Engine Emergencies; Single Engine Failure - MD Helicopters MD900 Flight Manual

3−3.

ENGINE EMERGENCIES

The ENG OUT warning annunciator is located between the TORQUE and EGT
vertical displays. When the IIDS senses an engine failure, the ENG OUT
TORQUE
ENG
OUT

SINGLE ENGINE FAILURE

Indications: ENG OUT annunciator illuminated and low rotor tone on for one cycle.
Affected engine torque, N
Conditions: At a hover - IGE:
Procedures:
F
Land
Conditions: At a hover - OGE:
Procedures:
F
Collective pitch
NOTE
: The decision to land or fly−away, following a single engine failure, will depend
on ambient conditions and aircraft gross weight. Refer to Section V for best rate
of climb speed, single engine rate of climb and descent, and height velocity
envelope performance data.
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
warning flashes and the low rotor RPM tone is activated
EGT
for one cycle. The EGT and TORQUE displays also re-
scale. The ENG OUT advisory is disabled with aircraft
on the ground.
and N
P
FAA Approved
Reissue 2
Original
decreasing to zero.
G
ADJUST TO MAINTAIN OEI LIMITS
CSP−902RFM207E−1
Emergency and
Malfunction Procedures
3−3