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Lakota EPs
| Question | Answer |
|---|---|
| Single Engine Failure | ORALS OEI establish rotor trim to max Affected eng id Land as soon as practicable single engine shutdown perform |
| Overspeed | CVNATL collective raise var nr check man n2 trim- trim to max if not possible Affected eng, ID Twist grip rotate to idle and match q and FLI Land as soon as practicable |
| Underspeed | OBVANTS Oei establish bleed air consumers off var nr check man affected eng id N2 trim switch try to trim max and match q twist grip raise stop rotate to fly and match q and fli sing |
| loss of tail rotor effectiveness | CASSALAAA Collective reduce to maintain min side slip airspeed increase to 80 knts of higher suitable landing area select Shallow approach with nose left perform airspeed recuce to align nose to runway direction landing perform |