QRH: Immediate Action Items Flashcards

1
Q

Aborted Engine Start L, R

A

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

  1. FUEL CONTROL switch (affected side)………………….CUTOFF

QRH Rev. 17: 7.1

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2
Q

Airspeed Unreliable

A

Condition: Airspeed or Mach indications are suspected to be unreliable. (Items which can indicate unreliable airspeed are listed in the Additional Information section [of the QRH].)
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 disengage switch……Push
  2. A/T ARM switches (both)……….OFF
  3. F/D switches (both)…………………OFF
  4. Set the following gear up pitch attitude and thrust:
    Flaps extended….10 degrees and 85% N1
    Flaps up………………4 degrees and 70% N1

QRH Rev. 17: 10.1

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3
Q

[ ] CABIN ALTITUDE

A

Condition: Cabin altitude is excessive

  1. Don the oxygen masks.
  2. Establish crew communications.
  3. Check the cabin altitude and rate.
  4. If the cabin altitude is uncontrollable:
    [BRC Note: if vents are closed and altitude is increasing]
    SUPRNMRY OXYGEN switch…..
    ….Push to ON and hold for 1 second
    Without delay, descend to the lowest safe altitude or 10,000 feet, whichever is higher.
    To descend:
    [BRC note: this is without automation]
    Move the thrust levers to idle.
    Extend the speed brakes.
    If structural integrity is in doubt, limit the airspeed and avoid high maneuvering loads.
    Descend at VMO/MMO
    [BRC note: with automation
    spin down altitude in altitude window
    FLCH
    extend speed brake
    speed intervene
    adjust altitude]

QRH Rev 17: 2.1

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4
Q

Dual Eng Fail/Stall

A

Condition: Engine speed for both engines is below idle.

  1. FUEL CONTROL switches (both)………….CUTOFF, then RUN
  2. RAM AIR TURBINE switch……….Push and hold for 1 second

QRH Rev 17: 7.2

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5
Q

[ ] ENG AUTOSTART L, R

A

Condition: During a ground start, one of these occurs:
• Autostart did not start the engine
• Fuel control switch is in RUN at low engine RPM with the autostart switch OFF

  1. FUEL CONTROL switch (affected side)………………….CUTOFF

QRH Rev 17: 7.4

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6
Q

Eng Lim / Surge / Stall L, R

A

Condition: One or more of these occur:
• Engine indications are abnormal
• Engine indications are quickly nearing or show an exceedance
• 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

  1. A/T ARM switch (affected side)….Confirm……..OFF
  2. Thrust lever (affected side)………Confirm………Retard until engine indications stay within limits or the thrust lever is at idle

QRH Rev 17: 7.5

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7
Q

Eng Svr Damage / Sep L, R

A

Condition: One or more of these occur:
• Airframe vibrations with abnormal engine indications
• Engine separation

  1. A/T ARM switch (affected side)………………Confirm…OFF
  2. Thrust lever (affected side)……………………Confirm….Idle
  3. FUEL CONTROL switch (affected side)…Confirm…CUTOFF
  4. Engine fire switch (affected side)…………..Confirm….Pull

QRH Rev 17: 7.10

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8
Q

[ ] FIRE ENG L, R

A

Condition: Fire is detected in the engine

  1. A/T ARM switch (affected side)….Confirm….OFF
  2. Thrust lever (affected side)….Confirm….Idle
  3. FUEL CONTROL switch (affected side)…Confirm…CUTOFF
  4. Engine fire switch (affected side)….Confirm….Pull
  5. If the FIRE ENG message shows:
    Engine fire switch (affected side)……Rotate to the stop and hold for 1 second

QRH Rev 17: 8.2

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9
Q

[ ] STABILIZER

A

Condition: One of these occurs:
• Stabilizer movement without a signal to trim
• The stabilizer is failed

  1. STAB cutout switches (both)………………………..CUTOUT
  2. Do not exceed the current airspeed.

QRH Rev 17: 9.1

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