Limitations Flashcards
Runway slope
± 2%
Maximum Operating Altitude
43,100
Maximum Takeoff and Landing Altitude
8,400
# Maximum Takeoff and Landing Tailwind Component
10 knots
Flight Deck Security Door - operational check
once each flight day
Entry door evacuation slide systems must be armed and engaged
prior to taxi, takeoff, or landing
whenever passengers are carried
Severe turbulent air penetration speed
290 KIAS/.78 Mach (whichever is lower)
Do not operate HF radios
during refueling operations
APU starter duty cycle -
maximum of three consecutive starts or attempts within a sixty minute period
Do not use FLCH -
on final approach below 1000 feet AFE
Standby altimeters __do/do not__ meet altimeter accuracy requirements of RVSM
do not
Maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operation -
200 feet
The maximum allowable on-the-ground differences between Captain and First Officer altitude displays for RVSM operation are:
(Between CA and FO)
SEA LEVEL - 40 feet
5,000 feet - 45 feet
10,000 feet - 50 feet
The maximum allowable on-the-ground differences between Captain or First Officer altitude displays and Field Elevation for RVSM operation is:
75 feet
Avoid weather radar operation -
in a hangar, or within 50 feet (15.25 meters) of fueling operations or a fuel spill
Maximum Taxi Weight
413,000 lbs
Maximum Takeoff Weight
412,000 lbs
Maximum Landing Weight
320,000 lbs
Maximum Zero Fuel Weight
295,000 lbs
After takeoff, the autopilot must not be engaged below
200 feet AGL
Use of aileron trim with the autopilot engaged -
prohibited
Autoland wind limitations -
# Headwind 25 kts # Crosswind 25 kts # Tailwind 10 kts
Flight crew shall not blank _____ during takeoff
engine vibration
The minimum inflight fuel tank temperature is ____ above the freeze point of the fuel being used
3°C
