Limitations Boeing 767SF AC

  1. ETOPS max diversion time / distance
    • 60 mins.       440 NM
    • 75 mins.       539 NM
    • 120 mins.     862 NM
    • 138 mins.     991 NM
    • 180 mins.     1293 NM
    • At 330 KIAS
  2. Weight Limitations
    • Taxi.                           187 333 KG
    • T/O (Brake release).    186 880 KG
    • Landing.                     147 871 KG
    • Zero Fuel.                   140 160 KG
  3. No Reduced Thrust Take Off
    • -Windshear / Temp inversion below 1500 ft AGL.
    • -Contaminated Runway (standing water, slush, snow, ice over 25%).
    • -Prohibited by Jepp manual.
    • -Prohibited by MEL manual.
  4. Autopilot
    • -Do not engage CWS or CMD below 200 ft AGL.
    • -Aileron trim use with AP engaged is prohibited.
    • -No FLCH on final approach below 1000 ft abv field elevation.
  5. Speed Brakes
    Do not use below 800 AGL.
  6. Flaps max altitude.
    20 000 ft
  7. FLAP 1
    250 KIAS
  8. FLAP 5
    230 KIAS
  9. FLAP 15
    210 KIAS
  10. FLAP 20
    210 KIAS
  11. FLAP 25
    180 KIAS
  12. FLAP 30
    170 KIAS
  13. FUEL TEMP MAX
    MAX 49°.  For JP-4/Jet B, 43°.
  14. FUEL TEMP MIN
    • At least 3° abv fuel freeze point:
    • -Jet A, -40°
    • -Jet A1, -47°
  15. FUEL LOAD (Fin 637-646)
    • Main tank (per):       19 548 KG
    • Center tank:            38 646 KG
  16. FUEL LOAD (FIN 660 to 663)
    • Main tank (per):       19 300 KG Fin 660, 661
    • Main tank (per):       19 355 KG Fin 662, 663
    • Center tank:             38 517 KG Fin 660 to 663
  17. MAX FUEL IMBALANCE
    1100 KG when main tank fuel is 22 000 KG with linear reduction to 600 KG  with main tank is 38 000 KG then 600 KG max.
  18. Single fuel crossed valve check (637-646)
    Check valve before each flight.  Maintenance max 1 hour before flight.
  19. ENGINE ANTI-ICE SYSTEM IN FLIGHT
    • Must be ON when icing conditions exist or anticipated except climb/cruise with temp below 40° C SAT.  Descent: all temp in icing conditions.
    • Icing conditions is in flight TAT 10° C or below in visible moisture rain, snow, sleet, ice crystals and clouds/fog(1 SM or less).
  20. ENGINE ANTI ICE SYSTEM ON GROUND
    In icing conditions (OAT 10° C and below) with snow, ice, standing water or slush.
  21. ICE CRYSTAL CONDITIONS
    • Engine Anti Ice must be ON when temp 10° or below in ice crystal conditions.
    • Ice crystal conditions is visible moisture AND:
    • -Amber or red wx radar returns below A/C.
    • -Appearance of liquid water in windshield at temps too cold for rain.
    • -Auto Throttle unable to maintain selected airspeed.
    • -TAT on EICAS stays near 0° C.
  22. GEAR SPEEDS
    • Retract/Extend/Use:           270 KIAS M.82
    • Extend, alt system:            250 KIAS M.75
  23. MIN OXYGEN PRESSURE
    • 1450 PSI per bottle is OK for:
    • -120 ETOPS with 6 occupants.
    • -180 ETOPS with 4 occupants.
  24. APU STARTING
    • -APU may not start above FL350.
    • -Max 3 start (attempt or start) per 60 mins period.
  25. CARGO DOORS
    • Operations: Max 40 knots wind.
    • Door open:  Max 65 knots gust.
    •                   Main Deck: Max 60 knots.
  26. ENGINE STARTER
    • MAX 15 mins continuous operation.
    • Cooling
    • -5-10 mins ops: 10 mins cooling.
    • -10-15 mins ops: 15 mins cooling.
    • Max N2 to re-engage: 20%.
  27. ENGINE IGNITION
    ON for T/O, land, turbulence and icing conditions (auto with engine anti ice).
  28. ENGINE OIL SYSTEM
    • MIN OIL P°:       10 PSI
    • MAX OIL T°:       175° C.  MAX 10 mins 160°-175° C.
    • Temp must be above bottom of temp scale before T/O power.
  29. MAXIMUM ALTITUDE
    43 100 ft
  30. TAKE OFF AND LANDING
    8 400 ft P alt
  31. MAX CROSSWIND DEMONSTRATED
    33 knots. Not considered limiting on dry runway.
  32. DIMENSIONS
    • Wingspan: 156' 1" / 47.57M  Winglet:  166' 11" / 50.88M
    • Length: 180' 3" / 54.94M
    • Height: 52' / 15.85M
Author
Fredquatorze
ID
358854
Card Set
Limitations Boeing 767SF AC
Description
Limitations for the Air Canada Boeing 767SF
Updated