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REJECTED TAKEOFF - BELOW V1
1. Abort
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ENGINE FAILURE OR FIRE ON TAKEOFF - AT OR ABOVE V1
- 1. Rotate - VR.
- 2. Landing Gear - UP (after positive rate-of-climb).
- 3. Climb - V2 until1500ft AGL
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ENGINE FIRE (ENGINE FIRE SWITCH ILLUMINATED, FIRE BELL ACTIVATED)
- 1. Throttle (affected Engine) - IDLE.
- IF FIRE LIGHT REMAINS ON AFTER 15 SECONDS
- 2. Engine Fire Switch (affected engine) - LIFE COVER and PUSH
- 3. Either Illuminated BOTTLE ARMED Light - PUSH.
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ENGINE FAILURE DURING FINAL APPROACH
- 1. AP/TRIM/NWS Disengage Switch - PRESS and RELEASE.
- 2. Power (operating engine) - INCREASE (as required).
- 3. Flaps - APPROACH SCHEDULE.
- 4. Airspeed - VAPP MINIMUM.
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DOUBLE ENGINE FLAMEOUT/RESTART - TWO ENGINES
- 1. Ignition - BOTH ON
- 2. Fuel Boost Pump - BOTH ON
- 3. Throttles - IDLE
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COCKPIT OR CABIN FIRE OR SMOKE DETECT LIGHT ON
- 1. Oxygen Masks - DON and EMERGENCY
- 2. Smoke Goggles - DON, as required
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CABIN DECOMPRESSION (INDICATED BY A CABIN ALT 8500FT LIGHT OR 10,000 FEET CABIN ALTITUDE AURAL WARNING OR BOTH)
- 1. Oxygen Masks - DONE and 100%.
- 2. Oxygen Microphone Switches - MIC OXY MASK.
- 3. Emergency Descent - AS REQUIRED.
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EMERGENCY DESCENT
- 1. Throttles - IDLE.
- 2. Speedbrakes/Spoilers - DEPLOY
- 3. Initial Pitch Attitdue - 20° Down.
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BATTERY OVERHEAT (BATT O'TEMP LIGHT ON)
DUAL BATTERY INSTALLATION ONLY
- 1. Amperage - CHECK.
- 2. Battery Disconnect Switch - Position to overheated battery.
- 3. Amperage - NOTE DECREASE.
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BATTERY OVERHEAT (BATT O'TEMP LIGHT ON)
SINGLE BATTERY INSTALLATION ONLY
1. Battery Switch - OFF.
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AUTOPILOT FAILURE
1. AP/TRIM/NWS Disengage Switch - PRESS
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PRIMARY PITCH TRIM RUNAWAY OR FAILURE
- 1. AP/TRIM/NWS Disengage Switch - PRESS.
- 2. Secondary Trim Switch - ON (lift guarded cover).
- 3. Trim - AS REQUIRED. (SEC TRIM FAULT Light May Be Illuminated Until the Secondary Trim is Actuated.)
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UNCONTROLLED AIRPLANE ROLL
- 1. AP/TRIM/NWS Disengage Switch - PRESS.
- 2. Control Wheel - STOP ROLL - APPLY OPPOSITE ROLL CONTROL.
- IF ROLL NOT ARRESTED3. Spoiler Hold Down Switch - ON.
- IF ROLL STILL NOT ARRESTED4. Auxiliary Hydraulic Power - OFF.
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JAMMED ROLL CONTROL SYSTEM
- 1. AP/TRIM/NWS Disengage Switch - PRESS.
- 2. Pilot and Copilot Control Wheels - RELEASE.
- 3. Aileron/Spoiler Disconnect T-Handle - PULL.
- 4. Pilot's and Copilot's Control Wheels - VERIFY ROLL RESPONSE.
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THRUST REVERSER INADVERTENT IN-FLIGHT DEPLOYMENT (ARM, UNLOCK, AND DEPLOY LIGHTS ON)
- 1. Control Wheel/Autopilot - GRIP/DISENGAGE
- 2. Stow Switch (affected engine) - EMER.
- 3. Throttle (affected engine) - CHECK IDLE.
- 4. Airspeed - REDUCE TO 200KIAS MAXIMUM.
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THRUST REVERSER UNLOCK LIGHT ON INFLIGHT (NO OTHER INDICATION OF DEPLOYMENT)
- 1. Stow Switch - EMER (AFFECTED ENGINE).
- 2. Thrust Reverser Levers - CHECK THRUST REVERSER LEVERS AT STOWED (FULL FORWARD) POSITION.
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