EP's - FCOM 1 Exact - Title Only Flashcards
These are the ones listed in FCOM. - updated 15 Jul 21
AUTOMATIC UNLOCK
- FLT DK DOOR lock selector ……. Rotate to DENY and hold for 1 second.
- end of procedure -
Aborted Engine Start
- Engine start lever (affected engine) . . . . . . . . . . . . . . . CUTOFF
SMOKE, FIRE OR FUMES.
- Diversion may be needed.
- Don oxygen masks and set regulators to 100%
- Don smoke googles, as needed.
Airspeed Unreliable
- Autopilot (if engaged) . . . . . . . . . . . . . . . . . . . . . . . . Disengage
- Autothrottle (if engaged) . . . . . . . . . . . . . . . . . . . . . . Disengage
- F/D switches (both) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
- Set the following gear up pitch attitude and thrust:
Flaps extended . . . . . . . . . . . . . . . . . . . . . . 10° and 80% N1
Flaps up . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4° and 75% N1
Engine Limit or Surge or Stall
1 Autothrottle (if engaged) . . . . . . . . . . . . . . . . . . . . . . Disengage
2 Thrust lever (affected engine) …………. Confirm………..Retard until engine indications stay within limits or the thrust lever is closed
Loss Of Thrust On Both Engines
- ENGINE START switches (both) . . . . . . . . . . . . . . . . . . . . FLT
- Engine start levers (both). . . . . . . . . . . . . . . . . . . . . . . CUTOFF
- When EGT decreases:
- Engine start levers (both). . . . . . . . . . . . . . . . . .IDLE detent
4 If EGT reaches a redline or there is no increase in EGT within 30 seconds:
- Engine start lever (affected engine) . . Confirm . . . . .CUTOFF, then IDLE detent
- If EGT again reaches a redline or there is no increase in EGT within 30 seconds, repeat as needed
[NOTE: if the aircraft reverts to standby power, there are no MMO/VMO protections]
Runaway Stabilizer
- Control column . . . . . . . . . . . . . . . . . . . . . . . . . . . . Hold firmly
- Autopilot (if engaged) . . . . . . . . . . . . . . . . . . . . . . . . Disengage
- Do not re-engage the autopilot.
- Control airplane pitch attitude manually with control column and main electric trim as needed. - Autothrottle (if engaged) . . . . . . . . . . . . . . . . . . . . . . Disengage
- Do not re-engage the autothrottle. - If the runaway stops after the autopilot is disengaged: [end of checklist]
5 If the runaway continues after the autopilot is disengaged:
- STAB TRIM CUTOUTswitches (both). . . . . . . . . . . CUTOUT
- If the runaway continues:
- Stabilizer trim wheel . . . . . . . . . . . . . . . . . .Grasp and hold
6. Stabilizer………………………… Trim Manually
7. Anticipate trim requirements.
APU FIRE
- APU fire switch
. . . . . . . Confirm . . . .Pull, rotate to the stop, and hold for 1 second
- APU switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
WARNING HORN (INTERMITTENT) or WARNING LIGHT - CABIN ALTITUDE OR TAKEOFF CONFIGURATION
- If the intermittent warning horn sounds or a CABIN ALTITUDE light (if operative) illuminates in flight at an aircraft flight altitude above 10,000 feet MSL:
- Don the oxygen masks and set the regulators to 100%.
- Establish crew communications
- Go to the CABIN ALTITUDE WARNING or Rapid Depressurization checklist on page 2.1 (END OF PROCEDURE)
2 If the intermittent warning horn sounds or a TAKEOFF CONFIG light (if operative) illuminates on the ground when advancing the thrust levers to takeoff thrust:
- Ensure correct aircraft takeoff configuration
ENGINE OVERHEAT
- Autothrottle (if engaged) . . . . . . . . . . . . . . . . . . . . . . Disengage
- Thrust lever (affected engine) . . . . . . Confirm . . . . . . . . .Close
- If the ENG OVERHEAT light stays illuminated:
Go to the ENGINE FIRE or Engine Severe Damage or Separation checklist on page 8.2
———- end of procedure ———–
- If the ENG OVERHEAT light extinguishes:
Run the engine at reduced thrust to keep the light extinguished.
ENGINE FIRE OR ENGINE SEVERE DAMAGE OR SEPARATION
- Autothrottle (if engaged) . . . . . . . . . . . . . . . . . . . . . . Disengage
- Thrust lever (affected engine) . . . . ….. Confirm . . . . . . . . Close
- Engine start lever (affected engine) . ….Confirm . . .. . .CUTOFF
- Engine fire switch (affected engine) . . . Confirm . . . . . . . . Pull
[To manually unlock the engine fire switch, press the override and pull]
- If the engine fire switch or ENG OVERHEAT light is illuminated:
Engine fire switch . . . . Rotate to the stop and hold for 1 second
LANDING CONFIGURATION
- Ensure correct aircraft landing configuration.
TAKEOFF CONFIGURATION
- Ensure correct aircraft takeoff configuration.
Emergency Descent
- Advise Flight Attendants and ATC of the emergency descent.
- Passenger signs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
- Without delay, descend to the lowest safe altitude or 10,000 feet, whichever is higher.
- ENGINE START switches (both) . . . . . . . . . . . . . . . . . . CONT
- Thrust levers (both) . . ..Reduce thrust to minimum or as needed for anti-ice
- Speedbrake. . . . . . . . . . . . . . . . . . . . . . . . . . FLIGHT DETENT
- Set target speed to Mmo/Vmo
[If structural integrity is in doubt, limit speed as much as possible and avoid high maneuvering loads.]
[CAUTION! - (-700): When GW is greater than 143,000#, speed brake will autostow to the 50% flight detent if airspeed exceeds 320 kts. Do not override autostow function unless airspeed is less than 320 kts.]
CABIN ALTITUDE WARNING OR RAPID DEPRESSURIZATION
- Don oxygen masks and set regulators to 100%.
- Establish crew communications.
- Pressurization mode selector - MAN
- Outflow Valve switch - hold in CLOSE until the outflow valve indication shows fully closed
- if cabin altitude is UNCONTROLLABLE -
- Passenger signs - ON
- PASS OXYGEN switch - ON
- Go to the Emergency Descent checklist on page 0.1
- if cabin altitude is CONTROLLABLE -
- Continue Manual operation to maintain correct cabin altitude
- When the cabin altitude is at or below 10,000 feet - Oxygen masks may be removed