Term
| CABIN ALTITUDE or Rapid Depressurization |
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Definition
OXYGEN MASKS...........ON
CREW COMMUNICATIONS...........ESTABLISH |
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Term
| Dual Engine Failure (767 GE) |
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Definition
ENGINE START SELECTORS (Both)..........FLT
THRUST LEVERS (Both)...........CLOSE
FUEL CONTROL SWITCHES (Both)..........CUT OFF, THEN RUN
If engine appears stalled or EGT approaches the Standby Engine Indicator placard limit: Repeat the above step on affected engine(s)
[Reduces EGT and improves airflow] |
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Term
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Definition
AUTOMATION..........DISENGAGE
[Disengage autopilot and autothrottles, and turn off flight directors.]
Establish normal pitch attitude and thrust setting for phase of flight. |
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Term
| Maximum takeoff and landing pressure altitude: |
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Definition
8,400 feet
9,500 feet B767 tail numbers 335 and subsequent
14,000 feet B757 Tail numbers: 451 thru 470 |
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Term
| Maximum operating pressure altitude: |
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Definition
(757) - 42,000 feet
(767) - 43,100 feet |
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Term
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Definition
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Term
| Maximum takeoff and landing tailwind component: |
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Definition
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Term
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Definition
| 290 knots/ .78M, whichever is lower |
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Term
| Maximum demonstrated crosswind Takeoff and Landing: |
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Definition
| 30 knots (not considered limiting on a dry runway with all engines operating) |
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Term
| Flap extension, maximum altitude: |
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Definition
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Term
| Maximum temperature for JET A: |
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Definition
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Term
| Minimum fuel tank temperatures: |
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Definition
(757) Minus 45 degrees C or 3 degrees above the freezing point of the fuel being used (whichever is higher)
(767) 3 degrees C above the freezing point of the fuel being used |
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Term
| (757) Maximum fuel imbalance between left and right main tanks for all operations: |
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Definition
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Term
| (767) Maximum fuel imbalance between left and right main tanks for all operations: |
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Definition
2500 lbs (main tank fuel load 48,000lbs or less)
linear reduction to 1500 lbs (48,000 to 79,800 lbs)
1500 lbs (greater than 79,800 lbs) |
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Term
| (757) The center tank fuel pumps must be OFF for takeoff if center tank fuel is less than ______ with the aircraft readied for initial taxi. |
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Definition
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Term
| (757) Both Center Tank Fuel Pump switches must be selected OFF when center tank fuel quantity reaches approximately ________ during climb, cruise, or descent. |
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Definition
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Term
| Limitation for use of AUTOMATIC FLIGHT |
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Definition
| On takeoff, do not engage autopilot below 200 ft AGL. |
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Term
| LIMITATION for non-precision approach |
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Definition
| VOR approaches: 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. |
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Term
| Maximum taxi weights (pounds): |
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Definition
(757) 251,000
(767) 409,000
404,000 aircraft with "light weight gear" |
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Term
| Maximum landing weight (pounds): |
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Definition
(757) 210,000
(767) 326,000 |
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Term
| Maximum zero fuel weight (pounds): |
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Definition
(757) 200,000
(767) 309,000 |
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Term
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Definition
| Continuos ignition shall be on for flight in severe turbulence. |
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Term
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Definition
| Reverse thrust is restricted to ground use only. Backing the airplane with use of reverse thrust is not permitted. |
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Term
| Minimum turning radius (767) |
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Definition
| A 180 degree turn on a 150 ft wide runway is not authorized. |
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