CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Optional Equipment
Airframe Fuel FIlter
FAA Approved
Reissue 2
Original
10
−
57
PART IV
NORMAL PROCEDURES
Preflight
:
Power switch
BAT/EXT
Left and right boost pumps
ON
Attempting to drain the fuel filter with boost pumps off will cause
air to enter the fuel system.
Filter unit, drain valve, and associated lines
CHECK FOR LEAKS
Filter unit drain valve
PRESS TO DRAIN
NOTE
:
If the aircraft has been exposed to freezing temperatures, failure of the drain may
be due to ice formation in the filter element.
Press-to-test button
PRESS
AIRFRAME FILTER caution lights
ON
Left and right boost pumps
OFF
Power switch
OFF
Post Flight
:
When ambient temperature is expected to go below freezing, any water in the filter
unit should be drained following completion of flight.
Following the completion of the flight in progress after illumination of the FUEL
FILTER caution light, service the filter prior to the next flight.
CAUTION
Summary of Contents for MD900 Explorer
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