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Max. operating pressure altitude
757 42,000, 43100 767
Max. Takeoff and landing pressure altitude
- 9500' 767 Tail numbers: 335 and
- subsequent, 14,000' 757 Tail numbers 451-470
+ - 2%
takeoff oand landing tailwind component
Turbulent air speed
290/.78 whichever is lower
Max. demonstrated crosswind for T/O and landing
30kts (not considered limiting on a dry runway with all engines operation
Flap extension max. altitude
Maximum temp for Jet A
Minimum fuel tank temp
757= minus 45 degrees C or 3 degrees above the freezing poin of fuel being used ( whichever is higher)
767= 3 degrees C above te freezing point of the fuel being used.
767 Fuel imbalance
Fuel Imbalance 2500 lbs
linear reduction to 1500 lbs
Fuel imbalance 1500 lbs
- 48,000 or less (fuel imbalance 2500lbs)
- 48,000 to 79,800 (linear reduction to 1500lbs)
- greater than 79,800 (1500 lbs)
757 Max. fuel imbalance
The center tank fuel pumps must be off for takeoof if cneter tank fuel is less than (757)
Note: If takeoff is made with between 5000 and 1000 lbs in the center tank
position both center tank pumps on above 10,000 ft
Both center tank fuel pump switches must be selected off when center tank fule quanity reaches
1000 lbs during climb, cruise or descent.
Do not engagem autopilot below
One pilot must have raw data from the VOR associated with the approach displayed in the HSI VOR mode no later than the final approach fix.
Max. taxi weights
- 757: 251,000 lbs
- 767: 409,000lbs (405,000 - aircraft with "light weight gear")
Maximum Takeoff weights
- 757: 250,000 lbs
- 767: 408,000 (404,000 - aircraft with "light weight gear")
Maximum landing weight
- 757: 210,000lbs
- 767: 326,000 lbs
Mximum zero fuel weight
- 757: 200,000 lbs
- 767: 309,000 lbs
Ignition shall be on for takeoff and landing:
Continuous ignition shall be on for flight in severe turbulence
Reverse thrust is restricted to ground use only. Backing the airplane with use of reverse thrust is not permitted
Minimum Turning Radius
767: At 180 degree turn on a 150' wide runway is not authorized.
Use of wing anti-ice for flameout protection is only required
during descent in incing conditions at or below 22,000 ft.
Max zero Fuel wt
- 757- 200,000
- 767- 309,000
- winglet 312,300
767 with winglets
The LAS is installed to preserve the long-term life of the wing structure. Don no override the system in normal operations. Even in some:
non-normal situations (rapid depressurization), the system should not be overriddden.
767 with winglets
If aircraft gross weight is over:
340,000 lbs and speed brake lever is beyond 50%, do no exceed 320 kts.