Flashcards
Emergencies - 1
Cards in this deck (15)
- 1ENGINE FAILURE DURING TAKEOFF RUNBEFORE ROTATION: ABORT TAKE OFF
1. Throttle Lever: BOTH IDLE
2. Rudder Keep heading control - 2SINGLE GENERATOR FAILURE / OVERVOLTAGE1. FIELD LH (or RH): OFF
2. FIELD LH (or RH): ON
If the LH (or RH) GENERATOR caution stays displayed
3. FIELD LH (or RH): OFF
4. Avionic LH: OFF
5. ADF: OFF
If conditions permit:
7. Land as soon as practicable
6. CROSS BUS LH (or RH) OFF - 3BOTH GENERATORS FAILURE1. FIELD LH and RH BOTH OFF
2. FIELD LH and RH BOTH ON
If the LH (or RH) GENERATOR caution stays displayed
3. Verify good ammeter indications on restored alternator
4. Refer to Single generator failure / overvoltage drill
If both LH and RH GENERATOR cautions stay displayed
3. FIELD LH and RH BOTH OFF
4. CROSS BUS LH and RH BOTH OFF
If engine starting battery modification is applied
5. EMERG BATT switch ON
6. Land as soon as practical.
If engine starting battery modification is not applied
5. Land as soon as possible. - 4BOTH GENERATORS OVERVOLTAGE1. FIELD LH and RH BOTH OFF
2. FIELD LH and RH BOTH ON
If the LH (or RH) GENERATOR caution stays displayed
3. Verify good ammeter indications on restored alternator
4. Refer to Single generator failure / overvoltage drill
If both LH and RH OVERVOLT warning stay displayed
3. CROSS BUS LH and RH BOTH OFF
4. FIELD LH and RH BOTH OFF
5. FIELD LH and RH BOTH ON
If LH (or RH) OVERVOLT warning stays displayed
6. Verify good ammeter indications on restored alternator
7. Switch CROSS BUS on the restored alternator side
8. Refer to Single generator failure / overvoltage drill
If both LH and RH OVERVOLT warning stay displayed
6. FIELD LH and RH BOTH OFF
If engine starting battery modification is applied
7. EMERG BATT switch ON
8. Land as soon as practical.
If engine starting battery modification is not applied
Land as soon as possible. - 5PITOT HEATING SYSTEM FAILURE1. Pitot heat switch OFF
2. Verify Pitot Heating circuit breaker is IN
3. Pitot heat switch ON
4. Check PITOT HEAT caution light: - 6COOLANT LIQUID LOW LEVEL1. Check affected engine CHT/CT
If CHT is above 135°C or CT is above 120°C
2. Affected engine Reduce power setting to reduce CHT/CT up to the minimum practical
3. Land as soon as practical
If CHT/CT continues to rise and engine shows roughness or power loss
4. Affected engine SECURE
5. Land as soon as possible applying one engine inoperative landing procedure. - 7GEAR PUMP FAILUREIf TRANS light is OFF
1. Continue the mission monitoring the caution light.
If TRANS light is ON
2. Landing gear is not locked in UP position - 8ENGINE SECURING1. Throttle Lever IDLE
2. Ignition BOTH OFF
3. Propeller Lever FEATHER
4. Fuel Selector OFF
5. Electrical fuel pump OFF - 9PROPELLER OVERSPEEDING1. Throttle Lever REDUCE power to minimum practical
2. Propeller Lever REDUCE as practical (not in feathering)
3. RPM indicator CHECK - 10CHT/CT LIMIT EXCEEDANCE1. Check affected engine CHT/CT
If CHT is above 135°C or CT is above 120°C
2. Affected engine Reduce power setting to reduce CHT/CT up to the minimum practical
3. Land as soon as practical
If CHT/CT continues to rise and engine shows roughness or power loss
4. Affected engine SECURE (see engine securing procedure on
Para. 3)
5. Land as soon as possible applying one engine inoperative landing procedure. - 11OIL TEMPERATURE LIMIT EXCEEDANCE1. OIL PRESS CHECK
If oil pressure is within limits
2. Affected engine Reduce power setting to minimum applicable
3. Affected engine Keep propeller speed higher than 2000 RPM
If oil temperature does not decrease
4. Airspeed INCREASE
5. Land as soon as practical keeping the affected engine to the minimum necessary power
6. Monitor OIL PRESS and CHT/CT
if engine roughness / vibrations or erratic behaviour is detected:
7. Affected engine SECURE
8. Land as soon as possible - 12OIL PRESSURE LIMITS EXCEEDANCE1. OIL PRESS CHECK
If oil pressure exceeds upper limit (7 bar)
2. Throttle Lever first REDUCE affected engine power by 10%
3. Propeller Lever Keep low rpm
4. OIL PRESS CHECK (verify if within limits)
5. Land as soon as practical
If oil pressure is under the lower limit (0.8 bar)
2. Land as soon as practical
If oil pressure is continuously decreasing
3. Affected engine SECURE
4. Land as soon as possible - 13LOW FUEL PRESSURE1. Fuel press CHECK
2. Fuel quantity CHECK
3. Fuel consumption MONITOR
If a fuel leakage is deemed likely
4. Land as soon as possible.
If a fuel leakage can be excluded:
4. Electrical fuel pump ON
5. Feed the affected engine by means of opposite side fuel tank
If pressure does not come back within the limits
6. Land as soon as practical - 14UNINTENTIONAL FLIGHT INTO ICING CONDITIONS1. Carburettor heat BOTH ON
2. Pitot heat ON
3. Fly as soon as practical toward a zone clear of visible moisture, precipitation and with higher temperature, changing altitude and/or direction.
4. Control surfaces Move continuously to avoid locking
5. Propellers rpm INCREASE to prevent ice build-up on the blades - 15ELECTRICAL PITCH TRIM CONTROL FAILUREa) Trim Runaway:
In the event of trim runaway:
1. AP DISC switch (if AP is installed) PRESS and HOLD
2. TRIM DISC switch OFF
3. AP DISC switch (if AP is installed) RELEASE
4. Trim aircraft using trim wheel
b) Trim Jamming:
Should trim control be jammed / inoperative:
1. Pitch trim breaker CHECK
If circuit breaker is OUT:
2. Trim aircraft using trim wheel
If circuit breaker is IN:
2. TRIM DISC switch OFF
3. Trim aircraft using trim wheel
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- 1 P2006 (Emergencies) Flashcards on Emergencies - 1, created by Emirhan Dikicibaşı on 12/01/2023.
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- Emirhan Dikicibaşı
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