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Austrian virtual B767-300 Expanded Checklist 1

REV 19.05.2014 FOR FLIGHT SIMULATOR ONLY! © Dietmar Walch

Boeing 767-300

Expanded Checklist

Austrian virtual operated by Tyrolean

Issue 1



0.1 General information to use the “Austrian Virtual Checklist Boeing 767-300”.

0.2 This Checklist comprised the normal procedures to be followed when flying the Level-D

767-300 in the flight simulator. Not required items for flight simulation are cancelled. This

Checklist does not include procedures that are being done before or after your start or finish

the actual task. It´s not a “to do list”! Depending on different start up user settings, refer to

the “Level-D 767-300” AOM for correct system operation. Therefore the “Power-Up”

procedure is not part of the checklist. This Checklist should be used for flight simulation

only!

0.3 Perform following scan flow to check the cockpit systems:

1. Side panels,

2. Overhead Panel (from left upper to right lower side)

3. Glareshield Panel (AFDS Panel)

4. Main Instrument Panel

5. Pedestal (from forward to aft)

Following will be covered by this manual:

1.1 Preflight

1.2 Cockpit Preparation

1.3 Crew at Station

1.4 Before Engine Start

1.5 After Engine Start

1.6 Taxi

1.7 Before Take-Off

1.8 Climb

1.9 Descent

1.10 Approach

1.11 Final

1.12 After Landing

1.13 Transit parking

1.14 Final Parking

2.1 Wind Limitation Graph

2.2 Max Airspeed Limits & Flap Extension Limits

2.3 Cruise Level capability with all Engines & Graph

4.0 List of Abbreviations



1.1 RREFLIGHT CHECK LIST

The “Preflight Check List” has to be executed to ensure all relevant add-on software is active and

ready to perform the simulated flight in the virtual surround successful.

PARKING BRAKE ................................................................................................. SET

Necessary for FSFK / XCARS starting!

ENGINES ...................................................................................................... CUT OFF

Check Fuel Levers in the OFF position and engine values down – it´s important for proper function of

FSFK / XCARS. If you found Engine running, connect External Power or activate APU before Engine

shut-down. Otherwise you will be lost the electrical power. Realignment of IRS required!

OFP / LOAD SHEET ................................................................................. ON BOARD

Check data for limit and insert OFP and A/C Data into FMC.

RE-FUELING .......................................................................................... PERFORMED

Due to some single tank re-fueling problems, perform fueling during A/C selection in FS window.

VAT SERVER ......................................................................................... CONNECTED

FLIGHT PLAN ..................................................................................................... SENT

Compare data with the OFP and verify “sent” message.

WX GENERATOR .................................................................................................. SET

Connect desired weather add-ons.

LOCAL QNH .............................................................................. SET AND CHECKED

Set current QNH of departure airport and check all three altimeters.

XACARS / FSFK ............................................................................................. ACTIVE

XACARS or FSFK open, Flight Plan data checked and ready for start.



1.2 COCKPIT PREPARATION

The entire “Cockpit Preparation Check List” has to be executing for initial acceptance of the aircraft

before first online flight, or if start with a cold and dark cockpit.

IRS MODE SELECTOR ........................................................................................ NAV

Check all 3 IRS mode selectors on NAV and no FAULT or ALIGN light illuminated.

YAW DAMPER SWITCHES ............................................................................ L&R ON

EEC SWITCHES ............................................................................................. L&R ON

HYDRAULIC PANEL .................................................................................. CHECKED

- Primary Engine Pumps switches ON

- Primary Electrical Pumps switches OFF (see Note below)

- All 3 Demand Pumps switches OFF

Note: If FSPassenger in use switch one Primary Electrical Pump to ON, otherwise expect

malfunctions.

OVERHEAD CAUTIONS ............................................................................ CHECKED

Check for normal indication of Caution Lights.

EVACUATION SIGNS ................................................................................. CHECKED

Switch should be guarded OFF and test the EVAC light.

BATTERY SWITCH ................................................................................................ ON

STBY POWER SELECTOR ............................................................................... AUTO

ELECTRICAL PANEL ................................................................................. CHECKED

All electrical switches should be switched to ON or AUTO. Electrical switches are only turned OFF for

abnormal conditions.

EXT POWER OR APU ......................................................................... AS REQUIRED

- EXT Power: Check AVAIL light on. Press EXT PWR button to ON.

- APU Power: Use APU during push-back for engine starts and if Ground Air Starter not

available.

COCKPIT VOICE RECORDER ...................................................................... TESTED

Listen for test tone.

EMERGENCY LIGHT SWITCH ....................................................................... ARMED

PASSENGER OXYGEN SWITCH .................................................................... BLANK

RAM AIR TURBINE SWITCH .......................................................................... BLANK

IGNITION SWITCH ................................................................................................ SET

Set 1 for odd days, set 2 for even days, and BOTH for cold weather operations.



ENGINE START SELECTORS ............................................................................. OFF

FUEL JETTISON PANEL...................................................................................... OFF

Check switches blank and selector OFF

FUEL PANEL ......................................................................................................... SET

- FWD and AFT main fuel pumps OFF

- Center fuel pumps OFF

- Crossfeed switches OFF

FUEL QTY AND BALLANCE ..................................................................... CHECKED

Check the proper fuel quantity on board and balance in limit.

ENGINE AND WING ANTI-ICE ............................................................................. OFF

EXTERIOR LIGHTS ............................................................................. AS REQUIRED

Only position light should be ON. During darkness LOGO light should be switched also ON.

CARGO HEAT ...................................................................................................... OFF

WINDOW HEAT ...................................................................................................... ON

PASSENGER SIGNS ........................................................................... AS REQUIRED

CABIN PRESSURIZATION PANEL ..................................................................... SET

- Set landing altitude (round up the airport / runway elevation)

- Select AUTO 1 for odd days

- Select AUTO 2 for even days

- Set auto rate at the detent position

EQUIPMENT COOLING SWITCH ..................................................................... AUTO

TEMPERATURE CONTR. KNOBS ...................................................... AS REQUIRED

TRIM AIR SWITCH ................................................................................................. ON

This switch is always left ON

RECIRC FAN SWITCHES....................................................................................... ON

These switches should always left ON, otherwise no airflow provided in the cabin and flight deck.

PACK CONTR. SELECTOR ................................................................ AS REQUIRED

If the APU in use, turn the pack switches to AUTO.

If external air is in use, turn pack switches OFF

ISOLATION SWITCHES ......................................................................................... ON

L & R switches ON, center switch guarded ON.

ENGINE BLEED SWITCH....................................................................................... ON

These switches should always left ON.



APU BLEED SWITCH ............................................................................................. ON

This switch is always left ON

FMC ........................................................................................................... INITALIZED

Check database AIRAC cycle and program the FMC with route and performance information.

AFDS PANEL ......................................................................................................... SET

- NAV 1 Radio set MAN frequency, otherwise set AUTO

- FD switches ON

- A/T switch OFF

- IAS / MACH set calculated V2 from FMC

- HDG set runway heading or other required heading

- ALT set initial cleared altitude

- A/P Disengage bar UP


FLIGHT INSTRUMENTS ........................................................................................ SET

Note: These checks should be done after the IRU’s have aligned!

- Instrument source selector – NORM

- Airspeed – check and set speed bugs for take-off (automatic bug setting by mouse click)

- RMI – set pointer controls and verify headings

- EADI – check for anomalies

- EHSI – check for anomalies and set range and display mode as required (10nm range normal)

- Altimeter – set altimeter at local QNH

- VSI – indicates zero

- Clock – set

- Standby instruments – set.

WARNING ANNUNCIATOR ....................................................................... CHECKED

All should be off and blank.

STANDBY ENGINE GAUGES ........................................................................... AUTO

AUTO BRAKE SELECTOR .................................................................................. OFF

EICAS ......................................................................................................... CHECKED

- Check CAS messages for abnormal indications

- Check engine gauges for normal indications

- Check STATUS page and set lower EICAS screen to the ENGINE page

TRP ................................................................................... T/O AND # OF DERATING

Deration pre-select for T/O (turn knob to increase temperature) or CLB 1 or 2 if desired.

FLAPS / INDICATOR ........................................................................... IN / SHOW „0“

Check warning light are off and the indicator agrees with the flap handle position.



ALTERNATE FLAP SELECTOR ....................................................................... NORM

Check selector set to NORM and ALTN not displayed in the LE or TE switches.

LANDING GEAR ............................................................................. DOWN / 3 GREEN

Check no amber lights illuminated.

ALTERNATE GEAR SWITCH ......................................................... GUARDED / OFF

GND PROX OVERRIDE SWITCH ......................................................................... OFF

STABILIZER TRIM ................................................................................................. SET

Set green band (approx. 4 unites is normal).

SPEED BRAKES .............................................................................................. DOWN

THROTTLES .................................................................................................. CLOSED

FUEL CONTROL SWITCHES ....................................................................... CUT OFF

ENGINE AND APU FIRE PANEL ................................................................. NORMAL

Check that no handle is pulled and turned.

CARGO FIRE PANEL ................................................................................... NORMAL

ATC TRANSPONDER ........................................................................................... SET

Set the power switch to SBY or AUTO and the TCAS control knob to XPDR ONLY (only during low

visibility condition turn to TA for traffic information on ground).

COMM & AUDIO PANEL ....................................................................................... SET

Set radios as required.

ILS FREQUENCY ................................................................................ AS REQUIRED

Set to PARK or to required ILS frequency for possible re-landing.

AILERON / RUDDER TRIM ............................................................................ SET „0”

Check all trims at zero / neutral

1.3 CREW AT STATION

The “Crew at Station Check List” shall be carried out if both pilots on flight deck, the load sheet and

the ATC clearance received (if online).


Park brake set – important for FSFK / XCARS recording.



FUEL QTY CHECK ................................................................................ PERFORMED

Check the fuel quantity on board and compare the value with the OFP.

PASSENGER SIGNS .............................................................................................. ON

ALTIMETERS ...................................................................... SET / CROSS CHECKED

IRS ................................................................................................................ALIGNED

Check all 3 IRS mode selectors on NAV and no FAULT or ALIGN lights illuminated.

FMC ............................................................................................................ PROGRAM

Program all relevant data into FMC and check this by the OFP.

ATC CLEARANCE ..................................................................................... RECEIVED

If online check initial assigned altitude and set ALT selector window.

TRANSPONDER CODE......................................................................................... SET

Set and check correct ATC transponder code. Power switch to SBY or AUTO, TCAS selector knob to

XPDR.

AFDS / FLIGHT INSTRUMENTS ........................................................................... SET

Note: These checks should be done after the IRU’s have aligned!


- FD switches ON

- A/T switch OFF

- IAS / MACH set calculated V2 from FMC

- HDG set runway heading or other required heading

- ALT set initial cleared altitude

- A/P Disengage bar UP


- Instrument source selector – NORM

- Airspeed – check and set speed bugs for take-off (automatic bug setting by mouse click)

- RMI – set pointer controls and verify headings

- EADI – check for anomalies

- EHSI – check for anomalies and set range and display mode as required (10nm range normal)

- Altimeter – set altimeter at local QNH

- VSI – indicates zero

- Clock – set

- Standby instruments – set.

AILERON / RUDDER TRIM ............................................................................ SET „0“

Check all trims at zero / neutral



STABILIZER TRIM ......................................................................... ______UNITS SET

Set required trim according calculated value from FMC. Check trim is in green T/O range. Call out the

trim units.

Note: If all HYDR Pumps OFF switch both ELEC Pumps ON for hydraulic pressure to operate stabilizer

trim!

TAKE-OFF BRIEFING ........................................................................... PERFORMED

- Status of aircraft (take-off weight, limitations)

- Take-off configuration (flaps, T/O power settings)

- Acceleration altitude and climb procedure

- Reconfirmation of Runway, condition and length TORA

- Departure route and climb procedure / limitations

- Handling in case of emergency and re-landing

- Estimated ATC frequencies.

1.4 BEFORE ENGINE START

The “Before Engine Start Check List” shall be carried out before start-up and push-back clearance

received, “all engine clear” from ground staff received, all doors closed, cabin reported all PAX

seated, and ground equipment removed (excluding necessary ground equipment for the start-up

procedure).

The engines shall normally be started in the sequence #2 and then #1.

When N2 reach a minimum of 18% set fuel control switch to RUN and monitor EGT.

Abort the start sequence if temperature exceeds 750°C during start-up (expect higher EGT during

tailwind start-up).

PAX & SERVICE DOORS .............................................................................. CLOSED

FUEL PANEL ......................................................................................................... SET

Switch all fuel pumps ON in tank with fuel. Check FUEL CONFIG fail light and message not appears.

HYDRAULIC PANEL ................................................................................ ON & AUTO

- Primary electric pumps ON

- All demand pumps to AUTO

RED ANTI-COLL. LIGHT ........................................................................................ ON

PACK SWITCHES ................................................................................................ OFF

Check minimum pressure 25 PSI or above for engine start.

XACARS / FSFK ................................................................... RECORDING STARTED

Start “recording” of flight via XACARS / FSFK



1.5 AFTER ENGINE START Start with the “After Engine Start Check List” as soon as possible after stabilized engines.

PACK SWITCHES ............................................................................................. AUTO

ISOLATION SWITCHES ....................................................................................... OFF

CARGO HEAT SWITCHES ..................................................................................... ON

ENGINE ANTI-ICE ............................................................................... AS REQUIRED

If OAT below 10°C and visible moister observed select L & R ENG ANTI-ICE ON.

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

ENGINE START SELECTORS .......................................................................... CONT

AUTO BRAKE SELECTOR .................................................................................. RTO

EICAS ...................................................................................... RECALL & CHECKED

Check CAS messages and engine indications. There should no messages displayed in normal

operation.

ALERT LIGHTS .................................................................................................... OUT

All Caution & Warning lights should be extinguished.

GROUND EQUIPMENT ............................................ DISCONNECTED / ALL CLEAR

Check all ground connection removed and equipment clear from aircraft.

1.6 TAXI CHECK Start with the “Taxi Check List” before or short after “taxi clearance” by ATC received, and “all clear”

signal given by the ground staff. Switch on the taxi light and release parking brake. Set engine thrust

to the minimum required for taxi, to prevent noise and jet blast damage.

During night or low visibility it is recommended to switch on the wing inspection and the runway

turnoff lights.

FLIGHT CONTROLS .................................................................... CHECKED & FREE

Check elevator and aileron for full and free movement.

Check Rudder for full and free movement.

Check movements on EICAS status display.

FLAPS ............................................................................. AS REQUIRED / CHECKED

Set Flaps as required and call out the setting.



ATC CLEARANCE ..................................................................................... REVIEWED

Verify ATC clearance – otherwise ask ATC.

TARNSPONDER .............................................................................................. TA / RA

Push the TCAS toggle switch on the EHSI control panel to display the TFC on EHSI.

FLIGHT DIRECTORS .................................................................................. BOTH ON

AUTOTHROTTLE ........................................................................................... ARMED

LNAV / VNAV .................................................................................................. ARMED

Check status on the EADI. If A/P engaged while in the T/O mode and no other mode (LNAV & VNAV)

has been selected, the AFDS automatically enters the HDG HOLD and VERT SPEED modes!

1.7 BEFORE TAKE-OFF The “Before Take-Off Check List” shall be carried out short before holding point reached and cabin

finished with the “Security Announcements” and cockpit ready for departure.

TAKE-OFF CONFIGURATION ................................................................... CHECKED

Check flaps, trim, take-off speed and aircraft systems in proper configuration and ready for

departure.

CABIN SECURED ...................................................................................... RECEIVED

Confirm “cabin secured” call received.

CABIN CALL ..................................................................................................... GIVEN

Call from Cockpit to Cabin “cabin crew prepare for departure”

If runway line-up or take-off clearance received switch the white anti-collision light to ON, and switch

transponder to mode-s (x-ponder to ON).

Check runway and approach sector clear of traffic if possible.

Identify the runway designator.

If take-off clearance received, switch landing lights to ON.

Advance throttles to 70% N1 then press the N1 mode button, release brakes and start the flight time

counting on the clock.

Check N1 annunciation on the EADI.

80kts call out – verify THR HOLD mode.

V1, Vr, V2, positive – gear-up.

Above 400ft AGL engage A/P and select LNAV or HDG SEL as required if not preselected.

Above 1000ft engage VNAV (if not preselected). If VNAV not selected set FL CH and set speed 250 or

as required.



1.8 CLIMB The “Climb Check List” shall be carried out if workload allowed or latest passing 10.000ft.

From take-off up to 10.000ft perform “sterile flight deck” philosophy.

- No paperwork should be perform

- During night time dim panel lights to observe surrounding traffic

- No unessential conversation should be done

ALTIMETERS ...................................................................... STD / CROSS-CHECKED

When climbing through the transition altitude set the altimeter to 1013,25 hPa / 29,92 inHg.

MCP ............................................................................................................ CHECKED

Check MCP for proper setting.

FLAPS .................................................................................................. IN / CHECKED

Check flaps and indicator position in zero, and no fault lights or messages appear.

LDG GEAR ...................................................................................... UP / LIGHTS OUT

Check gear UP and lever in OFF position. All 3 lights out.

CLIMB POWER ...................................................................................................... SET

Check desired climb power (CLB, CLB1, CLB2) and both engine reach the setting.

1.9 DESCENT Perform “Descent Check List” prior TOD reached or ATC request descent. The ATIS information

should be received and the approach briefing should be done at this time.

PRESSURIZATION ..................................................................................... CHECKED

Check correct landing altitude of destination airport is set.

SEAT BELT ............................................................................................................. ON

Check or set switch to ON.

APPROACH BRIEFING ......................................................................... PERFORMED

Check estimated landing weight and required landing speed.

Check actual fuel and calculate holding time and range of alternate airport

Check area and approach limitations / weather conditions.

Set NAV aids to expected STAR and runway



1.10 APPROACH Perform the “Approach Check List” prior reach the initial approach point or 20NM ARC by VFR flight,

but latest after “approach clearance” received by ATC. Not exceed 250kts below FL100.

Perform “sterile flight deck” philosophy from 10.000ft until landing.

- No paperwork should be perform

- During night time dim panel lights to observe surrounding traffic

- No unessential conversation should be done

CABIN CALL ..................................................................................................... GIVEN

Approximately 10 minutes before landing call: “cabin crew prepare for landing”.

MET / ATIS DATAS ................................................................................... RECEIVED

Check latest ATIS information.

ALTIMETERS ...................................................................... SET / CROSS CHECKED

If approach clearance received rotate altimeter knob to the destination QNH, but latest at transition

altitude. (In the airspace of the USA set local QNH when passing 18.000ft)

LANDING DATA IN FMC .................................................................. SET / CHECKED

Check STAR, RWY, landing speed in FMC.

AIRSPEED BUGS ............................................................................. SET / CHECKED

Set speed bugs according FMC landing speed data (automatic bug setting by mouse click)

DH / DA ............................................................................................. SET / CHECKED

Set and check the decision high / decision altitude for assigned approach and landing.

APP / VOR ........................................................................................... AS REQUIRED

Set APP/NAV as required and crosschecked. ILS by tone identified.

AUTOBRAKES .................................................................................... AS REQUIRED

Check auto brake selector in desired position (1, 2, 3, 4, or MAX AUTO).



1.11 FINAL Perform “Final” Checklist between 2500ft and 1000ft AGL

GEAR ................................................................................................................ DOWN

Check gear lever down and no amber transient light illuminated

Check all 3 green LD GEAR lights on.

FLAPS .................................................................................................. AS REQUIRED

Check Flaps in the required landing position. Call out position.

SPEED BRAKES ............................................................................................ ARMED

1.12 AFTER LANDING

Perform “After Landing” Checklist during taxiing to the ramp, but not before active runway vacated.

Use APU and external lights as required.

SPEED BRAKES ...................................................................................................... IN

Check lever to IN position

FLAPS ......................................................................................................... IN OR SET

Set flaps to zero position. Verify flap position agree with indicator and no fault light appear.

AUTOBRAKES ..................................................................................................... OFF

Check amber AUTO BRAKES light extinguished after turn the selector from DISARM to OFF.

FLIGHT DIRECTOR SWITCHES ............................................................... BOTH OFF

ANTI COLL. LIGHT WHITE .................................................................................. OFF

TRANSPONDER ................................................................................................. STBY

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

CARGO HEAT SWITCHES ................................................................................... OFF



1.13 TRANSIT PARKING Perform “Transit Parking” Checklist if the same crew scheduled for the next flight, and stay on this

aircraft.


Check no movement of aircraft and set park brake. Important for XCARS / FSFK data transfer.

APU OR EXT POWER ........................................................................ ESTABLISHED

Check before shutdown the engine electrical power established by APU or GND power.

ANTI-ICE ............................................................................................................... OFF

ISOLATION SWITCHES ................................................................................. L&R ON

FUEL CONTROL SWITCHES ....................................................................... CUT-OFF

ENGINE START SELECTORS ............................................................................. OFF

RED ANTI COLL. LIGHT ..................................................................................... OFF

SEAT BELT ........................................................................................................... OFF

CABIN CALL DOORS OPEN ........................................................................... GIVEN

FUEL PUMPS ....................................................................................................... OFF

HYRAULIC PANEL ................................................................................................ SET

- Primary Engine Pumps are left ON

- Primary Electrical Pumps switches OFF

- All 3 Demand Pumps switches OFF

XACARS / FSFK ................................................................................................. SENT

Check your data and apply additional information into the remark field – if required. Sent your report



1.14 FINAL PARKING Perform “Final Parking” after last flight of the day, and no hand over to maintenance staff scheduled.

IRS MODE SELECTOR ........................................................................................ OFF

Align lights come on than goes off

EMERGENCY LIGHT SWITCH ............................................................................. OFF

Check UNARMED light illuminate

WINDOW HEAT SWITCHES ................................................................................ OFF

PACK SWITCHES ................................................................................................ OFF

APU OR EXTERNAL POWER ................................................................... DESELECT

STBY POWER SELECTOR .................................................................................. OFF

BATTERY SWITCH .............................................................................................. OFF

XACARS/ FSFK .................................................................................................. SENT

Check your data and apply additional information into the remark field – if required. Sent your report



2.1 WIND LIMITATION

All limits valid for take-off and landing.

Max Tailwind for T/O & Landing………………….15kts

Max Crosswind on Dry or Wet Runway……….33kts

Automatic Landing - Tailwind……………………...10kts

Automatic Landing - Crosswind……………….....25kts

Automatic Landing - Headwind……………….....25kts

Example:

Wind inclination = 30°

Wind velocity = 32kts

Result:

Headwind comp. = 28kts

Crosswind comp. = 16kts



2.2 MAX AIRSPEED LIMITS & FLAP EXTENSION LIMITS

This table shows the maximum airspeed limits and flap extension limits.

VMO / MMO…………………………...………….360kt / 0.86M

Normal Gear Extension / Retraction…….270kt / 0.82M

Maximum Flap Extension Altitude…………..…….20.000ft

Flaps 1……………………………………………………….…...250kts

Flaps 5………………….……………..………………………….230kts

Flaps 15…………………….…………………………………...210kts

Flaps 20……………….………………………………………...210kts

Flaps 25……………….………………………………………...180kts

Flaps 30………………………………….……………………...170kts

2.3 CRUISE LEVEL CAPABILITY WITH ALL ENGINES

This table shows the optimum and maximum cruising levels in reference to the cross weight.

Mach 0.82 Cruise Thrust Limit Pressure Alt (ft)

Weight in Ton

Optimum Altitude

ISA+10°C & below

ISA+15°C ISA+20°C

185 29400 34100 33200 32300

180 29900 34700 33900 32900

175 30500 35300 34600 33600

170 31200 35900 35200 34300

165 31800 36500 35800 35000

160 32500 37100 36400 35600

155 33200 37800 37050 36200

150 33900 38400 37700 36800

145 34600 39100 38300 37500

140 35300 39800 39000 38200

135 36100 40600 39700 38900

130 36800 41300 40500 39600

125 37600 42100 41300 40400

120 38400 42900 42100 41200

115 39300 43100 42900 42000

110 40300 43100 43100 42900

A/C Packs ON and Anti-Ice OFF



This graph shows the values from above. Right data show the altitude in feet, and the lower

data show the cross weight in tons.



4.0 LIST OF ABBREVIATIONS:

A/C Aircraft

AFDS Autopilot Flight Director

System

AFT Aft (rear)

AGL Above Ground Level

AIRAC Aeronautical

Information Regulation

And Control

ALT Altitude

ALTM Altimeter

AOM Aircraft Operator

Manual

A/P Auto Pilot

APU Auxiliary Power Unit

ARC Arc (curve)

A/T Auto Throttle

ATC Air Traffic Control

ATIS Air Traffic Information

Service

CAT Category

CAS Crew Alerting System

CG Center of Gravity

CI Cost Index

CLB Climb

DA Decision Altitude

DH Decision High

EADI Electronic Attitude

Direction Indicator

EGT Exhaust Gas

Temperature

EHSI Electronic Horizontal

Situation Indicator

EICAS Engine Indications Crew

Alerting System

ELT Emergency Locator

Transmitter

ENG Engine

EVAC Evacuation

EXT External

FD Flight Director

FL Flight Level

FL CH Flight Level Change

FMA Flight Mode

Annunciator

FMS Flight Management

System

FP Flight Plan

FS Flight Simulator

FSFK Flight Simulator Flight

Keeper

ft Feet

FWD Forward

GND Ground

hPa Hectopascal

IAS Indicated Air Speed

ILS Instrument Landing

System

IRS Inertial Reference

System

ISA International Standard

Atmosphere

kts Knots

L Left

LD Landing

LDG Landing / Landing Gear

LE Leading Edge

MAN Manual



MMO Maximum Operating

Limit Mach

NAV Navigation

NM Nautical Mile

OAT Outside Air

Temperature

OFP Operation Flight Plan

PAX Passenger

PWR Power

QNH Altitude based on local

pressure

R Right

RMI Radio Magnetic

Indicator

RTO Rejected Take-Off

RWY Runway

SED Standby Engine Display

SID Standard Departure

Route

STAR Standard Arrival Route

TA/RA Traffic Advisory /

Resolution Advisory

TCAS Traffic Alert and

Collision Avoidance

System

TE Trailing Edge

TFC Traffic

T/O Take-Off

TOGA Take-Off Go-Around

TORA Take-Off Run Available

TOW Take-Off Weight

TRP Thrust Rating Panel

WX Weather

VAT Virtual Air Traffic

VFR Visual Flight Rules

VSI Vertical Situation

Indicator

VMO Maximum Operating

Speed

XACARS Virtual Aircraft

Communications

Addressing and

Reporting System

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