Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
Max airport pressure altitude |
|
Definition
|
|
Term
|
Definition
|
|
Term
Max temp for takeoff/land |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
Max TW component takeoff or landing |
|
Definition
|
|
Term
max demonstrated crosswind with TRs |
|
Definition
|
|
Term
Min Oil Temp for starting: |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
[Engine Start] Max ITT (16 sec) |
|
Definition
|
|
Term
[Engine Start] Max ITT (50 sec) |
|
Definition
|
|
Term
[Engine Start] Max starter duty |
|
Definition
3 cycles, 5 minutes cooling before additional cycles |
|
|
Term
Max T/O N1, N2, ITT (5 minutes) |
|
Definition
|
|
Term
Max T/O N1, N2, ITT (with APR, 2 minutes) |
|
Definition
|
|
Term
Normal T/O N1, N2, ITT, (5 Minutes) |
|
Definition
|
|
Term
Normal T/O N1, N2, ITT (2 minute limit) |
|
Definition
|
|
Term
Max continuous N1, N2, ITT |
|
Definition
|
|
Term
Max permissible oil temp: |
|
Definition
|
|
Term
Max oil temp for single engine climb: |
|
Definition
|
|
Term
|
Definition
|
|
Term
max continuous oil pressure |
|
Definition
|
|
Term
min oil pressure at steady state idle |
|
Definition
|
|
Term
min oil pressure at takeoff power |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
[APU] Max altitude for engine start using APU |
|
Definition
|
|
Term
[APU] Max altitude for bleed air extraction |
|
Definition
|
|
Term
[APU] max altitude for start |
|
Definition
|
|
Term
[APU] max operating altitude |
|
Definition
|
|
Term
|
Definition
|
|
Term
APU Max starter Duty Cycle |
|
Definition
2 cycles, then 20 minutes cooling before additional cycles |
|
|
Term
[Max operating speeds] 0 - 10,000 ft |
|
Definition
|
|
Term
[Max operating speeds] 10,000 - 21,330 |
|
Definition
|
|
Term
[Max operating speeds] 21,330 - 25,640 |
|
Definition
|
|
Term
[Max operating speeds] 25,640 - 28,720 |
|
Definition
|
|
Term
[Max operating speeds] 28,720 and above |
|
Definition
|
|
Term
[Max operating speeds] RVSM |
|
Definition
|
|
Term
[Additional Speed Limits] Vfe flaps 20 |
|
Definition
|
|
Term
[Additional Speed Limits] Vfe flaps 30 |
|
Definition
|
|
Term
[Additional Speed Limits] Vfe Flaps 45 |
|
Definition
|
|
Term
[Additional Speed Limits] Vlo Ldg gear operating |
|
Definition
|
|
Term
[Additional Speed Limits] Vle Ldg gear extended |
|
Definition
|
|
Term
[Additional Speed Limits] Max tire speed |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
[Additional Speed Limits] Max speed for ADG ops |
|
Definition
250 KIAS after auto or manual deployment; 330 KIAS for 12 minutes reducing to 4 minutes at Vmo. flight test and training max is 215 KIAS |
|
|
Term
[Additional Speed Limits] turbulence penetration speed |
|
Definition
|
|
Term
[Electrical] Main Gen load limit below 35,000 ft |
|
Definition
|
|
Term
[Electrical] Main Gen load limit, above 35,000 ft |
|
Definition
|
|
Term
[Electrical] max continuous load on TR1 or 2 |
|
Definition
|
|
Term
[Electrical] max continuous load on ESS TRU1 and ESS TRU2 combined |
|
Definition
|
|
Term
[Fuel] max fuel imbalance between main tanks |
|
Definition
|
|
Term
[Fuel] Left/Right main tank capacity |
|
Definition
|
|
Term
[Fuel] fuselage tank capacity |
|
Definition
|
|
Term
|
Definition
|
|
Term
[Fuel] Takeoff with up to ___ in the aux tank is permitted provided there is at least ___ in each wing tank |
|
Definition
|
|
Term
[Fuel] Max flaps for fuel jettison |
|
Definition
|
|
Term
[Fuel] Min tail tank fuel for fuel jettison |
|
Definition
|
|
Term
|
Definition
|
|
Term
[Load Limits] Flaps down G limit |
|
Definition
|
|
Term
Max time for taxi light use if stationary |
|
Definition
|
|
Term
Maximum main tire pressure |
|
Definition
|
|
Term
max nosewheel tire pressure is ___ on the ground |
|
Definition
|
|
Term
[Flight Controls] Max altitude flaps extended |
|
Definition
|
|
Term
[Flight Controls] Min altitude spoilers extended |
|
Definition
|
|
Term
[Flight Controls] Spoilers must not be extended in flight below ____ (speed) |
|
Definition
|
|
Term
[automatic flight control system] use of autopilot prohibited below |
|
Definition
|
|
Term
[Pressurization] Max relief differential |
|
Definition
|
|
Term
[Pressurization] Taxi, takeoff and landing |
|
Definition
|
|
Term
Max rotation rate on takeoff |
|
Definition
|
|
Term
initial pitch target on rotation |
|
Definition
|
|
Term
cowl anti-ice must be on: |
|
Definition
OAT <10C, visible moisture or runways wet or contaminated |
|
|
Term
wing anti-ice must be on: |
|
Definition
Visible moisture present in any form below 400 ft AGL or the runway is wet or contaminated. Must be on for final taxi prior to takeoff if OAT <5C. If anti-ice fluid has been applied, wing anti-ice must be selected and confirmed ON just prior to thrust increase for takeoff |
|
|
Term
Cowl/Wing anti-ice must be on >= 22000 ft: |
|
Definition
ice indicated by ice detection system; or in icing conditions if ice detector failed |
|
|