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Beechcraft King Air 350i Emergency Procedures
Immediate Action Procedures
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10 procedures
- 1Condition Lever (affected)FUEL CUTOFF
- 2Prop Lever (affected)FEATHER
- 3Firewall Fuel ValveCLOSE
- 4Fire Extinguisher (if fire warning persists)ACTUATE
- 5GeneratorOFF
- 6Engine Auto IgnitionOFF
- 7AutofeatherOFF
- 8Brake Deice (if installed)OFF
- 9Electrical LoadMONITOR
- 10Bank 3 to 5 degrees into the operating engine while maintaining a constant heading
- 1Condition Lever (affected)FUEL CUTOFF
- 2Firewall Fuel ValveCLOSE
- 3Starter SwitchSTARTER ONLY
- 4Fire Extinguisher (if fire warning persists)ACTUATE
- 1Condition LeversFUEL CUTOFF
- 2Prop LeversFEATHER
- 3Firewall Fuel ValvesCLOSE
- 4Master Switch (gang bar)OFF
- 5Battery BusEMERG OFF
- 6SFDS PowerOFF
- 1Power LeversGROUND FINE
- 2Brakes - MAXIMUM OR AS REQUIRED TO ACHIEVE STOPPING DISTANCE
- 3Reverse thrustDO NOT USE WITH ONE ENGINE INOPERATIVE
- 4Single-engine ground fineUSE WITH CARE ON SURFACES WITH REDUCED TRACTION
- 1VR - ROTATE TO APPROXIMATELY 10 DEG PITCH ATTITUDE
- 2Landing Gear (positive climb established)UP
- 3AirspeedMAINTAIN V2 TO 400 FT AGL
- 4Propeller (inoperative engine)VERIFY FEATHERED
- 5Flaps (at 400 ft AGL minimum)UP AT V2 PLUS 9
- 6AirspeedINCREASE TO 125 KNOTS
- 7Inoperative engine cleanup at 1,500 ft AGL - CONDITION LEVER FUEL CUTOFF, PROP FEATHER, FIREWALL FUEL VALVE CLOSE, GENERATOR OFF
- 8AutofeatherOFF
- 1PowerREDUCE AS REQUIRED TO MAINTAIN CONTROL
- 2NoseLOWER TO ACCELERATE ABOVE VMCA
- 3PowerAS REQUIRED
- 4EngineSECURE PER ENGINE FIRE OR FAILURE IN FLIGHT
- 1Oil PressureCONFIRM BELOW 60 PSI
- 2Engine (if confirmed)SECURE PER ENGINE FIRE OR FAILURE IN FLIGHT
- 3Or land at the nearest suitable airport using the minimum power required to sustain flight
- 1Power LeversIDLE
- 2Prop LeversFULL FORWARD
- 3Flaps (202 knots maximum)APPROACH
- 4Landing Gear (184 knots maximum)DOWN
- 5Airspeed184 KNOTS MAXIMUM
- 1Oxygen MasksDON
- 2Mask Selector SwitchEMERG
- 3Mic SwitchesOXY
- 4Instrument Emergency Lights (if required)ON
- 5GeneratorsOFF
- 6ECS ModeMAN HEAT
- 7Cockpit DoorOPEN
- 8Avionics Master (if smoke persists)OFF, USE SFDS FOR AIRPLANE CONTROL
- 9Master Switch (gang bar)OFF
- 10Land - NEAREST SUITABLE AIRPORT, PLAN A FLAPS-UP LANDING AND LOWER GEAR MANUALLY
- 1Standby Pump (failed side)ON
- 2L Fuel Press or R Fuel Press CAS messageCONFIRM REMOVED
- 3Oil Temperature and Pressure Indicators (failed side)MONITOR
FLIGHT2.23.0Checklist
Beechcraft King Air 350iMSFS 2024 · Emergency Procedures · 10procedures · 57 steps
Engine Fire or Failure In Flight10 steps
| 01 | Condition Lever (affected)FUEL CUTOFF | |
| 02 | Prop Lever (affected)FEATHER | |
| 03 | Firewall Fuel ValveCLOSE | |
| 04 | Fire Extinguisher (if fire warning persists)ACTUATE | |
| 05 | GeneratorOFF | |
| 06 | Engine Auto IgnitionOFF | |
| 07 | AutofeatherOFF | |
| 08 | Brake Deice (if installed)OFF | |
| 09 | Electrical LoadMONITOR | |
| 10 | Bank 3 to 5 degrees into the operating engine while maintaining a constant heading |
Engine Fire On Ground4 steps
| 01 | Condition Lever (affected)FUEL CUTOFF | |
| 02 | Firewall Fuel ValveCLOSE | |
| 03 | Starter SwitchSTARTER ONLY | |
| 04 | Fire Extinguisher (if fire warning persists)ACTUATE |
Emergency Engine Shutdown On The Ground6 steps
| 01 | Condition LeversFUEL CUTOFF | |
| 02 | Prop LeversFEATHER | |
| 03 | Firewall Fuel ValvesCLOSE | |
| 04 | Master Switch (gang bar)OFF | |
| 05 | Battery BusEMERG OFF | |
| 06 | SFDS PowerOFF |
Engine Failure During Takeoff At Or Below V1 - Takeoff Aborted4 steps
| 01 | Power LeversGROUND FINE | |
| 02 | Brakes - MAXIMUM OR AS REQUIRED TO ACHIEVE STOPPING DISTANCE | |
| 03 | Reverse thrustDO NOT USE WITH ONE ENGINE INOPERATIVE | |
| 04 | Single-engine ground fineUSE WITH CARE ON SURFACES WITH REDUCED TRACTION |
Engine Failure During Takeoff At Or Above V1 - Takeoff Continued8 steps
| 01 | VR - ROTATE TO APPROXIMATELY 10 DEG PITCH ATTITUDE | |
| 02 | Landing Gear (positive climb established)UP | |
| 03 | AirspeedMAINTAIN V2 TO 400 FT AGL | |
| 04 | Propeller (inoperative engine)VERIFY FEATHERED | |
| 05 | Flaps (at 400 ft AGL minimum)UP AT V2 PLUS 9 | |
| 06 | AirspeedINCREASE TO 125 KNOTS | |
| 07 | Inoperative engine cleanup at 1,500 ft AGL - CONDITION LEVER FUEL CUTOFF, PROP FEATHER, FIREWALL FUEL VALVE CLOSE, GENERATOR OFF | |
| 08 | AutofeatherOFF |
Engine Failure In Flight Below Vmca4 steps
| 01 | PowerREDUCE AS REQUIRED TO MAINTAIN CONTROL | |
| 02 | NoseLOWER TO ACCELERATE ABOVE VMCA | |
| 03 | PowerAS REQUIRED | |
| 04 | EngineSECURE PER ENGINE FIRE OR FAILURE IN FLIGHT |
Oil Pressure Low3 steps
| 01 | Oil PressureCONFIRM BELOW 60 PSI | |
| 02 | Engine (if confirmed)SECURE PER ENGINE FIRE OR FAILURE IN FLIGHT | |
| 03 | Or land at the nearest suitable airport using the minimum power required to sustain flight |
Emergency Descent5 steps
| 01 | Power LeversIDLE | |
| 02 | Prop LeversFULL FORWARD | |
| 03 | Flaps (202 knots maximum)APPROACH | |
| 04 | Landing Gear (184 knots maximum)DOWN | |
| 05 | Airspeed184 KNOTS MAXIMUM |
Electrical Smoke Or Fire10 steps
| 01 | Oxygen MasksDON | |
| 02 | Mask Selector SwitchEMERG | |
| 03 | Mic SwitchesOXY | |
| 04 | Instrument Emergency Lights (if required)ON | |
| 05 | GeneratorsOFF | |
| 06 | ECS ModeMAN HEAT | |
| 07 | Cockpit DoorOPEN | |
| 08 | Avionics Master (if smoke persists)OFF, USE SFDS FOR AIRPLANE CONTROL | |
| 09 | Master Switch (gang bar)OFF | |
| 10 | Land - NEAREST SUITABLE AIRPORT, PLAN A FLAPS-UP LANDING AND LOWER GEAR MANUALLY |
Fuel Pressure Low3 steps
| 01 | Standby Pump (failed side)ON | |
| 02 | L Fuel Press or R Fuel Press CAS messageCONFIRM REMOVED | |
| 03 | Oil Temperature and Pressure Indicators (failed side)MONITOR |