In cruise flight, after detecting an engine failure, or after the IP announces “Simulated Engine 1 out,” what are the first flight control inputs made by the pilot?
Adjust the collective and cyclic as necessary to maintain single engine TQ and rotor RPM within limits
Following a single engine failure (continued flight possible), what airspeed must be maintained until 30 feet above touchdown?
At or above VSSE
What conditions must be met before conducting Slope Operations?
- Helicopter cleared
- A/C FLT page displayed on one MPD in both crew stations
- Before landing checks complete
- P* properly fitted w/ a boresighted HDU
How will the manually-controlled engine be set, relative to the good engine, following a EDECU Lockout?
Place the the malfunctioning engine in lockout and set TRQ 5 % below the good engine, plus or minus 5 %
How may a real-world engine failure be presented to the crew?
- Rapid drop in Ng, Np, Torque, TGT, Oil pressure and the symbolic torque value on the MPD/ HMD displays flashing
- Engine failure voice annunciation
- Engine (1 or 2) out Mstr Warning Flashing
- Autopage to ENG page
What conditions will cause en ENG 1 OUT voice message to annunciate?
- Engines running and ENG 1 Ng < 63 % (Throttle not in OFF)
or - ENG 1 Np < 93 % (Throttle in Fly, Torque < 24 %)
