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MSFS 2024 · General Aviation
Beechcraft Bonanza G36 Emergency Procedures
Immediate Action Procedures
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12 procedures
- 1Airspeed - 85 KTS MINIMUM immediately after takeoff, 110 KTS with sufficient altitude
- 2If engine failure occurs immediately after takeoff, landing straight ahead is usually advisable
- 3Turn toward the most favorable landing site
- 4Air Conditioner (if installed)OFF
- 5Fuel Selector Valve - SELECT OTHER TANK (feel for detent, check visually)
- 6MagnetosCHECK BOTH SELECTED
- 7Aux Fuel PumpHI
- 8MixtureFULL RICH, THEN LEAN AS REQUIRED
- 9If engine does not start: Aux Fuel Pump OFF, Mixture FULL RICH, Magnetos check L/R/BOTH, Alternate Air T-Handle PULL AND RELEASE
- 10If engine still does not start, go to MAXIMUM GLIDE CONFIGURATION
- 1ThrottleCLOSED
- 2BrakingAS REQUIRED TO ACHIEVE STOPPING DISTANCE
- 3If the airplane cannot be stopped on the remaining runway: Mixture - CUT OFF
- 4Ground LoopIF REQUIRED
- 5When stopped: Fuel Selector ValveOFF
- 6Battery 1 and 2, Alternator 1 and 2 - OFF; Magnetos - OFF
- 7Evacuate the airplane and move to a safe distance
- 1Firewall Air Control Knob - PULL TO CLOSE (red knob, outboard left lower subpanel)
- 2Fuel Selector ValveOFF
- 3MixtureCUT OFF
- 4PropellerLOW RPM
- 5Fuel Boost PumpOFF
- 6Magnetos - OFF; Alternator 1 and 2 - OFF
- 7EngineDO NOT ATTEMPT TO RESTART
- 8Then use EMERGENCY DESCENT, MAXIMUM GLIDE CONFIGURATION and LANDING WITHOUT POWER as required
- 1Landing GearUP
- 2FlapsUP
- 3PropellerLOW RPM
- 4Cowl FlapsCLOSED
- 5Airspeed110 KTS
- 6Air Conditioner (if installed) - OFF; Alternator 1 and 2 - OFF; ELT - ON
- 7Glide Ratio1.7 NM / 1,000 FEET
- 8Nearest Airport - DETERMINE (PFD NRST softkey, select airport, Direct-To, ENT twice)
- 9The landing gear will not retract unless the throttle is at approximately 17 in Hg manifold pressure or above
- 1Fuel Selector ValveOFF
- 2MixtureCUT OFF
- 3MagnetosOFF
- 4FlapsDOWN
- 5Landing GearDOWN or UP depending on terrain
- 6Airspeed85 KIAS MINIMUM
- 7Alternator 1 and 2OFF
- 8When landing is assured and the PFD is not required: Battery 1 and 2 - OFF
- 1If possible choose firm sod; make a normal approach using flaps as necessary
- 2When landing is assured: ThrottleCLOSED
- 3MixtureCUT OFF
- 4Alternator 1 and 2OFF
- 5MagnetosOFF
- 6Fuel Selector ValveOFF
- 7Maintain wings level during landing
- 8Battery 1 and 2 (after landing)OFF, then evacuate and move to a safe distance
- 1Airspeed - 154 KTS OR LESS (lower speeds facilitate manual extension)
- 2LANDING GEAR MOTOR Circuit BreakerPULL (left circuit breaker panel)
- 3Landing Gear HandleDOWN
- 4Handcrank Handle CoverREMOVE (at rear of front seat)
- 5Handcrank - ENGAGE AND TURN CCW AS FAR AS POSSIBLE (approximately 50 turns)
- 6Verify GEAR DN and LOCKED lights illuminated and warning horn silent at idle
- 7Handcrank - DISENGAGE, THEN STOW; Landing Gear Handle - DO NOT MOVE
- 8LANDING GEAR MOTOR Circuit BreakerDO NOT RESET
- 9Consider the gear UNLOCKED until the airplane is on jacks and the system has been cycled and checked
- 1Battery 1 and Alternator 1OFF
- 2Firewall Air Control - PULL (if smoke or fire is present in the engine compartment)
- 3Autopilot and Flight DirectorDISENGAGE
- 4Avionics Switch and all electrical equipment switchesOFF
- 5To dissipate smoke: Firewall Air Control FULL FORWARD (if engine is not the source), wing root and overhead fresh air outlets OPEN
- 6If smoke subsidesLAND AS SOON AS PRACTICAL
- 7If smoke persists: maintain control on standby instruments, Battery 2 and Alternator 2 - OFF, land as soon as practical
- 8Dissipation of smoke is not sufficient evidence the fire is out
- 1PowerIDLE
- 2PropellerHIGH RPM
- 3Landing Gear (154 kts maximum)DOWN
- 4Flaps (154 kts maximum)APPROACH
- 5Airspeed154 KIAS
- 1Intentional spins are prohibited. Act IMMEDIATELYthe longer the delay the harder recovery becomes
- 2Steps 1 through 3 AGGRESSIVELY and SIMULTANEOUSLY:
- 3Control ColumnFULL FORWARD, AILERONS NEUTRAL
- 4Full RudderOPPOSITE THE DIRECTION OF SPIN
- 5ThrottleIDLE
- 6RudderNEUTRALIZE WHEN ROTATION STOPS
- 7Execute a smooth pullout
- 1ThrottleRETARD
- 2AirspeedREDUCE UNTIL RPM IS AT OR BELOW 2,700
- 3Oil PressureCHECK
- 4If loss of oil pressure caused the overspeed, the engine will seize after a short period
- 5Land as soon as practical
- 6If the engine seizes, use MAXIMUM GLIDE CONFIGURATION and LANDING WITHOUT POWER
- 1MixtureCUT OFF
- 2StarterCONTINUE TO CRANK
- 3Fuel Selector ValveOFF
- 4MagnetosOFF
- 5Battery 1 and 2, Alternator 1 and 2OFF
- 6Evacuate the airplane and move to a safe distance
FLIGHT2.22.0Checklist
Beechcraft Bonanza G36MSFS 2024 · Emergency Procedures · 12procedures · 91 steps
Engine Failure In Flight10 steps
| 01 | Airspeed - 85 KTS MINIMUM immediately after takeoff, 110 KTS with sufficient altitude | |
| 02 | If engine failure occurs immediately after takeoff, landing straight ahead is usually advisable | |
| 03 | Turn toward the most favorable landing site | |
| 04 | Air Conditioner (if installed)OFF | |
| 05 | Fuel Selector Valve - SELECT OTHER TANK (feel for detent, check visually) | |
| 06 | MagnetosCHECK BOTH SELECTED | |
| 07 | Aux Fuel PumpHI | |
| 08 | MixtureFULL RICH, THEN LEAN AS REQUIRED | |
| 09 | If engine does not start: Aux Fuel Pump OFF, Mixture FULL RICH, Magnetos check L/R/BOTH, Alternate Air T-Handle PULL AND RELEASE | |
| 10 | If engine still does not start, go to MAXIMUM GLIDE CONFIGURATION |
Engine Failure During Take-Off Ground Roll / Aborted Takeoff7 steps
| 01 | ThrottleCLOSED | |
| 02 | BrakingAS REQUIRED TO ACHIEVE STOPPING DISTANCE | |
| 03 | If the airplane cannot be stopped on the remaining runway: Mixture - CUT OFF | |
| 04 | Ground LoopIF REQUIRED | |
| 05 | When stopped: Fuel Selector ValveOFF | |
| 06 | Battery 1 and 2, Alternator 1 and 2 - OFF; Magnetos - OFF | |
| 07 | Evacuate the airplane and move to a safe distance |
Engine Fire In Flight8 steps
| 01 | Firewall Air Control Knob - PULL TO CLOSE (red knob, outboard left lower subpanel) | |
| 02 | Fuel Selector ValveOFF | |
| 03 | MixtureCUT OFF | |
| 04 | PropellerLOW RPM | |
| 05 | Fuel Boost PumpOFF | |
| 06 | Magnetos - OFF; Alternator 1 and 2 - OFF | |
| 07 | EngineDO NOT ATTEMPT TO RESTART | |
| 08 | Then use EMERGENCY DESCENT, MAXIMUM GLIDE CONFIGURATION and LANDING WITHOUT POWER as required |
Maximum Glide Configuration9 steps
| 01 | Landing GearUP | |
| 02 | FlapsUP | |
| 03 | PropellerLOW RPM | |
| 04 | Cowl FlapsCLOSED | |
| 05 | Airspeed110 KTS | |
| 06 | Air Conditioner (if installed) - OFF; Alternator 1 and 2 - OFF; ELT - ON | |
| 07 | Glide Ratio1.7 NM / 1,000 FEET | |
| 08 | Nearest Airport - DETERMINE (PFD NRST softkey, select airport, Direct-To, ENT twice) | |
| 09 | The landing gear will not retract unless the throttle is at approximately 17 in Hg manifold pressure or above |
Landing Without Power8 steps
| 01 | Fuel Selector ValveOFF | |
| 02 | MixtureCUT OFF | |
| 03 | MagnetosOFF | |
| 04 | FlapsDOWN | |
| 05 | Landing GearDOWN or UP depending on terrain | |
| 06 | Airspeed85 KIAS MINIMUM | |
| 07 | Alternator 1 and 2OFF | |
| 08 | When landing is assured and the PFD is not required: Battery 1 and 2 - OFF |
Landing With Gear Retracted - With Power8 steps
| 01 | If possible choose firm sod; make a normal approach using flaps as necessary | |
| 02 | When landing is assured: ThrottleCLOSED | |
| 03 | MixtureCUT OFF | |
| 04 | Alternator 1 and 2OFF | |
| 05 | MagnetosOFF | |
| 06 | Fuel Selector ValveOFF | |
| 07 | Maintain wings level during landing | |
| 08 | Battery 1 and 2 (after landing)OFF, then evacuate and move to a safe distance |
Landing Gear Manual Extension9 steps
| 01 | Airspeed - 154 KTS OR LESS (lower speeds facilitate manual extension) | |
| 02 | LANDING GEAR MOTOR Circuit BreakerPULL (left circuit breaker panel) | |
| 03 | Landing Gear HandleDOWN | |
| 04 | Handcrank Handle CoverREMOVE (at rear of front seat) | |
| 05 | Handcrank - ENGAGE AND TURN CCW AS FAR AS POSSIBLE (approximately 50 turns) | |
| 06 | Verify GEAR DN and LOCKED lights illuminated and warning horn silent at idle | |
| 07 | Handcrank - DISENGAGE, THEN STOW; Landing Gear Handle - DO NOT MOVE | |
| 08 | LANDING GEAR MOTOR Circuit BreakerDO NOT RESET | |
| 09 | Consider the gear UNLOCKED until the airplane is on jacks and the system has been cycled and checked |
Electrical Smoke or Fire8 steps
| 01 | Battery 1 and Alternator 1OFF | |
| 02 | Firewall Air Control - PULL (if smoke or fire is present in the engine compartment) | |
| 03 | Autopilot and Flight DirectorDISENGAGE | |
| 04 | Avionics Switch and all electrical equipment switchesOFF | |
| 05 | To dissipate smoke: Firewall Air Control FULL FORWARD (if engine is not the source), wing root and overhead fresh air outlets OPEN | |
| 06 | If smoke subsidesLAND AS SOON AS PRACTICAL | |
| 07 | If smoke persists: maintain control on standby instruments, Battery 2 and Alternator 2 - OFF, land as soon as practical | |
| 08 | Dissipation of smoke is not sufficient evidence the fire is out |
Emergency Descent5 steps
| 01 | PowerIDLE | |
| 02 | PropellerHIGH RPM | |
| 03 | Landing Gear (154 kts maximum)DOWN | |
| 04 | Flaps (154 kts maximum)APPROACH | |
| 05 | Airspeed154 KIAS |
Inadvertent Spin7 steps
| 01 | Intentional spins are prohibited. Act IMMEDIATELYthe longer the delay the harder recovery becomes | |
| 02 | Steps 1 through 3 AGGRESSIVELY and SIMULTANEOUSLY: | |
| 03 | Control ColumnFULL FORWARD, AILERONS NEUTRAL | |
| 04 | Full RudderOPPOSITE THE DIRECTION OF SPIN | |
| 05 | ThrottleIDLE | |
| 06 | RudderNEUTRALIZE WHEN ROTATION STOPS | |
| 07 | Execute a smooth pullout |
Propeller Overspeed6 steps
| 01 | ThrottleRETARD | |
| 02 | AirspeedREDUCE UNTIL RPM IS AT OR BELOW 2,700 | |
| 03 | Oil PressureCHECK | |
| 04 | If loss of oil pressure caused the overspeed, the engine will seize after a short period | |
| 05 | Land as soon as practical | |
| 06 | If the engine seizes, use MAXIMUM GLIDE CONFIGURATION and LANDING WITHOUT POWER |
Engine Fire On The Ground6 steps
| 01 | MixtureCUT OFF | |
| 02 | StarterCONTINUE TO CRANK | |
| 03 | Fuel Selector ValveOFF | |
| 04 | MagnetosOFF | |
| 05 | Battery 1 and 2, Alternator 1 and 2OFF | |
| 06 | Evacuate the airplane and move to a safe distance |