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Maximum Operating Pressure Altitude 757
42,000 ft
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Maximum Takeoff & Landing Pressure Altitude 757 Tail Numbers 451 through 470
14,000 ft
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Maximum Takeoff & Landing Pressure Altitude 767 Tail N335 and subsequent
9500 ft
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Maximum Takeoff & Landing Pressure Altitude
8400 ft
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Maximum Operating Pressure Altitude 767
43,100 Ft.
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Automatic Flight
On takeoff, do not engage Auto Pilot below 200 ft AGL
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Navigation
- VOR Approaches:
- One pilot must have Raw Data from the VOR associated with the approach displayed in the HSI VOR Mode no later then the Final Approach Fix
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Ignition
Continuous Ignition shall be ON for flight in Severe Turbulance
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Reverse Thrust
Reverse Thrust is restricted to Ground use ONLY.
Backing the aircraft with use of Reverse Thrust is NOT permitted.
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Minimum Oil Temp for Takeoff (PW)
+50 C
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Minimum Oil Temp for advancing Thrust Levers (RR)
0 degree C
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Minimum Turn radius (767)
A 180 Degree turn on a 150 ft wide Runway IS NOT authorized.
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Maximum Takeoff & Landing Tailwind Component
10 Kts
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Turbulent Airspeed
290 kts / 0.78 MACH whichever is LOWER
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Max Demonstrated Crosswind Takeoff & Land
30 kts
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Flap Extension Maximum Altitude
20,000 ft
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Maximum Temp for Jet-A
+49 C
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Minimum Fuel Tank Temperatures 757
Minus 45 C, or 3 degrees C above the Freezing Point of the fuel being used. (whichever is HIGHER)
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Minimum Fuel Tank Temperatures 767
3 degrees C above the Freezing Point of the fuel being used
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Maximum Fuel Imbalance between Left and Right Main Tanks for ALL operations 757
1800#
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Maximum Fuel Imbalance between Left and Right Main Tanks for ALL operations 767
- Main Tank fuel Load / Fuel Imbalance:
- <48,000# / 2500#
- 48,000 to 79,800 / Linear reduction to 1500#
- >79,800 # / 1500#
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(757)
The Center Tank Fuel Pumps must be OFF for Takeoff if Center tank fuel is less than _____# with the Airplane ready for initial taxi
5000#
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(757)
Both Center Tank fuel pumps must be selected OFF when Center Tank fuel quantity reaches approximately ______# during Climb, Cruise or Descent
1000#
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