Limitations Flashcards
Maximum operating altitude_____
FL410
Maximum takeoff and landing tailwind_____
15 kts
Maximum takeoff and landing altitude_____
8,400 ft
Minimum takeoff and landing temperature_____
-54°c
Maximum operating speed limit_____
Vmo/Mmo, Gear and Flap placards
Severe turbulence penetration speed_____
280/.76
With either one or both engine BLEED air switches ON, do not operate PACKS in HIGH for_____
takeoff, approach, or landing
Engine anti-ice must be ON during all ground/flight ops when icing conditions exist or is expected except______
in climb or cruise below -40°c SAT
Engine anti-ice must be ON prior to and during descent_____
in all icing conditions no matter the OAT
Autopilot must not be engaged on takeoff below_____
1,000 ft AGL
Autopilot must be disengaged during a single channel approach by_____
50 ft AGL
Autopilot must be disengaged during manually flown HGS AIII approach by_____
500 ft AGL
Aileron trim with autopilot engaged is_____
Prohibited
Engines: Warm-up/Cool-down time_____
3 min/at or near idle for 3 min
Takeoff thrust time limit_____
5 minutes (*10 min if loss of thrust during takeoff)
EGT start maximum _____
725°c
ENGINE START switches must be in CONT for_____
- Takeoff
- Landing
- Anti-ice operation
- During hail, sleet or moderate-heavy rain
ENGINE START switches must be in FLT for_____
Severe Turbulence
Starter duty cycle (normal start)_____
2 minutes: first attempt
APU load: bleed and electric max altitude_____
10,000 ft
APU load: bleed only max altitude_____
17,000 ft
APU load: electric only max altitude_____
FL410
APU operating altitude max_____
FL410
APU BLEED air switch must be closed for 2 min. ____ and 1 min. _____ (shutdown time delay met automatically when APU switch selected off).
after start/prior to shutdown
APU bleed valve maybe open during engine start but avoid_____
Engine power above idle
APU Bleed valve must be closed when another source is pressurizing the _____ expect for engine start.
left bleed air duct
Flap extension max altitude_____
FL200
Holding in icing conditions with flaps extended is_____
Prohibited
Speed Brakes are NOT to be used below _____
1,000 ft AGL
Speed Brake lever NOT to be extend_____
beyond the FLIGHT DETENT
Load Alleviation System manual override is_____
not authorized
Fuel temperature minimum_____
-37°c
Fuel imbalance between main tanks must be_____
scheduled to be zero
Fuel imbalance must not exeed 1,000 lbs for_____
any phase of flight (taxi, takeoff, flight or landing)
Main Wing Tanks must be scheduled to be full if the Center Tank contains more than_____
1,000 lbs
Center Tank FUEL PUMP switches must not be ON while on the ground unless Center Tank fuel contains at least_____
1,000 lbs (except when defueling or transferring fuel)
Center Tank Fuel Pumps must not be On unless personnel are in the flight Deck monitoring the_____
LOW PRESSURE lights
When a LOW PRESSURE Center Tank Fuel Pump light illuminates_____
switch the corresponding Center Tank Fuel Pump OFF
If the Center Tank is empty postition both Center Tank FUEL PUMP switches_____
OFF
Electric Hydraulic Pump ground operation requires a minimum of_____
1675 lbs in respective fuel tank
