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Piper PA-28-161 Warrior II (Just Flight) Emergency Procedures
Immediate Action Procedures
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12 procedures
- 1StarterCRANK ENGINE
- 2MixtureIDLE CUT-OFF
- 3ThrottleOPEN
- 4Fuel pumpOFF
- 5Fuel selectorOFF
- 1If sufficient runway remains for a normal landingLAND STRAIGHT AHEAD
- 2If sufficient altitude has been gained to attempt a restart:
- 3Fuel selectorSET TO FULLEST TANK
- 4Fuel pumpON
- 5MixtureCHECK RICH
- 6Carburettor heatON
- 7If power is not regainedPROCEED WITH POWER OFF LANDING
- 1If at low altitude: Airspeed63 KIAS MINIMUM, prepare for power off landing
- 2If altitude permits:
- 3Fuel selectorSWITCH TO FULLEST TANK
- 4Fuel pumpON
- 5MixtureRICH
- 6Carburettor heatON
- 7PrimerLOCKED
- 8Engine gaugesCHECK FOR INDICATION OF CAUSE
- 9When power is restored: Carburettor heat - OFF, Fuel pump - OFF
- 10If power is not restored - TRIM FOR 73 KIAS and prepare for a power off landing
- 1Trim for 73 KIAS
- 2Locate a suitable field and establish a spiral pattern 1,000 ft above the field at the downwind position
- 3When the field can be easily reachedSLOW TO 63 KIAS for the shortest landing
- 1Fuel selectorOFF
- 2ThrottleCLOSED
- 3MixtureIDLE CUT-OFF
- 4Fuel pumpOFF
- 5Cabin heatOFF
- 6Proceed with the power off landing procedure
- 1BATT MASTR switchOFF
- 2ALTR switchOFF
- 3Cabin heatOFF
- 4Land as soon as possible
- 1Oil annunciator lightON
- 2Pressure indicatorIN LOW SECTOR
- 3ThrottleREDUCE AS FAR AS POSSIBLE
- 4Oil temperatureCHECKED
- 5If oil temperature in the red sectorREDUCE THROTTLE
- 6Prepare for a forced landing and land as soon as possible
- 1Fuel pumpON
- 2Fuel quantityCHECKED
- 3Fuel selectorSWITCH TANKS
- 1Check the circuit breaker panel; close an open breaker only once. If it opens again the equipment has failed
- 2AmmeterCHECK TO VERIFY INOPERATIVE ALTERNATOR
- 3If the ammeter shows zero: ALTR switchOFF
- 4Reduce electrical loads to minimum
- 5ALTR FIELD circuit breakerCHECK AND RESET AS REQUIRED
- 6ALTR switchON
- 7If power is not restored: ALTR switch - OFF, reduce loads and land as soon as practical. The battery is the only remaining source of power
- 1Flight into known icing conditions is PROHIBITED
- 2Carburettor heatON
- 3Cabin heatFULL HOT
- 4Pitot heatON
- 5EngineMAX POWER / RPM
- 6Adjust course and/or altitude to obtain the best outside air conditions. Divert to the nearest airport
- 1Intentional spins are PROHIBITED
- 2RudderHOLD OPPOSITE DIRECTION OF ROTATION
- 3YokeFULL FORWARD, AILERONS NEUTRAL
- 4ThrottleIDLE
- 5When spinning stops - CENTRALISE RUDDER, LEVEL THE WINGS AND EASE OUT OF THE DIVE
- 1Pitot heatON
- 2If erroneous indications persist, carry out a precautionary approach maintaining an adequate airspeed margin above stall warning activation speed
FLIGHT2.23.0Checklist
Piper PA-28-161 Warrior II (Just Flight)MSFS 2024 · Emergency Procedures · 12procedures · 64 steps
Engine Failure During Start5 steps
| 01 | StarterCRANK ENGINE | |
| 02 | MixtureIDLE CUT-OFF | |
| 03 | ThrottleOPEN | |
| 04 | Fuel pumpOFF | |
| 05 | Fuel selectorOFF |
Engine Failure During Take-off7 steps
| 01 | If sufficient runway remains for a normal landingLAND STRAIGHT AHEAD | |
| 02 | If sufficient altitude has been gained to attempt a restart: | |
| 03 | Fuel selectorSET TO FULLEST TANK | |
| 04 | Fuel pumpON | |
| 05 | MixtureCHECK RICH | |
| 06 | Carburettor heatON | |
| 07 | If power is not regainedPROCEED WITH POWER OFF LANDING |
Engine Failure In Flight10 steps
| 01 | If at low altitude: Airspeed63 KIAS MINIMUM, prepare for power off landing | |
| 02 | If altitude permits: | |
| 03 | Fuel selectorSWITCH TO FULLEST TANK | |
| 04 | Fuel pumpON | |
| 05 | MixtureRICH | |
| 06 | Carburettor heatON | |
| 07 | PrimerLOCKED | |
| 08 | Engine gaugesCHECK FOR INDICATION OF CAUSE | |
| 09 | When power is restored: Carburettor heat - OFF, Fuel pump - OFF | |
| 10 | If power is not restored - TRIM FOR 73 KIAS and prepare for a power off landing |
Power Off Landing3 steps
| 01 | Trim for 73 KIAS | |
| 02 | Locate a suitable field and establish a spiral pattern 1,000 ft above the field at the downwind position | |
| 03 | When the field can be easily reachedSLOW TO 63 KIAS for the shortest landing |
Engine Fire In Flight6 steps
| 01 | Fuel selectorOFF | |
| 02 | ThrottleCLOSED | |
| 03 | MixtureIDLE CUT-OFF | |
| 04 | Fuel pumpOFF | |
| 05 | Cabin heatOFF | |
| 06 | Proceed with the power off landing procedure |
Electrical Fire4 steps
| 01 | BATT MASTR switchOFF | |
| 02 | ALTR switchOFF | |
| 03 | Cabin heatOFF | |
| 04 | Land as soon as possible |
Low Oil Pressure6 steps
| 01 | Oil annunciator lightON | |
| 02 | Pressure indicatorIN LOW SECTOR | |
| 03 | ThrottleREDUCE AS FAR AS POSSIBLE | |
| 04 | Oil temperatureCHECKED | |
| 05 | If oil temperature in the red sectorREDUCE THROTTLE | |
| 06 | Prepare for a forced landing and land as soon as possible |
Low Fuel Pressure3 steps
| 01 | Fuel pumpON | |
| 02 | Fuel quantityCHECKED | |
| 03 | Fuel selectorSWITCH TANKS |
Alternator Failure7 steps
| 01 | Check the circuit breaker panel; close an open breaker only once. If it opens again the equipment has failed | |
| 02 | AmmeterCHECK TO VERIFY INOPERATIVE ALTERNATOR | |
| 03 | If the ammeter shows zero: ALTR switchOFF | |
| 04 | Reduce electrical loads to minimum | |
| 05 | ALTR FIELD circuit breakerCHECK AND RESET AS REQUIRED | |
| 06 | ALTR switchON | |
| 07 | If power is not restored: ALTR switch - OFF, reduce loads and land as soon as practical. The battery is the only remaining source of power |
Icing6 steps
| 01 | Flight into known icing conditions is PROHIBITED | |
| 02 | Carburettor heatON | |
| 03 | Cabin heatFULL HOT | |
| 04 | Pitot heatON | |
| 05 | EngineMAX POWER / RPM | |
| 06 | Adjust course and/or altitude to obtain the best outside air conditions. Divert to the nearest airport |
Spin Recovery5 steps
| 01 | Intentional spins are PROHIBITED | |
| 02 | RudderHOLD OPPOSITE DIRECTION OF ROTATION | |
| 03 | YokeFULL FORWARD, AILERONS NEUTRAL | |
| 04 | ThrottleIDLE | |
| 05 | When spinning stops - CENTRALISE RUDDER, LEVEL THE WINGS AND EASE OUT OF THE DIVE |
Airspeed Indicating System Failure2 steps
| 01 | Pitot heatON | |
| 02 | If erroneous indications persist, carry out a precautionary approach maintaining an adequate airspeed margin above stall warning activation speed |