777 Flashcards

1
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:

PASS OXYGEN switch . . . …………… Push to ON and hold for 1 second

Without delay, descend to the lowest safe altitude or 14,000 feet, whichever is higher.

To descend: Move the thrust levers to idle. Extend the speedbrakes. If structural integrity is in doubt: Limit airspeed and avoid high maneuvering loads. Descend at Vmo/Mmo. If fuel is not critical and terrain permits: The aircraft may descend to 10,000 feet or MSA, which ever is higher, in order to remove the need for oxygen masks.

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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.)

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

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3
Q

Automatic Unlock

A

Condition: The correct emergency access code is entered.

  1. FLT DK DOOR lock selector . . . . ……….. Rotate to DENY and hold for 1 second
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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
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5
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 appropriate limits or the thrust lever is at idle
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6
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
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7
Q

Aborted engine start

A

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

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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 stays shown:
Engine fire switch . . . . . . . . . . . . . . . . . . . .Rotate to the stop and hold for 1 second

If after 30 seconds, the FIRE ENG message stays shown:
Engine fire switch (affected side) . . . . . . . . . . . . . . . Rotate to the other stop and hold for 1 second

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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.
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10
Q

Evacuation

A

Condition: An evacuation is needed.

1 Parking brake …………………. Set

2 EVAC COMMAND then HORN SHUTOFF . ………… ON/PULL Activate the EVAC COMMAND to warn crew, then pull HORN SHUTOFF to silence.

3 OUTFLOW C C VALVE switches (both) . . . . . . . . . . . …. MAN F/O

4 OUTFLOW VALVE MANUAL switches (both) . . . . . . . . . . . . . . . ….. Hold in OPEN until the outflow valve indications show fully open to depressurize the airplane

5 FUEL CONTROL switches (both) . . . . . . . . . . . . . . . … CUTOFF

6 Advise the cabin to evacuate.

7 Advise the tower.

8 Engine fire switches (both) . . . . . . . . . . . . . Pull

9 APU fire switch . . . . . . ….. Override and pull

10 If an engine or APU fire warning light is illuminated:
Illuminated fire switch . . . . . . . . …………… Rotate to the stop and hold for 1 second

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11
Q

FIRE APU

A

Condition: Fire is detected in the APU.

  1. APU fire switch . . . . . ….. Confirm………. Pull, rotate to the stop and hold for 1 second
  2. Choose one: FIRE APU message stays shown: Plan to land at the nearest suitable airport.Go to step 3

FIRE APU message blanks:Go to step 3

  1. Do not accomplish the following checklist: APU SHUTDOWN
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