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DCS WORLD · Rotary
Mi-24P Hind Emergency Procedures
Immediate Action Procedures
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6 procedures
- 1Affected engine fuel cockCLOSE immediately
- 2Fire extinguisherDISCHARGE
- 3Remaining engineMAXIMUM POWER
- 4AirspeedMAINTAIN ETL single engine
- 5Declare emergency
- 6Land immediately at nearest suitable area
- 1CollectiveLOWER immediately to maintain NR
- 2AutorotationESTABLISH
- 3MAYDAYDECLARE
- 4Select landing area into wind
- 5Airspeed150 km/h in descent
- 6FlareBEGIN 75 m AGL
- 7CollectiveINCREASE at 3-4 m for cushioned landing
- 1CollectiveREDUCE to reduce torque reaction
- 2AutorotationENTER if spin uncontrolled
- 3SpeedINCREASE above ETL (reduces pedal requirement)
- 4Running landing if controllable
- 5Avoid hovertail rotor authority insufficient
- 6Land immediately with forward speed maintained
- 1Control forcesEXPECT greatly increased
- 2SpeedREDUCE and avoid abrupt inputs
- 3Avoid hover if possible
- 4Running landing preferred
- 5Land as soon as practical
- 1CollectiveREDUCE immediately
- 2TorqueMONITOR both engines
- 3Duration and peakNOTE for maintenance
- 4Land as soon as practical if sustained
- 5Post-flight inspection required before next flight
- 1MAYDAYDECLARE
- 2Select landing areaavoid obstacles
- 3Head into wind
- 4Approach speed120-150 km/h
- 5Flare at 50-75 m AGL
- 6Cushion touchdown with collective at 2-4 m AGL
- 7Shut down after landing
FLIGHT2.22.0Checklist
Mi-24P HindDCS WORLD · Emergency Procedures · 6procedures · 36 steps
Engine Fire6 steps
| 01 | Affected engine fuel cockCLOSE immediately | |
| 02 | Fire extinguisherDISCHARGE | |
| 03 | Remaining engineMAXIMUM POWER | |
| 04 | AirspeedMAINTAIN ETL single engine | |
| 05 | Declare emergency | |
| 06 | Land immediately at nearest suitable area |
Engine Failure / Autorotation7 steps
| 01 | CollectiveLOWER immediately to maintain NR | |
| 02 | AutorotationESTABLISH | |
| 03 | MAYDAYDECLARE | |
| 04 | Select landing area into wind | |
| 05 | Airspeed150 km/h in descent | |
| 06 | FlareBEGIN 75 m AGL | |
| 07 | CollectiveINCREASE at 3-4 m for cushioned landing |
Tail Rotor Failure6 steps
| 01 | CollectiveREDUCE to reduce torque reaction | |
| 02 | AutorotationENTER if spin uncontrolled | |
| 03 | SpeedINCREASE above ETL (reduces pedal requirement) | |
| 04 | Running landing if controllable | |
| 05 | Avoid hovertail rotor authority insufficient | |
| 06 | Land immediately with forward speed maintained |
Hydraulic Failure5 steps
| 01 | Control forcesEXPECT greatly increased | |
| 02 | SpeedREDUCE and avoid abrupt inputs | |
| 03 | Avoid hover if possible | |
| 04 | Running landing preferred | |
| 05 | Land as soon as practical |
Overtorque5 steps
| 01 | CollectiveREDUCE immediately | |
| 02 | TorqueMONITOR both engines | |
| 03 | Duration and peakNOTE for maintenance | |
| 04 | Land as soon as practical if sustained | |
| 05 | Post-flight inspection required before next flight |
Forced Landing7 steps
| 01 | MAYDAYDECLARE | |
| 02 | Select landing areaavoid obstacles | |
| 03 | Head into wind | |
| 04 | Approach speed120-150 km/h | |
| 05 | Flare at 50-75 m AGL | |
| 06 | Cushion touchdown with collective at 2-4 m AGL | |
| 07 | Shut down after landing |