MD Helicopters MD900 with PW206E, Flight Manual

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CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
Emergency and
Malfunction Procedures
FAA Approved
Original
3–10
F
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 NON CRITICAL 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:
F
Continue flight
F
Advise maintenance
Indications: EGT indication blanks
Conditions: In flight
Procedures:
F
Continue flight
F
Advise maintenance
Conditions:
On ground prior to starting
Procedures:
F
Do not attempt start, or abort start.
F
Advise maintenance
CAUTION