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24 Cards in this Set
- Front
- Back
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1. Maximum operating pressure altitude:
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1. Maximum operating pressure altitude:
(757) 42,000 ft (767) 43,100 ft |
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2. Maximum takeoff and landing pressure altitude:
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2. Maximum takeoff and landing pressure altitude:
8400 ft 9500 ft B767 tail numbers: 335 and subsequent 14,000 ft B757 tail numbers: 451 through 470 |
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3. Runway Slope Limits:
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3. Runway Slope Limits:
+/-2% |
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4. Maximum takeoff and landing tailwind component:
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4. Maximum takeoff and landing tailwind component:
10 kts |
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5. Turbulent air speed:
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5. Turbulent air speed:
290 knots/.78M, whichever is lower |
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6. Maximum demonstrated crosswind Takeoff and Landing:
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6. Maximum demonstrated crosswind Takeoff and Landing:
30 kts (not considered limiting on a dry runway with all engines operating) |
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7. Flap extension, maximum altitude:
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7. Flap extension, maximum altitude:
20,000 ft |
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8. Maximum temperature for JET A:
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8. Maximum temperature for JET A:
49 degrees C |
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9. Minimum fuel tank temperatures:
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9. Minimum fuel tank temperatures:
(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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10. Maximum fuel imbalance between left and right main tanks for all operations:
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10. Maximum fuel imbalance between left and right main tanks for all operations:
(757) 1800 lbs |
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11. Maximum fuel imbalance between left and right main tanks for all operations:
(767) |
11. Maximum fuel imbalance between left and right main tanks for all operations:
(767) Fuel Imbalance Main Tank Fuel Load 2500 lbs 48,000 or less linear reduction to 1500 48,000 to 79,800 1500 lbs greater than 79,800 |
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12.
(757) (AD 2002-19-52) |
12. (757) (AD 2002-19-52) The center tank fuel pumps must be OFF for takeoff if center tank fuel
is less than 5000 lbs with the aircraft readied for initial taxi. |
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13. (757) (AD 2002-19-52)
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13. (757) (AD 2002-19-52) Both center tank fuel pumps must be selected OFF when center tank
fuel quantity reaches approximately 1,000 lbs during climb, cruise or descent |
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14. Automatic Flight:
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14. Automatic Flight:
On takeoff, do not engage autopilot below 200 ft AGL |
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15. Navigation:
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15. Navigation:
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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16. Maximum taxi weight (pounds):
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16. Maximum taxi weight (pounds):
(757) 251,000 (767) 409,000 |
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17. Maximum takeoff weight (pounds):
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17. Maximum takeoff weight (pounds):
(757) 250,000 (767) 408,000 |
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18. Maximum landing weight (pounds):
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18. Maximum landing weight (pounds):
(757) 210,000 (767) 326,000 |
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19. Maximum zero fuel weight (pounds):
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19. Maximum zero fuel weight (pounds):
(757) 200,000 (767) 309,000 (767) 312,300 winglets |
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20. Ignition:
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20. Ignition:
Continuous ignition shall be on for flight in severe turbulence |
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21. Reverse Thrust:
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21. 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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22. Minimum oil temperature for takeoff:
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22. Minimum oil temperature for takeoff:
(PW) 50°C |
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23. Minimum oil temperature for advancing thrust levers:
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23. Minimum oil temperature for advancing thrust levers:
(RR) 0°C |
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24. Minimum turning radius:
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24. Minimum turning radius:
(767) A 180° TURN ON A 150 FT WIDE RUNWAY IS NOT AUTHORIZED |
