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13 Cards in this Set
- Front
- Back
- 3rd side (hint)
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Aborted Engine Start (7.1) |
1. Engine start lever (affected side)
CUTOFF |
Condition: On the ground, an aborted engine start is needed. Objective: To shut down the engine and motor it. |
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Airspeed Unreliable (10.1) |
1. Autopilot (if engaged) 2. Autothrottle (if engaged) 3. F/D switches (both) 4. Set the following gear UP pitch attitude and thrust: |
Condition: Airspeed or Mach indications are suspectedto 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 thePerformance Inflight chapter. |
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APU FIRE (8.1) |
1. APU FIRE SWITCH PULL, ROTATE to the stop, and hold for 1 second
OFF |
Condition: Fire is detected in the APU. |
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CABIN ALTITUDE WARNING
or Rapid Depressurization (2.1) |
1. Don oxygen masks and set regulators to 100% 2. Establish crew communications 3. Pressurization mode selector 4. Outflow VALVE switch Hold in CLOSE 5. IF cabin altitude is uncontrollable: Passenger signs ................... ON PASS OXYGEN switch .......... ON Go to Emerg. Descent 0.1 |
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. |
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Emergency Descent (0.1) |
1. Announce the emergency descent. PF will advise the cabin crew on the PA system of impending rapid descent. PM will advise ATC and obtain the area altimeter setting. 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 ** |
Condition: One or more of these occur: •Cabin altitude cannot be controlled •A rapid descent is needed. ** If structural integrity is in doubt, limit speed as much as possible and avoid high maneuvering loads. |
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ENGINE FIRE, or severe damage or separation (8.2) |
1. Autothrottle (if engaged) 2. Thrust lever (affected engine) ..... Confirm ..... CLOSE 3. Engine start lever (affected engine) ..... Confirm ..... CUTOFF 4. Engine fire switch (affected engine) ..... Confirm ..... PULL * 5. If the engine fire switch or ENG OVERHEAT light isilluminated: Engine fire switch ROTATE to the stop and hold for 1 second If after 30 seconds the engine fire switch or ENGOVERHEAT light stays illuminated: Engine fire switch ROTATE to theother stop andhold for 1 second |
Condition: One or more of these occur: •Engine fire warning •Airframe vibrations with abnormal engine indications •Engine separation. * To manually unlock the engine fire switch, press the override and pull. |
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Engine Limit or Surge or Stall (7.2) |
1. Autothrottle (if engaged) DISENGAGE 2. Thrust lever (affected engine) ..... Confirm ..... RETARD until engine indicationsstay within limits or the thrust lever is closed |
Condition: One or more of these occur: •Engine indications are abnormal •Engine indications are rapidly approachingor 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. |
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ENGINE OVERHEAT (8.4) |
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 Severe Damage or Seperation checklist (8.2) |
Condition: An overheat is detected in the engine. |
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LANDING CONFIGURATION (15.1) |
1. Assure correct airplane landing configuration |
Condition: In flight, the steady warning horn sounds. |
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Loss of Thrust on Both Engines (7.4) |
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 950 or there is no increase in EGT within 30 seconds: Engine start lever (affected side) ..... Confirm ..... CUTOFF, then IDLE detent If EGT again reaches 950 or there is no increase in EGT within 30 seconds, repeat as needed. |
Condition: Both of these occur: •Both engines have a loss of thrust •Both ENG FAIL alerts show. Objective:To restart at least one engine. |
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Runaway Stabilizer (9.1) |
1. Control column 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 NNC. 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 |
Condition: Uncommanded stabilizer trim movement occurs continuously. |
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TAKEOFF CONFIGURATION (15.1) |
1. Assure correct airplane takeoff configuration. |
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. |
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