CSP
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902RFM207E
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1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Optional Equipment
Airframe Fuel FIlter
FAA Approved
Reissue 2
Original
10
−
56
PART III
EMERGENCY AND MALFUNCTION PROCEDURES
FUEL FILTER CLOGGED
Indications:
Yellow
FILTER
FUEL
L
R
caution indicator ON.
Conditions:
Left, right, or both airframe fuel filter(s) in impending bypass condition.
Procedures:
With both fuel boost pumps operational.
Continue the flight in progress.
Service the airframe filter prior to next flight.
Procedures:
With single fuel boost pump failure.
Continue the flight in progress.
Leave operating fuel boost pump ON.
If flight is continued into low fuel conditions (less than 300 pounds
remaining), the engine with the failed boost pump will experience
an early flame out due to a loss of the fuel transfer system (Ref.
Land as soon as practical if fuel level falls below 300 pounds.
Procedures:
With dual fuel boost pump failure.
Land as soon as possible.
FUEL BOOST PUMP FAILURE
Procedures:
Leave operating fuel boost pump ON.
If flight is continued into low fuel conditions (less than 300 pounds
remaining), the engine with the failed boost pump will experience
an early flame out due to a loss of the fuel transfer system (Ref.
Continue the flight in progress.
Land as soon as practical if fuel level falls below 300 pounds.
CAUTION
CAUTION
Summary of Contents for MD900 Explorer
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