CSP
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902RFM207E
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1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Systems Description
Original
7
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32
Reissue 2
FUEL METERING UNIT (FMU)
SHROUD BOX (2 PL)
ENGINE DECK
FUEL SHUTOFF
VALVE (2 PL)
FUEL PRESSURE
SWITCH (2 PL)
RH FUEL FEED
VAPOR SHROUD
TEE FITTING (2 PL)
RH FUEL FEED SYS
TO FWD RH
VENT SYS
FUEL FILLER
ASSY
FLAME
ARRESTOR (2 PL)
VENT OVBD
DRAIN (2 PL)
SUMP DRAIN CABLE
SPRING LOADED
FLAPPER VALVE
FUEL BOOST
PUMP (2 PL)
SUMP OVBD
DRAIN (2 PL)
FUEL QTY PROBE
(2 PL) LEFT AND RIGHT
SUMP DRAIN
VALVE (2 PL)
FUEL CELL
LOW FUEL LEVEL
SENSOR (2 PL)
CENTER BAFFLE
CENTER BAFFLE
FUEL BOOST
PUMP (2 PL)
FEED LINE TO R ENGINE
FEED LINE TO L ENGINE
”T” FITTING (2 PL)
R FUEL XFER TUBING
L FUEL XFER TUBING
EJECTOR PUMP (2 PL)
CHECK VALVE (2 PL)
FUEL TRANSFER SYSTEM
FUEL CELL OUTLET
VAPOR SHROUD
FWD LH
VENT SYS
LH FUEL FEED
VAPOR SHROUD
LH FUEL
FEED SYS
FUEL FEED
FRANGIBLE
CONNECTOR (2 PL)
ENGINE DECK FRANGIBLE
CONNECTOR (2 PL)
TEE FITTING VAPOR
SHROUD DRAIN (2 PL) TO
ENGINE DRAIN SYSTEM
VENT-ROLLOVER
VALVE (4 PL)
TO AFT LH
VENT SYS
LEFT
ENGINE
RIGHT
ENGINE
LOOKING DOWN
GRAVITY FILL VALVE
AND FLAPPER VALVE
F92
−
073
Figure 7
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17. Fuel System Schematic
Summary of Contents for MD900 Explorer
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