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MSFS 2024 · General Aviation
Pilatus PC-12 Emergency Procedures
Immediate Action Procedures
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8 procedures
- 1PCLIDLE
- 2BrakingAS REQUIRED
- 3Engine switch (if overrun or collision likely)OFF
- 4FUEL EMERG shut offPRESS LATCH DOWN AND PULL LEVER UP
- 5MASTER POWER switchEMERGENCY OFF
- 6AircraftEVACUATE AFTER STOPPING
- 1Aircraft - LAND STRAIGHT AHEAD, MAX 30 DEG BANK TO AVOID OBSTRUCTIONS
- 2Flaps40 DEG
- 3Final approach speed at 10,450 lb88 KIAS, NOT BELOW DYNAMIC SPEED BUG
- 4PCLIDLE
- 5Engine switchOFF
- 6FUEL EMERG shut offPRESS LATCH DOWN AND PULL LEVER UP
- 7MASTER POWER switch after touchdownEMERGENCY OFF
- 8AircraftEVACUATE AFTER STOPPING
- 1Landing gearDOWN IF LANDING SITE ALLOWS, OTHERWISE KEEP UP
- 2Flaps40 DEG
- 3Final approach speed at 10,450 lb - 88 KIAS FLAPS 40, 91 KIAS FLAPS 30, 101 KIAS FLAPS 15
- 4PCLIDLE
- 5Engine switchOFF
- 6FUEL EMERG shut offPRESS LATCH DOWN AND PULL LEVER UP
- 7MASTER POWER switch after touchdownEMERGENCY OFF
- 1AutopilotUSE FLC AT BEST GLIDE AND HDG OR NAV MODE
- 2Best glide (propeller feathered)119 KIAS AT 10,450 LB, 110 KIAS AT 9,040 LB
- 3PCLIDLE
- 4AircraftPROCEED TO NEAREST AIRFIELD AVOIDING HIGH TERRAIN
- 5Remaining fuelCHECK
- 6Air Start - CARRY OUT IF NO MECHANICAL DAMAGE SUSPECTED AND TIME PERMITS
- 7Emergency DescentMAKE IF CABIN ALTITUDE ABOVE 10,000 FT
- 8Forced LandingMAKE IF NO AIR START
- 1PCLREDUCE TO MINIMUM TO SUSTAIN FLIGHT
- 2ACS Bleed Air switchOFF FOR 5 SECONDS, RESET TO ON
- 3Electrical HEAT/COOL switchINHIBIT
- 4PCL - IDLE AND DESCEND TO DENSER AIR, IF REQUIRED TO 15,000 FT
- 5ACS Bleed Air switchOFF
- 6Aircraft - LAND AS SOON AS POSSIBLE, RETAINING GLIDE CAPABILITY TO THE SELECTED AIRFIELD
- 1Go Around switch (if autopilot engaged)PRESS
- 2POWER CONTROL LEVERSET TO T/O
- 3Climb airspeed85 KIAS
- 4FlapsSET 15 DEG (MAX 165 KIAS)
- 5Climb airspeed pusher normal mode95 KIAS
- 6Climb airspeed pusher ice mode105 KIAS
- 7Landing Gear SelectorUP WITH POSITIVE RATE OF CLIMB
- 8Yaw DamperON
- 1Engine switchOFF TO ABORT THE START OR DRY MOTORING RUN
- 2EPECS - AUTOMATICALLY ABORTS ON ITT EXCEEDANCE, HUNG START, NO LIGHT-OFF OR STARTER PUSH
- 3Dry motor run30 SECONDS COMMANDED AUTOMATICALLY
- 4STARTER annunciatorGREEN IN PFD ENGINE WINDOW
- 5Dry Motoring Run 3A-9-01REQUIRED BEFORE A SUBSEQUENT START ATTEMPT
FLIGHT2.22.0Checklist
Pilatus PC-12MSFS 2024 · Emergency Procedures · 8procedures · 55 steps
Rejected Takeoff (not engine related)7 steps
| 01 | PCLIDLE | |
| 02 | BrakingAS REQUIRED | |
| 03 | ReverseAS REQUIRED | |
| 04 | Engine switch (if cannot stop on remaining runway)OFF | |
| 05 | FUEL EMERG shut offPRESS LATCH DOWN AND PULL LEVER UP | |
| 06 | MASTER POWER switchEMERG OFF | |
| 07 | AircraftEVACUATE AFTER STOPPING |
Engine Failure Before Rotation6 steps
| 01 | PCLIDLE | |
| 02 | BrakingAS REQUIRED | |
| 03 | Engine switch (if overrun or collision likely)OFF | |
| 04 | FUEL EMERG shut offPRESS LATCH DOWN AND PULL LEVER UP | |
| 05 | MASTER POWER switchEMERGENCY OFF | |
| 06 | AircraftEVACUATE AFTER STOPPING |
Engine Failure After Rotation - Gear Down8 steps
| 01 | Aircraft - LAND STRAIGHT AHEAD, MAX 30 DEG BANK TO AVOID OBSTRUCTIONS | |
| 02 | Flaps40 DEG | |
| 03 | Final approach speed at 10,450 lb88 KIAS, NOT BELOW DYNAMIC SPEED BUG | |
| 04 | PCLIDLE | |
| 05 | Engine switchOFF | |
| 06 | FUEL EMERG shut offPRESS LATCH DOWN AND PULL LEVER UP | |
| 07 | MASTER POWER switch after touchdownEMERGENCY OFF | |
| 08 | AircraftEVACUATE AFTER STOPPING |
Engine Failure After Rotation - Gear Up7 steps
| 01 | Landing gearDOWN IF LANDING SITE ALLOWS, OTHERWISE KEEP UP | |
| 02 | Flaps40 DEG | |
| 03 | Final approach speed at 10,450 lb - 88 KIAS FLAPS 40, 91 KIAS FLAPS 30, 101 KIAS FLAPS 15 | |
| 04 | PCLIDLE | |
| 05 | Engine switchOFF | |
| 06 | FUEL EMERG shut offPRESS LATCH DOWN AND PULL LEVER UP | |
| 07 | MASTER POWER switch after touchdownEMERGENCY OFF |
Engine Failure in Flight - Total Power Loss8 steps
| 01 | AutopilotUSE FLC AT BEST GLIDE AND HDG OR NAV MODE | |
| 02 | Best glide (propeller feathered)119 KIAS AT 10,450 LB, 110 KIAS AT 9,040 LB | |
| 03 | PCLIDLE | |
| 04 | AircraftPROCEED TO NEAREST AIRFIELD AVOIDING HIGH TERRAIN | |
| 05 | Remaining fuelCHECK | |
| 06 | Air Start - CARRY OUT IF NO MECHANICAL DAMAGE SUSPECTED AND TIME PERMITS | |
| 07 | Emergency DescentMAKE IF CABIN ALTITUDE ABOVE 10,000 FT | |
| 08 | Forced LandingMAKE IF NO AIR START |
Engine Surging6 steps
| 01 | PCLREDUCE TO MINIMUM TO SUSTAIN FLIGHT | |
| 02 | ACS Bleed Air switchOFF FOR 5 SECONDS, RESET TO ON | |
| 03 | Electrical HEAT/COOL switchINHIBIT | |
| 04 | PCL - IDLE AND DESCEND TO DENSER AIR, IF REQUIRED TO 15,000 FT | |
| 05 | ACS Bleed Air switchOFF | |
| 06 | Aircraft - LAND AS SOON AS POSSIBLE, RETAINING GLIDE CAPABILITY TO THE SELECTED AIRFIELD |
Balked Landing (Go-Around)8 steps
| 01 | Go Around switch (if autopilot engaged)PRESS | |
| 02 | POWER CONTROL LEVERSET TO T/O | |
| 03 | Climb airspeed85 KIAS | |
| 04 | FlapsSET 15 DEG (MAX 165 KIAS) | |
| 05 | Climb airspeed pusher normal mode95 KIAS | |
| 06 | Climb airspeed pusher ice mode105 KIAS | |
| 07 | Landing Gear SelectorUP WITH POSITIVE RATE OF CLIMB | |
| 08 | Yaw DamperON |
Aborted Start (EPECS)5 steps
| 01 | Engine switchOFF TO ABORT THE START OR DRY MOTORING RUN | |
| 02 | EPECS - AUTOMATICALLY ABORTS ON ITT EXCEEDANCE, HUNG START, NO LIGHT-OFF OR STARTER PUSH | |
| 03 | Dry motor run30 SECONDS COMMANDED AUTOMATICALLY | |
| 04 | STARTER annunciatorGREEN IN PFD ENGINE WINDOW | |
| 05 | Dry Motoring Run 3A-9-01REQUIRED BEFORE A SUBSEQUENT START ATTEMPT |