MD Helicopters MD900 with PW206E, Руководство по эксплуатации самолета

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CSP–900RFM206E–1
Emergency and
Malfunction Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
3–3
3–3. ENGINE EMERGENCIES
ENG
OUT
TORQUE
EGT
The ENG OUT warning annunciator is located between the TORQUE and EGT
vertical displays. When the IIDS senses an engine failure, the ENG OUT
warning flashes and the low rotor RPM tone is activated
for one cycle. The EGT and TORQUE displays also re−
scale. The ENG OUT advisory is disabled with aircraft
on the ground.
SINGLE ENGINE FAILURE
Indications: ENG OUT annunciator illuminated and low rotor tone on for one cycle.
Affected engine torque, N
P
and N
G
decreasing to zero.
Conditions:
At a hover − IGE:
Procedures:
F
Land
Conditions:
At a hover − OGE:
Procedures:
F
Collective pitch ADJUST TO MAINTAIN OEI LIMITS
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.