Memory limitations

Card Set Information

Author:
jrossemail
ID:
233755
Filename:
Memory limitations
Updated:
2013-09-10 01:35:50
Tags:
md11
Folders:

Description:
limitations and memory items
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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,

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