeter Procedures The pressure scale reading on the Captains, standby and Copilots altimeters shall be set to a common value as follows:
Departing aircraft shall use QNH whilst climbing until passing transition altitude, thereafter using standard pressure.
Aircraft descending for landing change to QNH on departing transition level; however, aircraft may relate vertical position to QNH as soon as a clearence down to an altitude (QNH) or after an approach clearance has been received and descent commenced, provided level flight above the Transition Altitude is not anticipated (an anticipatory altimeter setting resulting from the procedure above may occasionally need to be reversed to standard pressure upon an ATC request for an unexpected level-off or for FL report prior to crossing the transition level).
Decision height reference indicator setting For takeoff set decision height reference indicator to -20 feet.
For approaches where DA/MDA is based on the use of barometric altimeter, set the decision height reference indicator to: - 150ft for precision approaches
- 300ft for non-precision approaches.
For approaches where DH is based on the use of radio altimeter, set the decision height reference indicator to: - applicable DH for CATII/IIIA/IIIB
- -20 feet for CATIIIB without DH.
Reference altitude marker (RAM) setting For takeoff set reference altitude marker to single-engine cleanup altitude,
according to AAM.
For Non-precision approaches: Set RAM to applicable MDA.
For CAT I approaches: Set RAM to applicable value.
For CAT II/III approaches: Set RAM to zero (12 o'clock position).
L a u d a A i r B O E I N G 7 6 7 L a u d a A i r B O E I N G 7 6 7 Normal Procedures Operations Manual Introduction
January 13, 2000 Rev.3 NP.10.5
EHSI MAP Mode Procedure It is Lauda Air policy to use EHSI MAP MODE for takeoff.
If a close-in turn after T/O is defined by an ILS DME distance (e.g. SZG rwy16) or the LOC has to be followed (e.g. INN rwy 08) the system requires the PNF to position the EHSI MODE SELECTOR to EXP ILS with relevant ILS frequency selected, in order to receive required ILS DME reading for track varification. EHSI MAP should be reselected by the PNF as soon as practicable after ILS DME info is no longer required.
Instrument Approach Procedures General During the intermediate approach EHSI MAP mode should be used. Generally for instrument approaches EHSI ILS or EHSI VOR mode, as applicable,
should be selected on one side, preferably by PF (Expanded ILS/VOR mode is recommended).
- For ILS approaches EHSI MAP mode can be used on both side of pilots, but if ILS DME readout is required for APP select EHSI ILS mode prior to intercepting localizer.
- For VOR approaches select EHSI VOR mode prior commencing the VOR approach.
- For NDB and circling approaches the EHSI MAP mode may only be used as additional information to RAW DATA.
Note: Intercept localizer with HDG SEL (localizer intercept in LNAV-Mode is not authorized).
Note: Circling is a visual maneuver where the runway, runway lights or special visual circling aids should be kept in sight while at MDA for circling.
The A/T ARM switch will stay in ARM throughout the approach and landing
(except S/E). Setting of missed approach altitude: -on precision approaches at G/S capture -on non-precision approaches
at MDA
Normal Procedures L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Introduction Operations Manual
NP.10.6 Rev.3 January 13, 2000
Final Approach Procedure General During final approach the following is not permitted: After passing FAF/FAP: - resetting of minima (new minima should be
called out instead by PF and confirmed by PNF) Below 500ft : - change of configuration - recall items - reading of non-normal checklist
L a u d a A i r B O E I N G 7 6 7 L a u d a A i r B O E I N G 7 6 7 Normal Procedures Operations Manual Introduction
January 13, 2000 Rev.3 NP.10.7
Area of Responsibility and Panel Scan
Normal Procedures L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Introduction Operations Manual
NP.10.8 Rev.3 January 13, 2000
Intentionally Blank
Lauda Air BOEING 767 Operations Manual
Normal Procedures Chapter NP Amplified Procedures Section 20
March 18, 2000 Rev.3 P.20.1
PREFLIGHT
Exterior Inspection Prior to each flight, the captain must verify the airplane is acceptable for flight. Check:
Flight control surfaces unobstructed and all surfaces clear of ice, snow, or frost.
Door and access panels (not in use) properly secured.
Ports and vents unobstructed.
Airplane free of damage and fluid leakage.
Wheel chocks in place and ground locking pins removed and nose gear steering lever in normal position.
Tire condition.
Gear struts not fully compressed.
Cockpit Preparation The following procedures assume the crew is aware of the airplane maintenance status.
Cockpit Preparation First Officer (electrical power not established) This procedure assumes electrical power is not established.
The following cockpit preparation procedures are accomplished to permit safe application of electrical power.
STANDBY POWER selector ..............................................AUTO
BATTERY switch .................................................................ON Verify battery DISCH light illuminated and standby bus OFF light extinguishes.
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.2 Rev.3 March 18, 2000
HYDRAULIC ELECTRIC pump switches ............................. OFF
HYDRAULIC DEMAND pump selectors................................ OFF
Landing gear lever ........................................................... DOWN
ALTERNATE FLAPS selector ...........................................NORM
Electrical power ............................................................ Establish APU selector - START
If APU desired, rotate selector to START and release to ON, or; EXTERNAL POWER switch - PUSH
If external power desired, push switch when AVAIL light illuminated and verify ON light illuminated.
Cockpit Preparation First Officer (electrical power established) This procedure assumes the power up procedure has been accomplished and electrical power is established.
After electrical power is established, the following procedures are accomplished in their entirety on each originating trip or crew change, or following maintenance action.
BULK CARGO HEAT selector .................................NORM/VENT Select as appropriate for cargo carried.
FLIGHT RECORDER switch ...........................................NORM
SERVICE INTERPHONE switch.......................................... OFF
RESERVE BRAKES AND STEERING RESET/DISABLE switch....................CLOSED (guarded position)
Verify ISLN light extinguished.
Circuit breakers.................................................................Check
RAIN REPELLENT...........................................................Check Verify sight gage level is above refill mark, pressure indicator within green band and shutoff valve handle in vertical position.
A/C documents and route manuals ......................................Check
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.3
Emergency equipment........................................................Check Fire Extinguisher - Checked and stowed
Verify trigger safety wire intact. Crash axe - Stowed Smoke goggles - Stowed Life vests (If required) - Stowed
IRS ................................................................... OFF, then NAV Verify ALIGN lights illuminated.
Note: A complete IRS alignment is recommended if the total time in the navigation mode is expected to exceed 18 hours.
YAW DAMPER switches ......................................................ON INOP lights remain illuminated until IRS alignment complete.
ELECTRONIC ENGINE CONTROL switches ...................NORM
Hydraulic system .................................................................. Set PRIMARY ENGINE pump switches - ON
The PRESS lights remain illuminated until the associated engine is started.
PRIMARY ELECTRIC pump switches - OFF DEMAND pump selectors - OFF
WINDOW HEAT switches* ...................................................ON Verify INOP lights extinguished.
HF radios ............................................................................ Set
EVACUATION SIGNAL COMMAND Switch* .............................................CLOSED (guarded position)
Electrical system .................................................................. Set BATTERY switch - ON
Verify DISCH light extinguished. STANDBY POWER selector - AUTO
* As installed
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.4 Rev.3 March 18, 2000
Verify standby power bus OFF light extinguished.
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.5
BUS TIE switches - AUTO Verify AC BUS OFF and utility bus OFF lights extinguished.
GENERATOR CONTROL switches - ON The OFF and DRIVE lights remain illuminated until the associated engine is started.
APU selector ..................................................................START If APU required in lieu of external power for electrical or pneumatic power, rotate selector to START and release to ON.
Lighting panel ....................................................................... Set TAXI and RUNWAY TURNOFF light switches OFF
EMERGENCY LIGHTS switch ............ ARMED (guarded position) Verify UNARMED light extinguished.
PASSENGER OXYGEN ON light .............................Extinguished
CAUTION: Switch activation will cause deployment of passenger oxygen mask.
RAM AIR TURBINE UNLKD light ............................Extinguished
CAUTION: Switch activation will cause deployment of ram air turbine.
Engine ignition selector ....................................................1 OR 2
Fuel system ......................................................................... Set FUEL JETTISON* - OFF FUEL PUMP switches - OFF CROSSFEED VALVE switch(es)* - OFF
Verify VALVE light(s)* extinguished.
WING and ENGINE ANTI-ICE switches ............................. OFF
Lighting panel ....................................................................... Set
* As installed
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.6 Rev.3 March 18, 2000
POSITION light switch - ON RED and WHITE ANTI-COLLISION light switches - OFF WING light switch - As required LANDING and NOSE GEAR light switches - OFF
WINDOW HEAT switches* ...................................................ON Verify INOP lights extinguished.
CARGO HEAT switches* .......................................................ON
PASSENGER SIGNS selectors .............................................. Set NO SMOKING selector - AUTO or ON SEATBELTS selector - AUTO or ON
Pressurisation system ........................................................... Set CABIN ALTITUDE AUTO RATE control - INDEX LANDING ALTITUDE Destination airport elevation CABIN ALTITUDE MODE selector - AUTO 1 or AUTO 2
EQUIPMENT COOLING mode selector .............................AUTO
Lighting panel ....................................................................... Set LOGO light switch - ON during nighttime operation INDICATOR LIGHTS switch As desired
AIR CONDITIONING system ............................................... Set APU and ENGINE BLEED air switches - ON
Verify APU VALVE light extinguished.
Engine OFF lights remain illuminated until associated engine is started.
LEFT, CENTER and RIGHT ISOLATION switches - ON Verify VALVE lights extinguished.
PACK control selectors - AUTO Verify PACK OFF lights extinguished.
TRIM AIR switch ON RECIRCULATION FAN switches - ON
* As installed
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.7
Verify INOP lights extinguished.
COMPARTMENT temperature controls - AUTO Set as desired and verify INOP lights extinguished.
FORWARD CARGO air CONDITIONING/
VENT FAN system* .............................................................. Set
CARGO HEAT switches* .......................................................ON
Right VOR/DME ..............................................................AUTO
Right FLIGHT DIRECTOR switch .........................................ON
EICAS display...................................................................Check Indications Normal. Verify:
primary engine indications display existing conditions
no exceedance values are displayed.
Secondary ENGINE display switch Push Secondary ENGINE display Verify:
secondary engine indications display existing conditions
no exceedance values are displayed.
STATUS display switch Push STATUS display Verify:
hydraulic quantities do not display RF
oxygen pressure is sufficient for flight.
If any status message is displayed, refer to the Minimum Equipment List (and Dispatch Deviation Guide for information only or airline equivalent) to determine if dispatch relief is available.
COMPUTER selector - AUTO THRUST REFERENCE SETTING selectors - BOTH and IN
Verify TO mode annunciated.
CDU ................................................................................... Set INIT REF key Push INDEX line select key Push
* As installed
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.8 Rev.3 March 18, 2000
IDENT line select key Push IDENT page Check
Verify active date current. POS INIT line select key Push
Verify time correct. Present position Enter
Enter present position using the most accurate latitude and longitude. ROUTE line select key Push
Enter: flight number
route.
ACTIVATE line select key Push EXEC key Push DEP ARR key Push
Select runway and SID. ROUTE line select key Push
Verify SID and route are correct. EXEC key Push
PERF INIT line select key - Push Enter: reserve fuel cruise altitude cost index. step size value.
TAKEOFF line select key - Push TAKEOFF page1: Enter takeoff flap setting. TAKEOFF page2: Check and/or enter: acceleration height. runway wind. runway slope.
Flight instrument control panel ............................................... Set ADI DH Reference marker set -20 HSI RANGE selector Select:
10 NM range as pilot flying.
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.9
20 NM range as pilot non flying. HSI Mode selector - MAP WEATHER RADAR switch - OFF MAP switches - AS DESIRED
Weather radar ...................................................................... Set
Fire extinguishing system ..................................................Check ENGINE and APU fire switches - IN CARGO FIRE switches - OFF ENGINE, CARGO, and APU fire bottle discharge lights - Extinguished
VHF comms ........................................................................ Set
Audio selector panel .............................................................. Set
ADF ................................................................................... Set
Transponder ......................................................................... Set Transponder ALTITUDE SOURCE selector* ON Transponder mode selector* STBY Transponder code window - 2000
ILS ...................................................................................... Set
ACARS* ............................................................................... Set
Cockpit window ......................................... CLOSED and Locked Verify handle in locked (forward) position and WINDOW NOT CLOSED decal hidden from view.
Crew oxygen ...........................................................Test and set Mask - Stowed Normal/100% selector - 100% RESET/TEST slide lever - Push and hold
Verify yellow cross appears momentarily in flow indicator.
EMERGENCY/TEST selector - Push and hold
* As installed
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.10 Rev.3 March 18, 2000
Simultaneously push the EMERGENCY/TEST selector and RESET/TEST slide lever. Verify yellow cross appears continuously in flow indicator.
EMERGENCY/TEST selector - Release RESET/TEST slide lever - Release
Verify yellow cross no longer appears in flow indicator.
Right INSTRUMENT SOURCES SELECTOR/switches ........Check FLIGHT DIRECTOR source selector - R NAV source selector - FMC R Alternate source switches - OFF
Right flight instruments ......................................................... Set
NOTE: IRS alignment must be complete before VSI, ADI, HSI, and RDMI checks.
Altimeter - Set Set barometric indication. Verify proper altitude and no flag.
Vertical speed indicator - Check Verify indication zero and OFF flag not in view.
Clock - Set ADI - Check
Verify proper attitude, flight director command bars, flight mode displays TO, TO, FD, proper airspeed, and no flags.
HSI - Check Verify magnetic track, present heading, appropriate route and no flags. Plan mode may be selected to verify route.
Airspeed indicator* - Check Verify proper speed and no flags.
RDMI - Check Position ADF/VOR selectors, as desired. Verify present heading and no inappropriate flags.
AUTOLAND STATUS annunciator ....................................Check Verify blank indications.
HEADING REFERENCE switch .........................NORM or TRUE Position as required.
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.11
ALTERNATE GEAR EXTEND switch ................................. OFF
ALTERNATE FLAPS .......................................................Check ALTERNATE FLAPS selector - NORM ALTERNATE FLAPS switches - OFF
GROUND PROXIMITY/ CONFIGURATION GEAR OVERRIDE switch.................................................... OFF
GROUND PROXIMITY FLAP OVERRIDE switch .................................................... OFF
Seat ................................................................................Adjust Position set for optimum eye reference.
Rudder pedals ..................................................................Adjust Adjust to permit full rudder pedal and brake application.
Accomplish BEFORE START CHECKLIST TO THE LINE on command of Captain.
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.12 Rev.3 March 18, 2000
Cockpit Preparation Captain
Maintenance documents.....................................................Check
Left VOR/DME ................................................................AUTO
AFDS MCP ...................................................................................................... Set
Left FLIGHT DIRECTOR switch - ON AUTOTHROTTLE switch - ARM IAS/MACH selector - Set 100 HEADING - Set initial heading BANK LIMIT selector - AUTO ALTITUDE - Set initial altitude AUTOPILOT DISENGAGE bar - UP
CDU ................................ ................................................... Set INIT REF key Push INDEX line select key Push IDENT line select key Push IDENT page Check
Verify active date current. POS INIT line select key Push
Verify present position and time correct. ROUTE line select key Push
Verify: flight number correct
route correct.
PERF INIT line select key - Push Verify: reserve fuel correct cruise altitude correct cost index correct step size value correct.
TAKEOFF line select key - Push TAKEOFF page1: Verify takeoff flap setting correct.
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.13
TAKEOFF page2: Verify: acceleration height correct runway wind correct runway slope correct.
Flight instrument control panel ............................................... Set ADI DH Reference marker set -20 HSI RANGE selector Select:
10 NM range as pilot flying. 20 NM range as pilot non flying.
HSI Mode selector - MAP WEATHER RADAR switch - OFF MAP switches - AS DESIRED
SPEEDBRAKE lever ....................................................... DOWN
Reverse thrust levers ...................................................... DOWN
NOTE: Movement of the reverse thrust lever could result in operation of the engine thrust reverser.
Forward thrust levers ...................................................CLOSED
FLAP lever .......................................................................... Set Position lever to agree with flap position.
PARK BRAKE ...................................................................... Set Observe PARK BRAKE light illuminated.
STABILIZER TRIM CUTOUT switches ............................NORM
FUEL CONTROL switches ..........................................CUT OFF
Audio Selector Panel ............................................................. Set
Cockpit window ........................................ CLOSED & LOCKED Verify handle in locked (forward) position and WINDOW NOT CLOSED decal hidden from view.
Crew oxygen ...........................................................Test and set
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.14 Rev.3 March 18, 2000
Mask - Stowed Normal/100% selector - 100% RESET/TEST slide lever - Push and hold
Verify yellow cross appears momentarily in flow indicator.
EMERGENCY/TEST selector - Push and hold Simultaneously push the EMERGENCY/TEST selector and RESET/TEST slide lever. Verify yellow cross appears continuously in flow indicator.
EMERGENCY/TEST selector - Release RESET/TEST slide lever - Release
Verify yellow cross no longer appears in flow indicator.
Left INSTRUMENT SOURCES SELECTOR/switches ..........Check FLIGHT DIRECTOR source selector - L NAV source selector - FMC L Alternate source switches - OFF
Flight instruments ................................................................. Set
NOTE: IRS alignment must be complete before RDMI, ADI, HSI and VSI checks.
Metric altimeter* - Check Verify proper altitude and no flag.
Airspeed indicator* - Check Verify proper speed and no flags.
RDMI - Check Position ADF/VOR selectors as desired. Verify present heading and no inappropriate flags.
ADI - Check Verify proper attitude, flight director command bars, flight mode displays TO, TO, FD, proper airspeed, and no flags.
HSI - Check Verify magnetic track, present heading, appropriate route and no flags. Plan mode may be selected to verify route.
* As installed
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.15
Altimeter - Set Set barometric indication. Verify proper altitude and no flags.
Vertical speed indicator - Check Verify zero rate and no flag.
Clock - Check
AUTOLAND STATUS annunciator ...... ..............................Check Verify blank indications.
RESERVE BRAKES and STEERING switch ............................OFF Verify VALVE light extinguished.
Standby flight instruments ......... ............................................ Set Attitude indicator - Check
Verify proper attitude. Position ILS selector to OFF and verify no flags. Airspeed indicator - Check
Verify proper speed. Altimeter - Set
Set barometric indication. Verify proper altitude.
Standby engine indicator selector .......................................AUTO
AUTO BRAKES selector ..................................................... OFF
Seat ................................................................................Adjust Position seat for optimum eye reference.
Rudder pedals ...................................................................Adjust Adjust to permit full rudder pedal and brake application.
Call for BEFORE START CHECKLIST TO THE LINE.
Note: A takeoff briefing shall be accomplished by the pilot flying after the preflight check, so as not to interfere with the Before Start Procedure. It shall include: - aircraft configuration - normal departure procedure: anticipated routing - MCP setting and NAV setting - rejected takeoff procedure
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.16 Rev.3 March 18, 2000
- departure procedure with one engine inoperative - extras
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.17
Cockpit Preparation - Final This procedure is accomplished after flight documents are aboard and flight crew is ready for push back and/or engine start.
INIT REF key Push
CDU...........................................................................Set C Verify fuel quantities agree:
upload fuel quantity
EICAS
CDU.
Enter: zero fuel weight.
THRUST LIM line select key Push Select takeoff thrust:
full thrust or
assumed temperature derate. Verify correct thrust reference mode displayed.
TAKEOFF line select key Push Enter CG. Position Shift (If required) - ENTER
Select or enter takeoff speeds.
MCP............................................................................ Set C IAS/MACH selector Rotate
Set V2 speed in the IAS/MACH window.
Pushback and/or start clearance..................................Obtain C, F/O Obtain clearance from ATC and ground crew.
Before start setup................................................... Command C
HYDRAULIC system..................................................... Set F/O
Note: Pressurize right system first to prevent fluid transfer between systems.
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.18 Rev.3 March 18, 2000
Right DEMAND pump selector AUTO
Verify FAULT light extinguished.
C1 and C2 PRIMARY pump switches ON
Verify FAULT lights extinguished.
Center DEMAND pump selector AUTO
Verify FAULT lights extinguished.
Left DEMAND pump selector AUTO
Verify FAULT lights extinguished.
NOTE: Centre number two PRESS light will illuminate until an engine is started.
FUEL panel................................................................... Set F/O
LEFT and RIGHT FUEL PUMP switches ON
Verify PRESS lights extinguished.
If center tank contains fuel:
CENTER FUEL PUMP switches ON
Note: PRESS lights may not be extinguished due to load shedding. Indications will be normal after engine start.
RED ANTI-COLLISION light switch..............................ON F/O
PACK CONTROL selectors.......................................... OFF F/O
Trim ..................................................____ Units, zero, zero C
Stabilizer trim ___ UNITS
Set for takeoff.
Check in illuminated greenband.
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.19
Aileron trim ZERO
Rudder trim ZERO
Recall.......................................................................Check C
Verify only appropriate alert messages displayed.
RECALL/CANCEL switch Push
Verify messages cancelled.
Secondary Engine Display .............................................ON C
Call for BEFORE START CHECKLIST BELOW THE LINE. C
Accomplish remaining items on BEFORE START checklist.F/O
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.20 Rev.3 March 18, 2000
ENGINE START
Engine Start Procedure The term L (R) engine is used with ground personnel and in the cockpit. The normal start sequence is right then left.
Captain First Officer
Call START _____ ENGINE. Position _____ START selector to GND. Push CLOCK switch.
Observe oil pressure increase.
Position _____ FUEL CONTROL switch to run at maximum motoring N2** ( 15% minimum).
Push CLOCK switch..
Monitor engine displays for normal indications until stabilized at idle.
Reset CLOCK. Reset CLOCK.
Note: **Maximum motoring speed is reached when N2 acceleration is less than approximately 1% in five seconds.
Note: Do not advance thrust beyond that required for taxi until 50C oil temperature.
Monitor engine displays for start parameters listed below until engine is stabilized at idle:
Oil pressure should rise before selecting RUN.
EGT should rise within 20 seconds after selecting RUN.
N1 rotation must increase at EGT rise.
EGT must stay within limits.
N2 should reach idle within two minutes after selecting RUN.
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.21
Repeat procedure to start remaining engine.
Note: Momentary ENGINE STARTER message may occur on initiation of second engine start.
After Start Procedure
After start setup .................................................. Command C
APU selector............................................................... OFF F/O
ENGINE ANTIICE selectors .............................As required F/O
Left and Right Isolation switches .................................. OFF F/O
Pack Control Selector ................................................AUTO F/O
EICAS Display..........................................................Check C Recall Switch PUSH
Verify only appropriate alert messages displayed. Status Display ON
Flight controls...........................................................Check C Displace control wheel and control column to full travel in both directions and verify:
freedom of movement
controls return to center.
Hold the nose wheel steering tiller during rudder check to prevent undesired nose wheel movement. Displace rudder pedals to full travel in both directions and verify:
freedom of movement
rudder pedals return to center.
EICAS Display.............................................................. Set C Secondary Engine Display - ON
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.22 Rev.3 March 18, 2000
Auto Brakes Selector ...................................................RTO C
Ground equipment.......................................................Clear C
Call for AFTER START CHECKLIST. C
Accomplish AFTER START checklist. F/O
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.23
TAXI-OUT AND TAKEOFF
Before Takeoff Procedure
Captain First Officer
Obtain taxi clearance.
Position ELAPSED TIME selector to RUN with start of taxi or start of pushback whichever occurs first.
Brief taxi clearance.
Verify and call "LEFT SIDE CLEAR".
Verify and call "RIGHT SIDE CLEAR".
Position TAXI and RUNWAY TURN OFF light switches ON.
Release parking brake.
Call for FLAPS _____ as required for takeoff.
Position flap lever to takeoff setting and call "FLAPS _____ SET", when flaps have reached the commanded position.
Notify cabin crew to be seated for takeoff.
Call for BEFORE TAKEOFF CHECKLIST.
Accomplish BEFORE TAKEOFF checklist.
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.24 Rev.3 March 18, 2000
Takeoff Procedure
Captain First Officer
Position LEFT and RIGHT LANDING light switches ON and TAXI light switch OFF.
Verify TFC displayed on HSI.
Select WXR as required.
Align airplane with runway.
Position STROBE light switch ON.
Position transponder mode selector to TA/RA.
Verify TFC displayed on HSI.
Select WXR as required.
After takeoff clearance received call "YOUR CONTROLS" if the first officer is the pilot flying.
Reply "MY CONTROLS" if pilot flying.
Position ELAPSED TIME selector to RUN.
Release brakes.
Advance thrust levers to approximately 1.1 EPR.
Push EPR/THR switch.
Adjust takeoff thrust prior to 80 knots, if required.
Pilot flying Pilot not flying
Verify correct takeoff thrust set.
Monitor engine instruments throughout takeoff.
Verify 80 knots and call CHECKED. Call "80 KNOTS".
Monitor airspeed.
Rotate at VR.
Establish a positive rate of climb.
Call "V1".
At VR call "ROTATE".
Monitor airspeed and vertical speed.
Continued
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.25
Pilot flying Pilot not flying
Verify positive rate of climb.
Call for GEAR UP.
Call "POSITIVE RATE", when a positive rate of climb is indicated on the pressure altimeter and VSI.
Position landing gear lever UP.
Maintain V2 +15 to 25
After climb stabilized, at 400 feet call for LNAV or HEADING SELECT, HEADING _____".
Push LNAV or heading select switch.
Set heading as required.
At flap retraction altitude, call for VNAV or FLCH".
Push VNAV or FLCH.
Call for "FLAPS _____" according to flap retraction schedule.
Position flap lever as directed and call "FLAPS _____ SET", when flaps have reached the commanded position.
After flap retraction call "ENGAGE CENTER A/P".
Engage center A/P.
Call for AFTER TAKEOFF
CHECKLIST.
Accomplish AFTER TAKEOFF
checklist.
Note: LNAV shall be used if it is obvious that LNAV track can be followed after takeoff.
Heading select shall be used as a preference over LNAV if: - large heading changes have to be executed immediately after takeoff - clearance by ATC to follow a specific heading after takeoff - departure procedure or route does not commence at the end of runway - initial turning points are determined by DME distance (noise abatement)
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.26 Rev.3 March 18, 2000
CLIMB AND CRUISE
Climb Procedure
Pilot Flying Pilot Not Flying
Set altimeters to standard and call "STANDARD", flight level "_____".
Call "TRANSITION" at transition altitude.
Verify altimeter setting and indication and call "CHECKED".
Verify altitude and call "CHECKED". Call "10.000" feet or flight level "100".
Captain First Officer
At 10.000 feet or flight level 100 position LANDING and RUNWAY TURNOFF light switches OFF.
At flight level 200 and no turbulence expected, position SEAT BELTS selector to AUTO.
Note: If required the SEAT BELTS selector maybe switched to AUTO below flight level 200 but above flight level 100/10000 ft if no turbulences expected.
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.27
Cruise Procedure
Pilot Flying Pilot Not Flying
At or before center tank fuel quantity reaches 500kgs, position CENTER FUEL PUMP switches OFF.
During the last hour of cruise on all Extended Range (more than one hour from adequate airport) flighs, perform Fuel Crossfeed Valve Check.*
Note: The fuel crossfeed valve check is not required on airplanes with two fuel crossfeed valves.
Note: During cruise in case of turbulences, no smoking and seat belts sign selectors will be operated by the captain also when acting as pilot flying.
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.28 Rev.3 March 18, 2000
APPROACH AND LANDING
Descent Procedure
Pilot Flying Pilot Not Flying
Prior to top of descent, modify active route as required for arrival and approach.
Review active route as required for arrival and approach.
Set VOR/ADF switches. Set RADIO or BARO minimum as required for approach. Select marker beacon on audio control panel.
Select VREF speed. Verify VREF speed.
Set AUTOBRAKE selector to desired brake setting.
Accomplish approach briefing.
When cleared to descend, set clearance limit altitude on MCP.
Captain First Officer
Position SEAT BELTS selector ON or cycle if already on.
Note: An approach briefing shall include:
- clearance limit - type of approach/ runway in use - highest sector altitude and actual sector altitude - initial approach altitude - inbound track - FAF/FAP or Outer Marker altitude - approach minimum, as applicable (MDA/DA/DH) - missed approach procedure - NAV setting - extras (to include braking & taxi procedure)
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.29
Pilot Flying Pilot Not Flying
Verify altitude and call "CHECKED". Call "10.000" feet or flight level "100".
Captain First Officer
At 10.000 feet or flight level 100 position LANDING and RUNWAY TURNOFF light switches ON.
Pilot Flying Pilot Not Flying
Verify correct arrival and approach procedures selected. Verify NAV aids are tuned and identified.
Set altimeters and call QNH setting "____ , _____" feet.
If transition level will be passed before an approach clearance or an clearance down to an altitude:
call "TRANSITION" at transition level.
Verify altimeter setting and indication and call "CHECKED".
or
If an approach clearance or an clearance down to an altitude has been received before passing the transition level:
Set altimeters and call QNH setting "____ , _____ " feet.
Verify altimeter setting and indication and call "CHECKED".
Call for "APPROACH CHECKLIST". Accomplish APPROACH checklist.
Captain First Officer
At 5000 feet or flightlevel 050 Position NO SMOKING selector ON Or cycle if already ON
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.30 Rev.3 March 18, 2000
Landing Procedure
Pilot Flying Pilot Not Flying
Call for FLAPS _____ according to flap extension schedule.
Position flap lever as directed and call "FLAPS _____ SET", when flaps have reached the commanded position.
When on localizer intercept heading with localizer and glideslope pointers displayed and approach clearance received arm APP mode.
Verify localizer capture and call CHECKED.
Call LOCALIZER CAPTURE.
At glideslope alive, call for:
GEAR DOWN
FLAPS 20.
Position landing gear lever DOWN. Position NO SMOKING selector AUTO and ON, for non-smoking flights only. Position flap lever to 20 and call "FLAPS 20 SET", when flaps have reached the commanded position.
Captain First Officer
Position speedbrake lever to ARM.
Pilot Flying Pilot Not Flying
Verify glideslope capture and call CHECKED.
Call GLIDESLOPE CAPTURE.
Call for FLAPS _____ as required for landing.
Position flap lever as commanded and call "FLAPS _____ SET", when flaps have reached the commanded position..
Set missed approach altitude on MCP. Verify missed approach altitude set and call _____ feet, FL _____ , CHECKED.
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.31
Call for LANDING CHECKLIST Accomplish LANDING checklist.
Monitor approach progress.
Verify AFDS status at 500 feet radio altitude.
Verify altitude and call CHECKED. Call 500feet, FLARE/ROLLOUT ARMED. (Autoland callout only)
Captain First Officer
Position NOSE LANDING light switch ON during night operation.
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.32 Rev.3 March 18, 2000
Go - Around Procedure
Pilot Flying Pilot Not Flying
Push GA switch.
Call for GO-AROUND,
FLAPS 20.
Position flap lever to 20 and call "FLAPS 20 SET" when flaps have reached the commanded position.
Verify rotation to goaround attitude and thrust increase. Verify thrust adequate for goaround and adjust if necessary.
Verify positive rate of climb.
Call for GEAR UP.
Call "POSITIVE RATE", when a positive rate of climb is indicated on the pressure altimeter and VSI.
Position landing gear lever UP.
At 400 feet, select LNAV or HDG SEL.
At flap retraction altitude, set speed bug to the maneuvering speed for the desired flap setting.
Call for FLAPS _____ according to flap retraction schedule.
Position flap lever as directed, and call "FLAPS _____ SET", when flaps have reached the commanded position.
After flap retraction and missed approach altitude captured, call for appropriate reference thrust mode .
(in case of continuous climb to CRZ altitude set climb thrust and then FLCH observe 10 MIN Thrust Limit)
Set appropriate thrust on TMSP.
Verify missed approach route being tracked and missed approach altitude captured.
Call for AFTER TAKEOFF CHECKLIST.
Accomplish AFTER TAKEOFF checklist.
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.33
Landing Roll Procedure
Pilot Flying Pilot Not Flying
Monitor rollout progress and proper autobrake operation.
Verify thrust levers closed and speedbrake lever up.
Without delay, raise reverse thrust levers to the interlocks, hold light pressure until release, and then apply reverse thrust as required.
Verify speedbrake lever up. If speedbrakes are not extended, call SPEEDBRAKES and the captain positions the speedbrake lever to up.
Verify 60 knots and call CHECKED. Initiate movement of reverse thrust levers to reach reverse idle detent by taxi speed.
Position levers full down (forward thrust) when engines have decelerated to reverse idle.
Call 60 KNOTS.
Prior to taxi speed, disarm the autobrake and continue manual braking as required.
Disconnect autopilot prior to runway turnoff.
Captain First Officer
Call "MY CONTROLS" at taxi speed. Reply "YOUR CONTROLS".
WARNING: After reverse thrust is initiated, a full stop landing must be made.
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.34 Rev.3 March 18, 2000
After Landing Procedure
Accomplished when clear of the active runway.
Captain First Officer
Position speedbrake lever DOWN. Start APU.
Position TAXI light switch ON and LANDING light switches OFF.
White Anti-Collision light switch OFF.
Position ELAPSED TIME selector to HOLD.
Select weather radar OFF.
Position AUTOBRAKE selector OFF. Position flap LEVER UP.
Select weather radar OFF. Position transponder mode selector to STBY and set transponder code 2000.
Assists Captain by finding cleared taxiways and parkposition with taxi chart.
Position TAXI and RUNWAY TURNOFF light switches OFF approaching parking position.
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.35
TAXI-IN AND PARK
Shutdown Procedure
Parking brake................................................................ Set C Verify PARK BRAKE light illuminated
ELAPSED TIME selector...........................................HOLD F/O
ENGINE ANTI-ICE selectors....................................... OFF F/O
Electrical power .................................................... Establish F/O
If APU power is required:
Check APU RUNNING.
If external power is desired: F/O
EXTERNAL POWER AVAIL light Illuminated
EXTERNAL POWER switch Push
FUEL CONTROL switches ....................................CUTOFF C Verify ENG and SPARE VALVE lights extinguished
SEAT BELT SIGN selector .......................................... OFF C
HYDRAULIC system..................................................... Set F/O
Note: Depressurize right system last to prevent fluid transfer between systems.
Left DEMAND pump selectors OFF
Center DEMAND pump selectors OFF
C1 and C2 PRIMARY pump switches OFF
Right DEMAND pump selector OFF
FUEL PUMP switches ................................................. OFF F/O
RED ANTI-COLLISION LIGHT switch........................ OFF F/O
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.36 Rev.3 March 18, 2000
Left and Right Isolation switches ....................................ON F/O
Right FLIGHT DIRECTOR switch................................ OFF F/O
Speed bugs .......................................................Set together F/O
Reference altitude marker ............... Set to 12 oclock position F/O
Elapsed Time ............................................................ Reset F/O
CDU...........................................................................Set F/O Set EICAS page Flight times
ADI DH Reference marker ........................................Set -20 F/O
ADF selectors*............................................................ANT F/O
ILS selector.............................................................. PARK F/O
Left FLIGHT DIRECTOR switch ................................. OFF C
Speed bugs .......................................................Set together C
Reference altitude marker ............... Set to 12 oclock position C
Elapsed Time ............................................................ Reset C
STATUS DISPLAY.....................................................Push C
CDU...........................................................................Set C Set PROG page 2/2
IAS/MACH selector................................................. Set 100 C
Parking brake ......................................................... Release C When wheel chocks in place, release the parking brake.
Call for SHUTDOWN CHECKLIST. C
Accomplish SHUTDOWN checklist. F/O
* As installed
Lauda Air BOEING 767 Normal Procedures Operations Manual Amplified Procedures
March 18, 2000 Rev.3 NP.20.37
Note: One pilot must be present on the flightdeck with passengers on board.
Cockpit must be left in a clean manner and both pilots are responsible for:
Interior cockpit lights are turned off.
Charts to be returned to their correct place in the Jeppesen binder.
Cups and waste to be removed and cockpit left in a tidy and clean state.
Normal Procedures Lauda Air BOEING 767 Amplified Procedures Operations Manual
NP.20.38 Rev.3 March 18, 2000
Secure Procedure
Accomplish only when aircraft will be left unattended .
IRS selectors .............................................................. OFF F/O
Left HF ...................................................................... OFF F/O
EMERGENCY LIGHTS switch..................................... OFF F/O
WINDOW HEAT switches.......................................... OFF F/O
Right HF .................................................................... OFF F/O
PACK CONTROL selectors.......................................... OFF F/O
CARGO HEAT switches .............................................. OFF F/O
APU selector/ External Power switch ............................ OFF F/O When APU RUN light extinguishes:
STANDBY POWER selector..................................AUTO F/O
BATTERY switch................................................... OFF F/O
Call for SECURE CHECKLIST. ........................................ C
Accomplish SECURE checklist. ........................................... F/O
L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Operations Manual
Normal Procedures Chapter NP Flight Patterns Section 30
October 15, 1997 NP.30.1
Takeoff F
lap
Ret
ract
ion
Sche
dule
Sele
ct n
ext f
lap
posi
tion
whe
n
With
in 2
0 kn
ots
of th
e m
aneu
verin
g
Spee
d fo
r th
at p
ositi
on a
nd
Acc
eler
atin
g.
Normal Procedures L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Flight Patterns Operations Manual
NP.30.2 October 15, 1997
ILS Approach
L a u d a A i r B O E I N G 7 6 7 L a u d a A i r B O E I N G 7 6 7 Normal Procedures Operations Manual Flight Patterns
October 15, 1997 NP.30.3
Non-Precision Approach
Mis
sed
appr
oach
-
Push
GA
sw
itch
(AFD
S)-
Flap
s 20
- G
o-ar
ound
atti
tude
- G
o-ar
ound
thru
st-
Pose
tive
rate
of
clim
b, g
ear u
p-
At 4
00 f
eet s
elec
t rol
l m
ode
(AFD
S)- A
t fla
p re
trac
tion
alti
tude
, set
spe
ed b
ug f
or
des
ired
flap
set
ting
- R
etra
ct f
laps
on
sche
dule
- A
fter
fla
p re
trac
tion,
set
clim
b th
rust
- Sel
ect V
NA
V o
r FL
CH
as
req
uire
d-
Ver
ify
trac
king
rou
te a
nd
alti
tutd
e ca
ptur
e- A
fter
Tak
eoff
che
cklis
t
Normal Procedures L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Flight Patterns Operations Manual
NP.30.4 October 15, 1997
Circling
L a u d a A i r B O E I N G 7 6 7 L a u d a A i r B O E I N G 7 6 7 Normal Procedures Operations Manual Flight Patterns
October 15, 1997 NP.30.5
Mis
sed
appr
oach
-
Push
GA
sw
itch
(AFD
S)-
Flap
s 20
- G
o-ar
ound
atti
tude
- G
o-ar
ound
thru
st-
Pose
tive
rate
of
clim
b, g
ear u
p-
At 4
00 f
eet s
elec
t rol
l m
ode
(AFD
S)- A
t fla
p re
trac
tion
alti
tude
, set
spe
ed b
ug f
or
des
ired
flap
set
ting
- R
etra
ct f
laps
on
sche
dule
- A
fter
fla
p re
trac
tion,
set
clim
b th
rust
- Sel
ect V
NA
V o
r FL
CH
as
req
uire
d-
Ver
ify
trac
king
rou
te a
nd
alti
tutd
e ca
ptur
e- A
fter
Tak
eoff
che
cklis
t
Normal Procedures L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Flight Patterns Operations Manual
NP.30.6 October 15, 1997
Circling Approach Plan View
Missed approach - Push GA switch (AFDS)- Flaps 20- Go-around attitude- Go-around thrust- Posetive rate of climb, gear up- At 400 feet select roll mode (AFDS)- At flap retraction altitude, set speed bug for desired flap setting- Retract flaps on schedule- After flap retraction, set climb thrust- Select VNAV or FLCH as required- Verify tracking route and altitutde capture- After Takeoff checklist
L a u d a A i r B O E I N G 7 6 7 L a u d a A i r B O E I N G 7 6 7 Normal Procedures Operations Manual Flight Patterns
October 15, 1997 NP.30.7
Visual Traffic Pattern
Go-
arou
nd
- Pu
sh G
A s
witc
h (A
FDS)
- Fl
aps
20-
Go-
arou
nd a
ttitu
de-
Go-
arou
nd th
rust
- Po
setiv
e ra
te o
f cl
imb,
gea
r up
- Po
sitio
n F/
D s
witc
hes
ON
- A
t 400
fee
t sel
ect r
oll
mod
e (
AFD
S)-
At f
lap
retr
actio
n a
ltitu
de, s
et
spee
d bu
g fo
r de
sire
d fl
ap s
ettin
g-
Ret
ract
fla
ps o
n sc
hedu
le-
Aft
er f
lap
retr
actio
n, s
et c
limb
thru
st- S
elec
t VN
AV
or F
LC
H a
s r
equi
red
- V
erif
y tr
acki
ng r
oute
and
a
ltitu
tde
capt
ure
- A
fter
Tak
eoff
che
cklis
t
L a u d a A i rL a u d a A i r B O E I N G 7 6 7 B O E I N G 7 6 7 Operations Manual
Normal Procedures Chapter NP Standard Callouts Section 40
January 13, 2000 Rev.3 NP.40.1
Standard Callouts
Both crewmembers should be aware of altitude, airplane position and situation. Avoid casual and non-essential conversation during critical phases of flight, particularly during taxi, takeoff, approach and landing. Unnecessary conversation reduces crew efficiency and alertness and is prohibited when below 10,000 feet.
The pilot not flying should accomplish callouts based on instrument indications or observations for the appropriate condition. The pilot flying should verify the condition/location from his instruments and acknowledge. If the pilot not flying does not make the required callout, the pilot flying should make it.
One of the basic fundamentals of the Crew Coordination Concept is that each crewmember must be able to supplement or act as a back-up for the other crewmember. Proper adherence to standard callouts is an essential element of a well-managed cockpit. These callouts provide both crewmembers required information about airplane systems and about the participation of the other crewmember. The absence of a standard callout at the appropriate time may indicate a malfunction of an airplane system or indication, or indicate the possibility of incapacitation of the other crewmember.
When optional GPWS voice callouts occur during approach, the pilot flying should acknowledge the electronic callout. If the normally expected electronic voice callout is not heard by the flight crew, the pilot not flying should make the callout.
When the aircraft is aligned by the captain and the first officer is PF, the captain has to decide when he will handover the controls to the first officer by the callout Your Controls and the first officer has to confirm this by the callout My Controls.
If the first officer is PF for the approach the captain has to decide when the controls can be taken over after landing by the callout My Controls and the first officer has to confirm this by the callout Your Controls.
Normal Procedures L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Standard Callouts Operations Manual
NP.40.2 Rev.3 January 13, 2000
Standard Callouts Summary
Condition/Location Callout (PNF)
Response (PF)
Takeoff 80 knots Checked 1)
V1
Rotate
Positive rate Gear up
Climb and Descent 1.000 to level off Checked
100/10.000 Checked
Approach
FD/ILS Localizer capture Glide slope capture
Checked Checked
ILS raw data Localizer intercept Glide slope intercept
Checked Checked
Precision approach Outer Marker / FAP _____ (feet) 2) , _____ (QNH)
Checked
Non precision approach VOR / NDB / FAF _____ (feet) 2) , _____ (QNH)
Checked
500 feet 500 Flare / rollout armed 3)
Checked 1)
100 feet above DH/MDA Approaching minimum Checked
DH/MAP Minimum Contact/Go -around 4)
Landing roll 60 knots Checked
After 500 feet above field elevation the pilot not flying calls out significant deviations from programmed airspeed, descent and instrument indications. Note: 1) Incapacitation check 2) Instrument approach chart altitude has to be called out 3) Autoland callout only 4) Not required, if runway in sight and confirmed by both pilots
L a u d a L a u d a A i r B O E I N G 7 6 7 A i r B O E I N G 7 6 7 Normal Procedures Operations Manual Standard Callouts
January 13, 2000 Rev.3 NP.40.3
Standard Phraseology A partial list of recommended words and phrases follows:
THRUST SETTINGS: (If Autothrottle System not available and/or Nonstandard procedures required )
Set takeoff thrust
Set (or select) go-around thrust
Set (or select) maximum continuous thrust
Set (or select) climb thrust
Set cruise thrust
AFDS SETTINGS:
Engage ___ autopilot
Arm autothrottle arm switch
Flight director switches on/off
Arm approach
Arm localizer
FLAP SETTINGS:
Flaps one
Flaps fifteen
Flaps twenty-five
Flaps up
Flaps five
Flaps twenty
Flaps thirty
AIRSPEED SETTINGS 80 Knots
V1
Rotate
Set VREF plus (additive) or
Set _____ knots
Set flaps_____speed
Normal Procedures L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Standard Callouts Operations Manual
NP.40.4 Rev.3 January 13, 2000
60 Knots
L a u d a L a u d a A i r B O E I N G 7 6 7 A i r B O E I N G 7 6 7 Normal Procedures Operations Manual Standard Callouts
January 13, 2000 Rev.3 NP.40.5
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Lauda Air BOEING 767 Operations Manual
Normal Procedures Chapter NP Cockpit/Cabin Reports and Signals Section 50
November 01, 1997 NP.50.1
Cockpit/Cabin Reports and Signals
Condition/location Captain Cabin
Before Boarding Emergency Equipment
checked and ok
Apron Close doors
XXX Pax on board and seated
Taxi-out
Cabin crew be seated for takeoff
Send CABIN READY message
Inflight Promotion video finished
At top of descent Position SEAT BELTS selector
ON or cycle if already ON
Approach (at 5000 feet
or flightlevel 050)
Position NO SMOKING
Selector ON or cycle if already ON
Send CABIN READY
message
Parking position Position SEAT BELT
Selector OFF
Open doors (ensure that slides are disarmed)
Normal Procedures L a u d a A i r B O E I N G 7 6 7L a u d a A i r B O E I N G 7 6 7 Cockpit/Cabin Reports and Signals Operations Manual
NP.50.2 November 01, 1997
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B767 Non Normal Procedures
767 1 NNP , Rev.2 Date 13.01.00, Page 1
TABLE OF CONTENTS B767 WORKBOOK CHAPTER 1: PROCEDURES B767 Non Normal Procedures
TABLE OF CONTENTS......................................................................................................... 1
1 INTRODUCTION ....................................................................................................................... 3
2 GENERAL COCKPIT PROCEDURES.......................................................................................... 3
3 REJECTED TAKEOFF ............................................................................................................... 4
4 MALFUNCTION HANDLING ...................................................................................................... 4
5 LOW ALTITUDE LEVEL OFF AFTER TAKEOFF......................................................................... 4
6 AUTOPILOT............................................................................................................................. 5
7 GO-AROUND............................................................................................................................ 5
ONE ENGINE GO-AROUND (WEIGHT AT OR BELOW MAXIMUM LANDING WEIGHT) .................. 5 ONE ENGINE GO-AROUND (WEIGHT ABOVE MAXIMUM LANDING WEIGHT) ............................. 5
8 HIGH ALTITUDE ENGINE FAILURE AND DRIFT DOWN PROCEDURE......................................... 6
9 RAPID DEPRESSURIZATION / EMERGENCY DESCENT............................................................. 7
10 FLAP/SLAT ASYMMETRY/DISAGREE....................................................................................... 8
B767 Non Normal Procedures
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I N T E N T I O N A L Y
L E F T
B L A N K
B767 Non Normal Procedures
767 1 NNP , Rev.2 Date 13.01.00, Page 3
1 INTRODUCTION LAUDA AIR has laid down the following additional procedures, in order to supplement the B767 Operations Manual and Boeing 767 Flight Crew Training Manual. With the exception of the procedures obtained in this section, no other deviation from any procedures in the above-mentioned manuals is recommended. Terms: CDR Commander=Pilot in left hand seat COP Co-pilot=Pilot in right hand seat PF Pilot flying PNF Pilot not flying
2 GENERAL COCKPIT PROCEDURES All Non-Normal Checklist items and responses have to be read by the PNF. The PF commands and verifies the required action.
When the need for a recall* action arises, both pilots identify the problem.
PF ...................................................... "Name of the checklist-recall items" PNF .............. "Checklist item" and set action after confirmation* with the PF When complete: PNF ..................................................................... "Recall items complete" * Except "Rapid Depressurization or Emergency Descent" refer to Non-normal procedures. Example: PNF ................................................ "left engine severe damage - confirm?" PF ................................................."left engine severe damage - confirmed" PF .............................................. "left engine severe damage - recall items" PNF ..................................................................... "left thrust lever - close" PF ............................................................................................... "close" PNF ...............................................................................................action PNF ........................................................... "left fuel control switch - cutoff" PF ............................................................................................ "cut - off" PNF ...............................................................................................action PNF ............................................................... "left engine fire switch - pull" PF .................................................................................................. "pull" PNF ...............................................................................................action PNF .............................. "left engine severe damage recall items completed" Note: Recall items on GND are performed by the CDR after confirmation with the COP(e.g. engine
severe damage) except passenger evacuation where both pilots have separate tasks. Distress Message (MAYDAY,...) should be sent in a case of serious and/or imminent danger and when requiring immediate assistance (e.g. engine failure, emergency descent,...).
B767 Non Normal Procedures
Page 4 , Date 13.01.00 767 1 NNP , Rev.2
3 REJECTED TAKEOFF Only the CDR will decide, if a takeoff has to be rejected. If the CDR decides to reject a takeoff, he will call "STOP" and carry out the rejected takeoff procedure.
4 Malfunction handling No recall items or malfunction identification after V1 shall be commenced before the gear is selected up and the aircraft is established in a climb. Thereafter items shall be handled by the PNF automatically in case of engine failure:
- APU.....................................................................................................START
- A/T arm switch......................................................................................... OFF - bank limit selector .................................................................15 IF REQUIRED Single engine clean up after takeoff (straight out climb): at S/E clean up altitude - select ALTHLD or V/S (0-200) FPM - select speed Vref 30+80 or 225 whichever is lower - clean up - select FLCH - bank limit selector - auto - set MCT Single engine clean up after takeoff (special turn procedure):
If a turn is required after takeoff, delay acceleration and single engine clean up until first turn is completed.
5 LOW ALTITUDE LEVEL OFF AFTER TAKEOFF When ALTCAPT occurs with the autothrottle still in THRHOLD:
- press SPD and select speed to Vref 30+80 or 225 kts, whichever is lower - clean up - alternatively, disconnect A/T, reduce thrust manually and select speed as above - clean up
When ALTCAPT occurs after V-NAV selection: - select speed VREF 30+80 or 225 kts, whichever is lower - clean up
B767 Non Normal Procedures
767 1 NNP , Rev.2 Date 13.01.00, Page 5
6 AUTOPILOT The use of autopilot is also recommended during single engine operation. The PF shall coordinate rudder and thrust (no rudder channel available).
7 GO-AROUND
ONE ENGINE GO-AROUND (WEIGHT AT OR BELOW MAXIMUM LANDING WEIGHT) Follow published missed approach procedure or ATC instruction.
- At or above 400ft: -select a roll mode -PNF checks flight directors on - At or above 1000ft: -set speed to Vref 30+80 -clean up - After clean up complete: -FLCH (at Vref 30+80)
-bank limit selector - auto -select MCT (TMSP)
ONE ENGINE GO-AROUND (WEIGHT ABOVE MAXIMUM LANDING WEIGHT) Coordinate with ATC and follow applicable contingency procedure as for takeoff on the same runway.
- At or above 400ft: -select a roll mode -PNF checks flight directors on - At S/E clean up ALT: -select ALT HLD or V/S (0-200) FPM -set speed to 225kts -clean up - After clean up complete: -FLCH (at VREF 30+80) -bank limit selector - auto
-select MCT (TMSP)
B767 Non Normal Procedures
Page 6 , Date 13.01.00 767 1 NNP , Rev.2
8 HIGH ALTITUDE ENGINE FAILURE A