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DCS WORLD · Rotary
Mi-8MTV2 Magnificent Eight Emergency Procedures
Immediate Action Procedures
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6 procedures
- 1Affected engine fuel cockCLOSE immediately
- 2Affected engineSHUT DOWN
- 3Remain engineMAXIMUM POWER
- 4Fire extinguisherDISCHARGE if fitted
- 5AirspeedMAINTAIN ETL for single engine flight
- 6Land immediately at nearest suitable area
- 1CollectiveLOWER immediately to maintain NR
- 2AutorotationESTABLISH (NR 95%)
- 3MaydayDECLARE position and intentions
- 4Select landing areaINTO WIND preferred
- 5Airspeed120-130 km/h for best glide
- 6FlareBEGIN 50-75 m AGL to reduce sink rate
- 7CollectiveINCREASE at 2-3 m AGL for cushioned landing
- 1CollectiveREDUCE to decrease torque
- 2Enter autorotation if rotation uncontrolled
- 3If controllablereduce speed and land immediately
- 4Head into wind for landing
- 5Skids-on at minimum speed
- 6Shut down immediately after touchdown
- 1Hydraulic pressureCHECK gauge
- 2ControlsEXPECT significantly increased forces
- 3SpeedREDUCE to improve control effectiveness
- 4Avoid abrupt inputs
- 5Land as soon as practicalfull-length landing area
- 6CrewASSIST with dual controls if two pilot
- 1CollectiveREDUCE immediately
- 2TorqueCHECK below maximum limit
- 3Land as soon as practical
- 4Record duration and peak torque for maintenance
- 5If sustained overtorqueland immediately, do not continue flight
- 1MAYDAYDECLARE position and intentions
- 2Select landing areaclear and level preferred
- 3Head into wind for landing
- 4Airspeed120 km/h approach
- 5At 50-75 m AGLBEGIN flare
- 6At 2-3 m AGLINCREASE collective for cushioned touchdown
- 7Shut down immediately after landing
FLIGHT2.22.0Checklist
Mi-8MTV2 Magnificent EightDCS WORLD · Emergency Procedures · 6procedures · 37 steps
Engine Fire6 steps
| 01 | Affected engine fuel cockCLOSE immediately | |
| 02 | Affected engineSHUT DOWN | |
| 03 | Remain engineMAXIMUM POWER | |
| 04 | Fire extinguisherDISCHARGE if fitted | |
| 05 | AirspeedMAINTAIN ETL for single engine flight | |
| 06 | Land immediately at nearest suitable area |
Engine Failure / Autorotation7 steps
| 01 | CollectiveLOWER immediately to maintain NR | |
| 02 | AutorotationESTABLISH (NR 95%) | |
| 03 | MaydayDECLARE position and intentions | |
| 04 | Select landing areaINTO WIND preferred | |
| 05 | Airspeed120-130 km/h for best glide | |
| 06 | FlareBEGIN 50-75 m AGL to reduce sink rate | |
| 07 | CollectiveINCREASE at 2-3 m AGL for cushioned landing |
Tail Rotor Failure6 steps
| 01 | CollectiveREDUCE to decrease torque | |
| 02 | Enter autorotation if rotation uncontrolled | |
| 03 | If controllablereduce speed and land immediately | |
| 04 | Head into wind for landing | |
| 05 | Skids-on at minimum speed | |
| 06 | Shut down immediately after touchdown |
Hydraulic Failure6 steps
| 01 | Hydraulic pressureCHECK gauge | |
| 02 | ControlsEXPECT significantly increased forces | |
| 03 | SpeedREDUCE to improve control effectiveness | |
| 04 | Avoid abrupt inputs | |
| 05 | Land as soon as practicalfull-length landing area | |
| 06 | CrewASSIST with dual controls if two pilot |
Overtorque5 steps
| 01 | CollectiveREDUCE immediately | |
| 02 | TorqueCHECK below maximum limit | |
| 03 | Land as soon as practical | |
| 04 | Record duration and peak torque for maintenance | |
| 05 | If sustained overtorqueland immediately, do not continue flight |
Forced Landing7 steps
| 01 | MAYDAYDECLARE position and intentions | |
| 02 | Select landing areaclear and level preferred | |
| 03 | Head into wind for landing | |
| 04 | Airspeed120 km/h approach | |
| 05 | At 50-75 m AGLBEGIN flare | |
| 06 | At 2-3 m AGLINCREASE collective for cushioned touchdown | |
| 07 | Shut down immediately after landing |