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Dornier Do 228-100 (Carenado) Emergency Procedures
Immediate Action Procedures
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6 procedures
- 1Aeroplane controlMAINTAIN
- 2POWER leversMAX
- 3LDG GEARUP (once airborne)
- 4AirspeedV2
- 5Faulty engineSHUTOFF and FEATHER
- 6FLAPS (clear of obstacle)UP at 100 KIAS or above
- 7Airspeed - VYSE (108 KIAS at MTOW, less 1 kt per 200 kg below)
- 1TakeoffABORT. Below V1 the takeoff must be rejected
- 2POWER leversTOWARDS GI, beta lights on, then towards REVERSE
- 3BrakesAPPLY AS NECESSARY
- 4Directional controlMAINTAIN with rudder and nose wheel steering
- 5ENG SPEED leversLOW at taxi speed
- 6At or above V1 the takeoff can be continued safely; abort only if enough runway remains to stop
- 1Failed engineIDENTIFY (dead foot, dead engine)
- 2Failed POWER leverGI
- 3Failed ENG SPEED lever - LIFT above the LOW gate and PULL AFT to shut off fuel
- 4Failed ENG SPEED leverPUSH INBOARD into the feather gate
- 5PropellerCONFIRM FEATHERED (76 deg blade angle)
- 6Live engineMAX CONTINUOUS POWER, ITT 923 deg C max
- 7AirspeedVYSE 108 KIAS, never below VMC 81 KIAS flaps up
- 8Negative torque sensing reduces the drag on its own but does NOT feather the propeller - the pilot must
- 1Affected POWER leverGI
- 2Affected ENG SPEED leverFUEL SHUTOFF, then FEATHER
- 3Affected FIRE COCKCLOSED
- 4Affected fire leverPULL
- 5Fire extinguisherDISCHARGE to the affected engine
- 6Affected boost pump and GENOFF
- 7Live enginePOWER as required, rudder trim for asymmetry
- 8Land as soon as possible
- 1START selector - AIR (it is set to AIR in the Before Take Off check)
- 2Affected boost pumpON, FUEL PRESS light out
- 3Affected ENG SPEED leverOUT of the feather gate, to LOW
- 4AirspeedWITHIN the airstart envelope
- 5StarterSTART
- 6ENRICHAS REQUIRED
- 7ITTMONITOR. Start limit is 1,149 deg C for 1 second
- 8GENON at 25 percent RPM or above
- 1AirspeedVYSE 108 KIAS until established on final
- 2Live engine ENG SPEED leverHIGH
- 3SYNCHROPHASEROFF
- 4FLAPS2 (20 deg), 130 KIAS maximum
- 5LDG GEARDN, check 3 green. 160 KIAS maximum
- 6AirspeedVREF, never below VMC
- 7FLAPS DN (30 deg)DELAY until the landing is assured
- 8Plan for no go-around. Single engine climb rate is marginal with flaps and gear out
FLIGHT2.23.0Checklist
Dornier Do 228-100 (Carenado)MSFS 2024 · Emergency Procedures · 6procedures · 45 steps
Engine Malfunction - At or After V17 steps
| 01 | Aeroplane controlMAINTAIN | |
| 02 | POWER leversMAX | |
| 03 | LDG GEARUP (once airborne) | |
| 04 | AirspeedV2 | |
| 05 | Faulty engineSHUTOFF and FEATHER | |
| 06 | FLAPS (clear of obstacle)UP at 100 KIAS or above | |
| 07 | Airspeed - VYSE (108 KIAS at MTOW, less 1 kt per 200 kg below) |
Engine Malfunction - Before V1 (Rejected Takeoff)6 steps
| 01 | TakeoffABORT. Below V1 the takeoff must be rejected | |
| 02 | POWER leversTOWARDS GI, beta lights on, then towards REVERSE | |
| 03 | BrakesAPPLY AS NECESSARY | |
| 04 | Directional controlMAINTAIN with rudder and nose wheel steering | |
| 05 | ENG SPEED leversLOW at taxi speed | |
| 06 | At or above V1 the takeoff can be continued safely; abort only if enough runway remains to stop |
Engine Failure - In Flight (Shutdown and Feather)8 steps
| 01 | Failed engineIDENTIFY (dead foot, dead engine) | |
| 02 | Failed POWER leverGI | |
| 03 | Failed ENG SPEED lever - LIFT above the LOW gate and PULL AFT to shut off fuel | |
| 04 | Failed ENG SPEED leverPUSH INBOARD into the feather gate | |
| 05 | PropellerCONFIRM FEATHERED (76 deg blade angle) | |
| 06 | Live engineMAX CONTINUOUS POWER, ITT 923 deg C max | |
| 07 | AirspeedVYSE 108 KIAS, never below VMC 81 KIAS flaps up | |
| 08 | Negative torque sensing reduces the drag on its own but does NOT feather the propeller - the pilot must |
Engine Fire8 steps
| 01 | Affected POWER leverGI | |
| 02 | Affected ENG SPEED leverFUEL SHUTOFF, then FEATHER | |
| 03 | Affected FIRE COCKCLOSED | |
| 04 | Affected fire leverPULL | |
| 05 | Fire extinguisherDISCHARGE to the affected engine | |
| 06 | Affected boost pump and GENOFF | |
| 07 | Live enginePOWER as required, rudder trim for asymmetry | |
| 08 | Land as soon as possible |
Engine Restart - In Flight8 steps
| 01 | START selector - AIR (it is set to AIR in the Before Take Off check) | |
| 02 | Affected boost pumpON, FUEL PRESS light out | |
| 03 | Affected ENG SPEED leverOUT of the feather gate, to LOW | |
| 04 | AirspeedWITHIN the airstart envelope | |
| 05 | StarterSTART | |
| 06 | ENRICHAS REQUIRED | |
| 07 | ITTMONITOR. Start limit is 1,149 deg C for 1 second | |
| 08 | GENON at 25 percent RPM or above |
Single Engine Approach and Landing8 steps
| 01 | AirspeedVYSE 108 KIAS until established on final | |
| 02 | Live engine ENG SPEED leverHIGH | |
| 03 | SYNCHROPHASEROFF | |
| 04 | FLAPS2 (20 deg), 130 KIAS maximum | |
| 05 | LDG GEARDN, check 3 green. 160 KIAS maximum | |
| 06 | AirspeedVREF, never below VMC | |
| 07 | FLAPS DN (30 deg)DELAY until the landing is assured | |
| 08 | Plan for no go-around. Single engine climb rate is marginal with flaps and gear out |