Memory limitations

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  1. Runway slope:
    +/-2%
  2. AFM: Maximum Taxi Weight:Center Gear Extended:
    633,000 lbs
  3. AFM: Maximum Start of Takeoff Weight:Center Gear Extended:
    630,500 lbs
  4. AFM: Maximum Zero Fuel Weight:Center Gear Extended:
    461,300 lbs
  5. AUTOPILOT
    AFM: For non-precision approaches, the autopilot must be disengaged no lower than theapplicable minimums minus 50 feet.
  6. Fuel imbalance
    AFM: Maximum lateral fuel imbalance between tank 1 and 3 is 2500 lbs.
  7. ALL ENGINE FLAMEOUT
    ENG IGN OVRD SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . OVRD ON

    ADG . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DEPLOY

    NOTE: All engine flameout can be recognized by decrease in EGT, N2 and fuel flow. This will be followed closely by a decrease in N1.Airstart envelope is 250 KIAS to VMO, SL to FL300. Control aircraft at an IAS to obtain a minimumN2 of 15% for air start.ENG IGN OVRD SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . OVRD ON Push ENG IGN OVRD switch and observe OVRD ON light illuminates.ADG . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DEPLOY
  8. ENGINE ABNORMAL START (HOT, HUNG OR NO START)
    FUEL SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

    • NOTE: In the event an engine start needs to be discontinued after an engine has achieved45-52% (starter cutout) and the next Engine Start switch has been pulled, discontinue nextengine start by pushing the ENG START switch in and verifying Switch light extinguishes.
    • FUEL SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
    • Move associated FUEL switch to OFF.
  9. TAILPIPE FIRE
    FUEL SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
  10. TWO ENGINES INOPERATIVE
    • THROTTLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MCT
    • NOTE: Below 14,000′ MSL, 5 minutes of go-around power is permissible, if required.
    • FLAPS (UNLESS ON FINAL) . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
    • NOTE: Flaps should be retracted, even if below normal flap retract airspeed, to reducedrag and aid in acceleration.
    • SPEED (UNLESS ON FINAL) . . . . . . . . . . . . . . . . . . . . . DRIFTDOWN ORUP/RET VMIN+30
    • NOTE: Delay gear retraction until flaps are up.
    • GEAR (UNLESS COMMITTED) . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
    • SLATS (UNLESS ON FINAL). . . . . . . . . . . . . . . . . . . . . . . . . . . . RET
    • NOTE: Slats should be retracted at slat retract airspeed.
  11. ►CABIN ALTITUDE
    • OXYGEN MASKS . . . . . . . . . . .. . ON/100%
    • OUTFLOW VALVE . . . . . . . . . . . . . . . . . . . . . . . . . . VERIFY CLOSED

    NOTE: In addition to the “CABIN ALTITUDE” alert displayed, an aural warning will sound

    .OXYGEN MASKS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON/100%

    OUTFLOW VALVE . . . . . . . . . . . . . . . . . . . . . . . . . . VERIFY CLOSED

    • If outflow VALVE is not closed, push CABIN PRESS SYSTEM SELECT switch and observeMANUAL light illuminates.
    • Rotate CABIN PRESS manual rate selector to DESC.

    CREW/COURIER(S) COMMUNICATIONS . . . . . . . . . . . . . . . . . . . ESTABLISH
  12. ►CRG FIRE LWR ___
    FLASHING CARGO FIRE AGENT DISCH SWITCH . . . . . . . . . . . . . . . . . PUSH

    LAND AT NEAREST SUITABLE AIRPORTNOTE: In addition to the “CRG FIRE LWR ___” alert displayed, an aural warning will sound.FLASHING CARGO FIRE AGENT DISCH SWITCH . . . . . . . . . . . . . . . . . PUSHNOTE: CARGO FIRE AGENT DISCH switch will continue to flash until LOW light illuminates.If CARGO FIRE AGENT 1 DISCH LOW light was illuminated due to prior lowpressure condition, associated CARGO FIRE AGENT 2 DISCH switch will beginflashing.If CARGO FIRE AGENT 2 DISCH switch is pushed inadvertently, AGENT 2 cylinderwill discharge and associated CARGO FIRE AGENT 1 DISCH switch will continueflashing.ASSOCIATED CARGO FLOW SWITCH . . . . . . . . . . . . . . . . . . . . . . . OFFPush associated CARGO FLOW switch and observe OFF light illuminates.ASSOCIATED CARGO TEMP SELECTOR . . . . . . . . . . . . . . . . . . . . . OFF
  13. ►ENG 2 A-ICE DUCT
    ENGINE 2 THROTTLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE

    NOTE: In addition to the “ENG 2 A-ICE DUCT” alert displayed, an aural warning will sound.ENGINE 2 THROTTLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLEENGINE 2 FUEL SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
  14. ►ENGINE __ FIRE
    THROTTLE . . . . . . . . . . . . . . . . . . .. IDLE

    • CONSEQUENCES:LAND AT NEAREST SUITABLE AIRPORT2 TO ENG, NO ENGINE AGENTS FOR APUNOTE: In addition to “ENGINE ___ FIRE” alert, fire warning bell will sound and ENG FIRE handlewill be illuminated.
    • THROTTLE . . .. . . . . . . . . . . . . . . . . IDLE
    • FUEL SWITCH . . . . . . . . . . . . . . . . . OFF
    • ENG FIRE HANDLE/AGT LOW LIGHT . . . . . . . . . . . . . . . DOWN, DISCH/CHECK

    • Pull
    • associated ENG FIRE handle full down. Rotate handle left or right to dischargeextinguishing agent. Observe appropriate AGT LOW light illuminates.After 30 seconds,
Author
ID
233755
Card Set
Memory limitations
Description
limitations and memory items
Updated
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