CSP
−
902RFM207E
−
1
Emergency and
Malfunction Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Original
3
−
9
Set power of the affected engine as desired.
Continue flight and monitor engine indications on the IIDS primary display.
There is no N
R
governing following EEC failures on both engines.
N
R
and power must be controlled by the pilot using a combination
of collective and twistgrips.
EEC NONCRITICAL FAULT
An EEC caution annunciator ON in flight may result in one of the following indica
tions.
Indications:
Engine torque matching may be degraded.
Conditions:
During flight
Procedures:
Continue flight
Advise maintenance
Indications:
EGT indication blanks
Conditions:
In flight
Procedures:
Continue flight
Advise maintenance
Conditions:
On ground prior to starting
Procedures:
Do not attempt start, or abort start.
Advise maintenance
CAUTION
Summary of Contents for MD900 Explorer
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