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39 Cards in this Set
- Front
- Back
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Fire on Deck
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1. PCL IDLE Stop - Disengage
2. PCLs - Off 3. Stop Aircraft 4. Engine Master switches - Off 5. Notify ground control or tower 6. Battery switch - Off 7. Abandon Aircraft |
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Tailpipe Fire
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1. PCL Idle stop - Disengage
2. PCLs - Off 3. Battery Switch - Norm 4. Engine Master Switch - On 5. Engine Starter Switch - Start (15 seconds) If Fire Persists 6. Engine Master Switches - Off 7. Batter Switch - off 8. Abandon Aircraft |
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Wet Start
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1. Power Control Lever - Off
2. Motor engine for 15 seconds 3. Engine starter switch - Stop |
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Hung Start
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1. PCL - Off
2. Engine Starter Switch - Stop |
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Hot Start
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1. PCL - Off
2. Engine Starter swtich - Stop 3. Record time/temperature excess |
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Engine Rollback
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1. Generator switch - Off
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Emergency Exit or Egress
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1. PCL Idle stop - Disengaged
2. PCLs - Off 3. Stop Aircraft 4. Engine Master switches - Off 5. Battery switch - Off 6. Canopy - Jettison (if required) 7. Abandon Aircraft |
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Severe Nosewheel Shimmy on Takeoff
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1. Below 65 KIAS - Abort
2. Above 65 KIAS - Apply Slight backstick to reduce shimmy; avoid premature rotation to the takeoff attitude |
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Unsafe Gear Up Indication
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1. Do not exceed 165 KIAS
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Securing Engine in Flight
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1. PCL Idle stop - Disengage
2. PCL - Off |
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Abort
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1. PCL Idle Stop - Disengage
2. PCLs - Idle or Secure 3. SPD BK switch - Out 4. Brakes - As Required 5. Hook - Down (if required) 6. Transmit Intentions If crash seems inevitable 7. PCLs - Off 8. Engine Master Switches - Off 9. Battery Switch - off 10 Canopy - Jettison (if required) 11 Abandon aircraft when completely stopped |
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Engine Fire/Failure During Takeoff
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1. Abort (if feasible)
If unable to abort 2. PCLs - Maximum Thrust When safely airborne 3. Landing gear - up 4. Establish safe flying speed 5. Reduce power on affected engine If Fire/failure is confirmed, secure affected engine: 6. PCL Idle stop - Disengage 7. PCL - Off 8. Engine Master switch - Off If fire persists: 9. Eject |
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Engine Failure during Flight
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One Engine
1. PCL Idle Stop - Disengage 2. Failed engine PCL - Off 3. Failed engine Master switch - Off Both Engines Above 5000 ft AGL 1. Perform abbreviated airstart on both engines simultaneously If no light-off and if time and altitude permit: 2. Perform single normal airstart If no start: 3. Eject prior to 5000 ft AGL If unable to eject or bailout 4. Refer to Landing emergencies for flamout landing procedures Below 5000 ft and above 1000 ft AGL 1. Convert airspeed to altitude (if airspeed permits) while performing abbreviated airstart on both engines simultaneously If no light-off 2. Eject Below 1000 ft AGL 1. Convert airspeed to altitude and Eject If dirty 2. Eject immediately |
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In Flight Vibrations
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1. Alternately reduce power on each engine to Idle.
2. Secure affected engine |
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Abbreviated Airstart
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1. Airstart/Ignition button - Depress and Hold
2. PCLs - Full Forward |
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Single Engine Fire
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1. PCL - Reduce
2 Check for Secondary indications If fire is confirmed 3. PCL Idle stop - Disengage 4. PCL - Off 5. Engine Master switch - Off If fire persists 6. Eject If fire is extinguished 7. Do not attempt to relight. Land as soon as possible following single engine landing procedures If light remains on and no secondary indications are present: 8. Shut down affected engine unless in or expecting instrument conditions, in which case, operate engine at low power setting. 9. Land as soon as practicable |
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Dual Engine Fire
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1. PCLs - Reduce
2. Check for secondary indications If fire is confirmed 3. PCL Idle stop - Disengage 4. PCLs - Off 5. Engine master switches - Off If fire persists 6. Eject If fire is extinguished 7. Do not attempt relights. Execute controlled ejection. If no secondaries are present and light remains on: 8. Operate engines at lowerst practicable power settings. 9. Land as soon as practicable. |
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Electrical Fire
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1. Battery switch - Off
2. GEN switches - Off 3. Descend below 20000 feet (if practicable) 4. Electrical equipment - Off |
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Normal Airstart
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1. Battery switch - Norm/Emergency
2. Descend below 25000 ft. If possible, stabilize at minimum recommended airspeed of 180 knots. 3. PCL Idle stop - Disengage 4. PCL - Off 5. Check engine Master switch - On 6. Check circuit breakers - In 7. Check minimum rpm - 8 percent 8. Airstart/Ignition button - Depress 9. PCL - Idle 10. EGT - Monitor |
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Binding/Jamming of controls in Flight
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1. Maintain control with stick, rudder, and trim as necessary
2. Reduce airspeed, if feasible, to 200 kias or less 3. Climb to or remain above 7000 ft AGL 4. Attempt to free controls. |
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Smoke, Fume, and Fog
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1. RAM EMER switch - On
2. Canopy defrost switch - Off |
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Loss of Canopy or Windscreen
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1. Adjust airspeed and altitude to minimize buffet and discomfort
2. Lower seats |
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Canopy Light in Flight
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1. Canopy switch - Down (close)
2. Pressurization - On 3. Airspeed - Reduce to minimum practicable |
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Structural failure or damage
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1.Reduce airspeed as practicable. At low altitudes, convert airspeed to altitude.
2. Determine if adequate control remains for continued flight, if not, eject. If control is available 3. Climb at reduced airspeed to recommended ejection altitude, 7000 ft AGL or higher. |
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Instrument Power failure
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1. Instr AC PWR switch - NO 2 INV
2. Check flight instruments for normal operation. |
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Hydraulic Power System Failure
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1. Hyd Boost Switch - Off
2. Reduce airspeed below 200 KIAS, trim as necessary |
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Hydraulic Boost Failure
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1. Hyd Boost Switch - Off
2. Reduce airspeed below 200 KIAS, trim as necessary. |
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Uncommanded Control Inputs
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1. Maintain control with stick, rudder, and trim, as necessary.
2. Elecator trim guage - Check If runaway elevator trim: 3. Execute runaway elevator trim procedures. If not runaway elevator trim: 4. Hyd Boost switch - Off 5. Reduce airspeed to below 200 KIAS |
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Runaway Elevator Trim
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1. Trim disconnect switch - Select
2. Trim Cont circuit breaker - Pull |
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Wheelbrake Failure
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1. PCL Idle stop - Disengaged
2. PCLs - Off 3. Arresting hook - Down 4. Attempt to bring aircraft to a halt and remain on prepared surface. If crash seems inevitable: 5. Engine Master switches - Off 6. Battery switch - Off 7. Jettison canopy 8. Abandon aircraft when completely stopped |
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Asymmetrical Flap Operation
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1. Reposition flap selector immediately.
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Cycling Wing Flaps
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1. Establish 145 to 165 KIAS.
2. Maintain safe altitude. |
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Oxygen System Failure
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1. Emergency Oxygen supply - Activate (if required)
2. Descend to aircraft altitude of 10000 feet or less. |
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Composite Disconnect Failure
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1. Oxygen valve - Off
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Single Engine Failure in the Landing Configuration
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1. Maximum power both engines, simultaneously retracting speedbrakes and leveling the wings.
2. Control rate of descent |
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Loss of Nose Landing Gear Strut or Wheel
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1. Do not retract gear
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Out of Control Flight
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Below 7000 ft AGL
1. Eject Above 7000 ft AGL 2. Flight controls - Visually check Neutral 3. Harness - Locked 4. PCLs - Idle 5. Speedbrakes - In 6. Trim - 2 deg to 8 deg Noseup 7. AOA, airspeed, turn needle - Analyze If recovery is indicated and and airspeed is greater than 150 knots 8. Recover (not to exceed 17 units) If spin is confirmed 9. Initiate spin recovery If high-speed spiral is confirmed 10. Initiate high speed spiral recovery procedures |
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Spin Recovery
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1. Flight controls - Maintain neutral
2. Rudder - Neutral When AOA breaks or rotation ceases: 3. Rudder - Neutral If airspeed is greater than 150 knots 4. Recover (not to exceed 17 units AOA). If recovery is not indicated passing 7000 ft AGL 5. Eject |
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High Speed Spiral Recovery
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1. Flight controls - Maintain neutral
2. Rudder - Smoothly apply opposite to turn needle When rotation ceases 3. Rudder - Neutralize 4. Recover (not to exceed 4g's or 17 units AOA). If recovery is not indicated passing 7000 ft AGL 5. Eject |
