20656924
Description
Flashcards by Rieul Gendron, updated more than 1 year ago
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Created by Rieul Gendron
over 4 years ago
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| Question | Answer |
| Memory items for: Engine Failure Prior to rotation | Both power levers to idle and apply brakes. See POH 3.3.1 |
| Memory items for: Engine failure airborne, after VMC, autofeather ON. | Set max power, confirm flaps 10, confirm if affected prop has autofeathered and feather only if no autofeather and total power loss. See POH 3.3.3 |
| Memory items for: Engine failure in flight (autofeather off) | Set max power, and, for the failed engine: Power lever: Retard to 10 PSI position, prop lever: feather, fuel lever: off See POH 3.3.4 |
| Memory items for: Left or right engine fire on ground | Stop aircraft Set parking brake Lift the fire bell mute switch Both power levers idle Feather both prop levers Both fuel levers off Affected engine 'fuel emergency' switch off Pull the affected engine 'fire pull handle' Both 'boost pump' switches off Evacuate aircraft See POH 3.4.1 |
| Memory items for: Left or right engine fire in flight | Lift the fire bell mute switch Set max power (unaffected engine) For the affected engine: Power lever: retard to 10 PSI position, prop lever: feather, fuel lever: off, 'fuel emergency' switch: off, 'fire pull handle': pull, 'boost pump' switch: off See POH 3.4.2 |
| Memory items for: one engine inoperative missed approach (flaps 10). | Set max power on the unaffected engine and climb at 80 KIAS. See POH 3.7.2 |
| Memory items for: no light-up during start or failure to accelerate during start | For the affected engine: Fuel lever: off, start switch: continue to motor for 10 seconds See POH 3.8.2 and 3.8.3 |
| Memory items for: High T5 temperature during start | For the affected engine: Fuel lever: off, Start switch: continue to motor for 10 seconds See POH 3.8.4 |
| Memory items for: Generator light fails to appear following start | Ensure the generator switch of the affected engine is OFF, then, if the light still fails to appear: 'BUS TIE' switch: OPEN MASTER switch: OFF Shut down aircraft following normal procedures See POH 3.8.6 |
| Memory items for: Stall recovery | Reduce pitch attitude and roll wings level, set max power and increase airspeed to VREF or higher. See POH 3.9 |
| Memory items for: engine shutdown in flight | Set max power on unaffected engine, and, for the affected engine: Power lever: retard to 10 PSI position, Prop lever: feather, Fuel lever: off. See POH 3.10.1 and 3.10.4 |
| Memory items for: Uncommanded feather | Set max power on unaffected engine, and, for affected engine, power lever: idle See POH 3.11.2 |
| Memory items for: Propeller reversal (blade latches NOT fitted) | For the affected engine: Power lever: retard to 10 PSI position, Prop lever: feather, Fuel lever: off. See POH 3.11.3 |
| Memory items for: 'Reset Props' light during final approach | Set prop levers to MAX RPM. See POH 3.11.6 |
| Memory items for: Aileron trim tab runaway | Reduce speed to relieve control forces, press aileron trim switch in the appropriate direction, and, when control forces are relieved, pull AIL TRIM ACT circuit breaker. See POH 3.17.1 |
| Memory items for: Engine failure airborne, prior to VMC | Power levers - retard as needed to maintain directional control. Land straight ahead (not necessarily runway heading). See POH 3.3.2 |
| Memory items for: Engine oil pressure light | Check the oil pressure gauge and if showing less than 40 PSI, shut down the affected engine. See POH 3.10.3 |
| Memory items for: T5 exceeds limit | Reduce the power lever of the affected engine until acceptable T5 is achieved and if acceptable T5 cannot be achieved: shut down the affected engine. See POH 3.10.5 |
| Memory items for: engine overspeed (NG exceeds limit) | Power lever of affected engine: reduce until acceptable NG is achieved. If acceptable NG cannot be achieved: shut down affected engine See POH 3.10.6 |
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