Memory limitations

+/-2%

633,000 lbs

630,500 lbs

461,300 lbs

AFM: For non-precision approaches, the autopilot must be disengaged no lower than theapplicable minimums minus 50 feet.

AFM: Maximum lateral fuel imbalance between tank 1 and 3 is 2500 lbs.

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

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.

FUEL SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

• 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.

• 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

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

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

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,