Term
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Definition
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Term
| Maximum takeoff and landing tailwind component |
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Definition
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Term
| Maximum operating altitude |
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Definition
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Term
| Maximum takeoff and landing altitude |
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Definition
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Term
| Maximum demonstrated crosswind |
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Definition
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Term
| Maximum allowable in-flight altitude display difference for RVSM |
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Definition
| 200' between Captain and First Officer displays |
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Term
| Maximum allowable ground altitude display difference for RVSM |
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Definition
Between Captain and FO:
SL to 5,000' - 50'
5001' to 10,000' - 60'
Between Captain or FO and Field Elevation:
SL to 10,000' - 75' |
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Term
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Definition
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Term
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Definition
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Term
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Definition
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Term
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Definition
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Term
| Maximum cabin differential pressure |
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Definition
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Term
| When is it recommended NOT to operate the air conditioning packs on HIGH? |
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Definition
| During takeoff, approach and landing with the engine bleed air switches ON |
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Term
| When must engine TAI be ON? |
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Definition
| When icing conditions exist or are anticipated, except during climb and cruise below -40ºC SAT |
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Term
| When is use of aileron trim prohibited? |
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Definition
| When the autopilot is engaged |
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Term
| What is the minimum altitude to engage the autopilot for takeoff? |
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Definition
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Term
| What is the minimum autopilot altitude during single channel operations on approach? |
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Definition
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Term
| What are the lat/long limitations for HDG SEL and ROLL CWS? |
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Definition
North of 89.30N
South of 89.30S |
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Term
| What are the maximum wind speeds for autoland operations? |
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Definition
| Headwind: 25 ktsCrosswind: 20 ktsTailwind: 15 kts |
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Term
| What are the maximum and minimum glideslope angles for autoland? |
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Definition
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Term
| What flap/engine and runway limitations are there for autoland capability? |
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Definition
Autoland capability may only be used with:
Flaps 30 or 40 and both engines operative
Runways at/below 8400' pressure altitude |
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Term
| What are the limitations for using the HUD system? |
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Definition
| Do not use the HUD system at latitudes greater than 85º latitude or when the Heading Reference Switch is in the TRUE position |
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Term
| When must engine ignition be ON? |
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Definition
takeoff
landing
operation in heavy rain
anti-ice operation |
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Term
| When is reverse thrust prohibited? |
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Definition
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Term
| What are the APU maximum operating altitudes? |
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Definition
Inflight - APU bleed + electrical load: 10,000'
Ground only - APU bleed + electrical load: 15,000' |
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Term
| What is the maximum altitude for APU bleed air? |
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Definition
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Term
| What is the maximum altitude for APU electrical load? |
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Definition
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Term
| When is it recommended to operate with the APU bleed valve closed? |
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Definition
Ground air connected and isolation valve open
Engine no. 1 bleed valve open
Isolation and engine no. 2 bleed valves open
May be open during start, but avoid engine power above idle |
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Term
| Maximum flap extension altitude |
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Definition
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Term
| When is the use of flaps prohibited? |
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Definition
| While holding in icing conditions |
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Term
| When are the speedbrake limitations? |
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Definition
Do not deploy less than 1000' RA
Do not extend beyond the flight detent in flight |
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Term
| What are the recommendations for using alternate flaps? |
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Definition
Allow 15 seconds between ALTERNATE FLAPS switch uses
Allow 5 minutes between each extend/retract cycle |
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Term
| What is the alignment limitation for the ADIRU? |
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Definition
| greater than 78.15º latitude |
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Term
| What is prohibited with the altimeters referenced to QFE? |
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Definition
VNAV or LNAV
Vertical Situation Display (VSD)
Look-Ahead terrain alerting and terrain display
Integrated Approach Navigation (IAN) - recommended |
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Term
| When should the Look-Ahead terrain alerting and terrain display functions not be used for takeoff, approach or landing? |
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Definition
| Within 15 nm of any airport not contained in the GPWS terrain database |
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Term
| When should the radar be OFF? |
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Definition
In a hangar
Within 50' or any personnel or fuel spill |
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Term
| Maximum tank fuel temperature |
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Definition
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Term
| Minimum inflight tank fuel temperature |
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Definition
| 3ºC above the freezing point of the fuel being used or -43ºC, whichever higher |
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Term
| Can the auxiliary fuel Maintenance (MAINT) switch be engaged in flight? |
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Definition
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Term
| What is the limitation for using center tank fuel? |
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Definition
| The center tank should be used until all auxiliary fuel has been transferred |
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Term
| What is the maximum fuel imbalance between tanks 1 and 2? |
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Definition
| 1000 lbs for taxi, takeoff, flight or landing |
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Term
| What are the fuel loading limitations for the center and auxiliary tanks? |
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Definition
Main tanks 1 and 2 must be full if center tank contains more than 1000 lbs
The center and main tanks must be scheduled to be full if the auxiliary fuel system is to be loaded or contains fuel |
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Term
| When must the anti-skid be operative for takeoff? |
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Definition
| When using assumed temperature reduced takeoff thrust |
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