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DCS WORLD · Rotary
SA342 Gazelle Emergency Procedures
Immediate Action Procedures
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6 procedures
- 1ThrottleCLOSE immediately
- 2Fuel cockCLOSE
- 3Fire extinguisherDISCHARGE if fitted
- 4AutorotationENTER immediately
- 5MAYDAYDECLARE
- 6Select landing area and execute forced landing
- 1CollectiveLOWER immediately to maintain NR
- 2AutorotationESTABLISH
- 3MAYDAYDECLARE position
- 4Select landing areainto wind preferred
- 5Airspeed100-120 km/h for best autorotation
- 6FlareBEGIN 30-50 m AGL
- 7CollectiveINCREASE at 2 m AGL to cushion landing
- 1CollectiveREDUCE to decrease torque reaction
- 2SpeedINCREASE above 100 km/h (reduces pedal load)
- 3Avoid hoverfenestron authority insufficient without engine
- 4Running landing into wind
- 5Power off landing preferred if pitch control available
- 6Land immediately
- 1Control forcesEXPECT increased
- 2Avoid abrupt inputs
- 3SpeedREDUCE to 100 km/h
- 4Land at nearest suitable area
- 5Running landing preferred over hover
- 1CollectiveREDUCE immediately
- 2NG - CHECK within limits
- 3Land as soon as practical
- 4Note duration and peak for maintenance
- 5Inspect rotor head before next flight
- 1MAYDAYDECLARE
- 2Select landing areaclear of obstacles
- 3Head into wind
- 4Airspeed100-120 km/h on approach
- 5Flare at 30-50 m AGL
- 6Cushion with collective at 2 m AGL
- 7Skids level on touchdown
FLIGHT2.22.0Checklist
SA342 GazelleDCS WORLD · Emergency Procedures · 6procedures · 36 steps
Engine Fire6 steps
| 01 | ThrottleCLOSE immediately | |
| 02 | Fuel cockCLOSE | |
| 03 | Fire extinguisherDISCHARGE if fitted | |
| 04 | AutorotationENTER immediately | |
| 05 | MAYDAYDECLARE | |
| 06 | Select landing area and execute forced landing |
Engine Failure / Autorotation7 steps
| 01 | CollectiveLOWER immediately to maintain NR | |
| 02 | AutorotationESTABLISH | |
| 03 | MAYDAYDECLARE position | |
| 04 | Select landing areainto wind preferred | |
| 05 | Airspeed100-120 km/h for best autorotation | |
| 06 | FlareBEGIN 30-50 m AGL | |
| 07 | CollectiveINCREASE at 2 m AGL to cushion landing |
Tail Rotor Failure6 steps
| 01 | CollectiveREDUCE to decrease torque reaction | |
| 02 | SpeedINCREASE above 100 km/h (reduces pedal load) | |
| 03 | Avoid hoverfenestron authority insufficient without engine | |
| 04 | Running landing into wind | |
| 05 | Power off landing preferred if pitch control available | |
| 06 | Land immediately |
Hydraulic Failure5 steps
| 01 | Control forcesEXPECT increased | |
| 02 | Avoid abrupt inputs | |
| 03 | SpeedREDUCE to 100 km/h | |
| 04 | Land at nearest suitable area | |
| 05 | Running landing preferred over hover |
Overtorque5 steps
| 01 | CollectiveREDUCE immediately | |
| 02 | NG - CHECK within limits | |
| 03 | Land as soon as practical | |
| 04 | Note duration and peak for maintenance | |
| 05 | Inspect rotor head before next flight |
Forced Landing7 steps
| 01 | MAYDAYDECLARE | |
| 02 | Select landing areaclear of obstacles | |
| 03 | Head into wind | |
| 04 | Airspeed100-120 km/h on approach | |
| 05 | Flare at 30-50 m AGL | |
| 06 | Cushion with collective at 2 m AGL | |
| 07 | Skids level on touchdown |