Other Limitations [B767] Flashcards
Runway Slope
+/- 2%
Max Operating Altitude
43,100’ PA
Max T/O & LDG Altitude
8,400’ PA
Nav & dislay systems do not support operations at latitudes greater than __ degrees North or South
87
Standby Altimeters do not meet the accuracy requirements of
RVSM
Max allowable IN-FLIGHT difference between Captain & First Officer altitude displays for RVSM operation
200 feet
Max allowable ON-GROUND difference between Captain & First Officer altitude displays for RVSM operation
Field Elevation - max diff CP & FO Sea Level - 40' 5,000' - 45' 10,000' - 50' max diff (pilot & field) any alt. - 75'
Crew & Supernumerary Evacuation
1 operable inertia reel AND 1 escape harness for each occupant
Smoke Barrier door must be closed during:
Taxi, takeoff, flight, and landing
Engine ignitions system must be on for
Takeoff and landing
Minimum INFLIGHT Fuel Temp
3 deg. C (5 deg. F) > freezing point of fuel
Max Fuel Temp
49 deg. C (120 deg. F)
JET-B, JP-4, NATO F-40, T-2, RP-4, No. 4 jet fuel
PROHIBITED
The Center Fuel Tank may contain up to _____ lbs of Fuel with less than full main tanks provided the center tank Fuel weight plus actual zero fuel weight, and CG limits are observed.
22,050 LBS
GE Engine Starter Limits (Normal Duty Cycle)
Five(5) minutes
1) Five (5) minutesON, followed by ON, followed by
one and one half one and one half (1 (1 1/2) minutes
OFF.