EP's - FCOM 1 Exact Flashcards
These are the ones listed in FCOM. - updated 15 Jul 21
Engine Limit or Surge or Stall - 7.2
Condition:
One or more of these occur:
- Engine indications are abnormal
- Engine indications are rapidly approaching or exceeding limits
- Abnormal engine noises are heard, possibly with airframe vibration
- There is no response to thrust lever movement or the response is abnormal
- Flames in the engine inlet or exhaust are reported.
Objective:
To attempt to recover normal engine operation or shut
down the engine if recovery is not possible
1 Autothrottle (if engaged) . . . . . . . . . . . . . . . . . . . . . . Disengage
2 Thrust lever (affected engine) …………. Confirm………..Retard until engine indications stay within limits or the thrust lever is closed
Runaway Stabilizer
9.2
Condition:
Uncommanded stabilizer trim movement occurs continuously.
- 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.
ENGINE FIRE OR ENGINE SEVERE DAMAGE OR SEPARATION
8.2
Condition:
One or more of these occur:
- Engine fire warning
- Airframe vibrations with abnormal engine indications
- Engine 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
Loss Of Thrust On Both Engines
7.6
Condition:
Both of these occur:
- Both engines have a loss of thrust
- Both ENG FAIL alerts show.
Objective:
To restart at least one engine
- 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]
Aborted Engine Start
7.1
CONDITION: On the ground, an aborted engine start is needed.
OBJECTIVE: To shut down the engine and motor it.
- Engine start lever (affected engine) . . . . . . . . . . . . . . . CUTOFF
LANDING CONFIGURATION
15.1
Condition:
In flight, the steady warning horn sounds.
- Ensure correct aircraft landing configuration.
CABIN ALTITUDE WARNING OR RAPID DEPRESSURIZATION
2.1
Condition:
One or more of these occur:
- A cabin altitude exceedance
- In flight, the intermittent cabin altitude/configuration warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates
- Don oxygen masks and set regulators to 100%.
- Establish crew communications.
WARNING HORN (INTERMITTENT) or WARNING LIGHT - CABIN ALTITUDE OR TAKEOFF CONFIGURATION
15.2
Condition:
One of these occurs:
- In flight, at an airplane flight altitude above 10,000 feet MSL, the intermittent warning horn sounds or a CABIN ALTITUDE light (if installed and operative) illuminates
- On the ground, the intermittent warning horn sounds or a TAKEOFF CONFIG light (if installed and operative) illuminates when advancing the thrust levers to takeoff thrust.
- 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
8.5
Condition:
An overheat is detected in the engine
- 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.
Airspeed Unreliable
10.1
Condition:
Airspeed or Mach indications are suspected to be unreliable. (Items which might indicate unreliable airspeed are listed in the Additional Information
section.)
Objective:
To identify a reliable airspeed indication, if possible, or to continue the flight using the Flight With Unreliable Airspeed table in the Performance Inflight chapter.
- 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
TAKEOFF CONFIGURATION
15.1
Condition:
On the ground, the intermittent cabin altitude/configuration warning horn sounds or a TAKEOFF CONFIG light (if installed and operative)
illuminates when advancing the thrust levers to takeoff thrust
- Ensure correct aircraft takeoff configuration.
Emergency Descent
0.1
Condition:
One or more of these occur:
- Cabin altitude cannot be controlled
- A rapid descent is needed
- 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.]
APU FIRE
8.1
Condition:
Fire is detected in the APU.
- APU fire switch
. . . . . . . Confirm . . . .Pull, rotate to the stop, and hold for 1 second
- APU switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
SMOKE, FIRE OR FUMES.
- Diversion may be needed.
- Don oxygen masks and set regulators to 100%
- Don smoke googles, as needed.
AUTOMATIC UNLOCK
- FLT DK DOOR lock selector ……. Rotate to DENY and hold for 1 second.
- end of procedure -
