767 Work Book - Training

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


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 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.


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


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


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.



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).



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



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



Area of Responsibility and Panel Scan



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


NP.20.4 Rev.3 March 18, 2000

Verify standby power bus OFF light extinguished.


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


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


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


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.


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


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.


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.


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.


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


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


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


NP.20.16 Rev.3 March 18, 2000

- departure procedure with one engine inoperative - extras


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.


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


Left DEMAND pump selector AUTO


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.


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


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.


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


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


March 18, 2000 Rev.3 NP.20.23

TAXI-OUT AND TAKEOFF

Before Takeoff Procedure


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.


NP.20.24 Rev.3 March 18, 2000

Takeoff Procedure


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


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)


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".


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.


March 18, 2000 Rev.3 NP.20.27

Cruise Procedure


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.


NP.20.28 Rev.3 March 18, 2000

APPROACH AND LANDING

Descent Procedure


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.


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)


March 18, 2000 Rev.3 NP.20.29


Verify altitude and call "CHECKED". Call "10.000" feet or flight level "100".


At 10.000 feet or flight level 100 position LANDING and RUNWAY TURNOFF light switches ON.


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.


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.


Call for "APPROACH CHECKLIST". Accomplish APPROACH checklist.


At 5000 feet or flightlevel 050 Position NO SMOKING selector ON Or cycle if already ON


NP.20.30 Rev.3 March 18, 2000

Landing Procedure


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.


Position speedbrake lever to ARM.


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.


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)


Position NOSE LANDING light switch ON during night operation.


NP.20.32 Rev.3 March 18, 2000

Go - Around Procedure


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.


March 18, 2000 Rev.3 NP.20.33

Landing Roll Procedure


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.


Call "MY CONTROLS" at taxi speed. Reply "YOUR CONTROLS".

WARNING: After reverse thrust is initiated, a full stop landing must be made.


NP.20.34 Rev.3 March 18, 2000

After Landing Procedure

Accomplished when clear of the active runway.


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.


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


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


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.


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


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


NP.30.4 October 15, 1997

Circling


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


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


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

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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


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


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


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


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


Intentionally Blank

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

Intentionally Blank

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


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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


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,...).


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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


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)


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8 HIGH ALTITUDE ENGINE FAILURE A

Documents

767 Work Book - Training