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Maximum operating pressure altitude for B757.
42,000 Feet.
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Maximum operating pressure altitude for B767.
43,100 Feet.
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Maximum takeoff and landing pressure altitude?
8,400 Feet.
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Maximum takeoff and landing pressure altitude for 767 fleet tail N335 and up?
9,500 Feet.
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Maximum takeoff and landing pressure altitude for 757 fleet N451 to 470?
14,000 feet.
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Runway slope limits.
plus or minus 2 percent.
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Maximum takeoff or landing tailwind component?
10 knots.
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Turbulent air penetration speed?
290 knots or .78 Mach. Which ever is lower.
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Maximum demonstrated crosswind component?
30 knots.
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Minimum turning radius (767).
A 180 degree turn is not authorized on a 150 foot wide runway In the B767.
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Maximum taxi weight B757.
251,000 pounds.
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Maximum taxi weight B767.
409,000 pounds.
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Maximum taxi weight B767 with "light weight gear."
405,000 pounds.
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Maximum takeoff weight B757.
250,000 pounds
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Maximum takeoff weight B767.
408,000 pounds.
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Maximum takeoff weight B767 with "light weight gear."
404,000 pounds.
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Maximum landing weight B757.
210,000 pounds.
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Maximum landing weight B767.
326,000 pounds.
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Maximum zero fuel weight B757.
200,000 pounds.
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Maximum zero fuel weight B767.
309,000 pounds.
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On takeoff, do not engage the autopilot below What altitude?
2000' AGL
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Flap extension, maximum altitude?
20,000 feet.
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Maximum fuel temperature for Jet A fuel?
49 degrees C.
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Minimum tank fuel temperature for B757.
B757. Minus 45 degrees C or 3 degrees above the freeze point of the fuel being used. (Which ever is higher).
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Minimum tank fuel temperature for B767.
B767. 3 degrees C above the freeze point of the fuel being used.
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Maximum fuel imbalance between left and right main tanks in B757.
1,800 pounds.
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Maximum fuel imbalance between left and right main tanks in B767.
- 2,500 pounds for 48,000 pounds or less.
- Linear reduction to 1,500 pounds greater than 79,800 pounds.
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Minimum oil temperature for advancing thrust levers (RR).
0 degrees C.
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Minimum oil temperature for takeoff (PW).
50 degrees C
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Reverse thrust is for:
Ground use only. Backing up using reverse thrust is not permitted.
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Ignition shall be on for flight in:
Continuous ignition shall be on for flight in severe turbulence.
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(767) flame out protection.
Use of wing anti ice for flame out protection is only required during descent in icing conditions at or below 22,000 feet.
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(757 AD 2002-19-52). The center tank fuel pumps must be in OFF for takeoff if center tank fuel is less than ----- pounds.
5,000 pounds.
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(757 AD 2002-19-52) both center tank fuel switches must be selected OFF when center tank quantity reaches ---- pounds during climb, cruise, or descent
1,000 pounds.
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