Eec Non Critical Fault - MD Helicopters MD900 Flight Manual

Set power of the affected engine as desired.
F
Continue flight and monitor engine indications on the IIDS primary display.
F
There is no N
CAUTION
N and power must be controlled by the pilot using a combination
R
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
F
Advise maintenance
F
Indications: EGT indication blanks
Conditions: In flight
Procedures:
Continue flight
F
Advise maintenance
F
Conditions: On ground prior to starting
Procedures:
Do not attempt start, or abort start.
F
Advise maintenance
F
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
governing following EEC failures on both engines.
R
FAA Approved
Reissue 2
Original
CSP−902RFM207E−1
Emergency and
Malfunction Procedures
3−9