EP's - FCOM 1 Exact Flashcards Preview

1. EP's & LIMITS > EP's - FCOM 1 Exact > Flashcards

Flashcards in EP's - FCOM 1 Exact Deck (15)
Loading flashcards...
1

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

2

Runaway Stabilizer

9.2

Condition:

Uncommanded stabilizer trim movement occurs ​continuously.

1. ​ Control column​ ​ . . . . . . . . . . . . . . . . . . . . . . . . . . . .​ Hold firmly​

2.​ Autopilot (if engaged)​ . . . . . . . . . . . . . . . . . . . . . . . . Disengage​

     - Do not​ re-engage the autopilot.​

     - Control airplane pitch attitude​ manually with control column ​and main electric trim as needed.​

3.​ Autothrottle (if engaged)​ . . . . . . . . . . . . . . . . . . . . . . Disengage​

     - Do not​ re-engage the autothrottle.​

4.​ If​ the runaway stops​ after the autopilot is disengaged: [end of checklist]

5 ​ If​ the runaway continues​ after the autopilot is disengaged:​

     - STAB​ TRIM CUTOUT​switches (both). . . . . . . . . . . CUTOUT

  - ​If​ the runaway continues:​  

          - Stabilizer ​trim wheel​ ​ . . . . . . . . . . . . . . . . .  .Grasp and hold

6. Stabilizer..................................... Trim Manually

7. Anticipate trim requirements.

3

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

1. ​ Autothrottle (if engaged)​ . . . . . . . . . . . . . . . . . . . . . . Disengage​

2. Thrust lever ​(affected engine) ​ . . . . .....  Confirm​ . . . . . . . . Close​

3.​ Engine start lever ​(affected engine)​ ​ . ....Confirm​ . . .. . .CUTOFF​

4. ​ Engine fire switch ​(affected engine)​ ​ . . . Confirm​ . . . . . . . .  Pull​

[To manually unlock the engine fire switch, press the override and pull​]

5. ​ If​ the engine fire switch or ENG OVERHEAT light is ​illuminated:​

          Engine fire switch​ ​ . . . . Rotate to the stop and ​hold for 1 second ​

 

4

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

1. ​ ENGINE START switches (both)​ ​ . . . . . . . . . . . . . . . . . . . . FLT​

2. ​ Engine start levers (both). . . . . . . . . . . . . . . . . . . . . . .​ CUTOFF​

3. ​ 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]

5

Aborted Engine Start

7.1

 

CONDITION: On the ground, an aborted engine start is needed.​

OBJECTIVE: ​To shut down the engine and motor it.

1. ​ Engine start lever (affected engine)​ . . . . . . . . . . . . . . .​ CUTOFF

6

LANDING CONFIGURATION

15.1

Condition:​

In flight, the steady warning horn sounds.

 

1. ​ Ensure correct aircraft landing configuration.

7

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

1. ​ Don oxygen masks and set regulators to 100%.​

2. ​ Establish crew communications.​

 

8

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.

1. ​ 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

9

ENGINE OVERHEAT

8.5

Condition:​

An overheat is detected in the engine

1. ​ Autothrottle (if engaged)​ . . . . . . . . . . . . . . . . . . . . . . Disengage ​

2. Thrust lever ​(affected engine)​ ​ . . . . . . ​ Confirm​ .​ . . . . . . . .Close ​

3. ​ 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 -----------

4. If the ENG OVERHEAT light extinguishes:

     Run the engine at reduced thrust to keep the light extinguished.

10

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.

 

1. ​ Autopilot (if engaged)​ . . . . . . . . . . . . . . . . . . . . . . . . Disengage​

2. Autothrottle (if engaged)​ . . . . . . . . . . . . . . . . . . . . . . Disengage​

3. ​F/D switches (both)​ . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .​ OFF​

4. ​ Set the following gear up pitch attitude and thrust:​

     Flaps extended​ . . . . . . . . . . . . . . . . . . . . . . 10° and 80% N1​

     Flaps up​ . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4° and 75% N1

11

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

1. ​ Ensure correct aircraft takeoff configuration.

12

Emergency Descent

0.1

 

Condition:​

One or more of these occur:​

•​ Cabin altitude cannot be controlled​

•​ A rapid descent is needed

1. ​Advise Flight Attendants and ATC of the emergency descent.

2. ​ Passenger signs​ ​ . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON​

3. ​ Without delay, descend to the lowest safe altitude or 10,000 ​feet, whichever is higher.​

4. ​ ENGINE START switches (both)​ . . . . . . . . . . . . . . . . . . CONT​

 

5. ​ Thrust levers (both)​ . . ..Reduce thrust to​ minimum or as​ needed​ for anti-ice​

 

6. ​Speedbrake. . . . . . . . . . . . . . . . . . . . . . . . . . FLIGHT DETENT

 

7.​ 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.]

13

APU FIRE

8.1

Condition:​

Fire is detected in the APU.

 

1. ​ APU fire switch​

. . . . . . . Confirm​ .​ . . .Pull, rotate to the​ stop, and hold ​for 1 second​

 

2. ​ APU switch​ ​ . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .​ OFF

14

SMOKE, FIRE OR FUMES.

 1.  Diversion may be needed.

2.   Don oxygen masks and set regulators to 100%

3.   Don smoke googles, as needed.

15

AUTOMATIC UNLOCK

1. FLT DK DOOR lock selector ....... Rotate to DENY and hold for 1 second.

- end of procedure -