Optional Equipment
Supplemental Fuel System
CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Original
10
−
32
AUXILIARY TANK FILLER NECK
MAIN FUEL TANK (REF.)
FUEL VENT LINE
FUEL LEVEL CONTROL VALVE
FUEL TRANSFER LINE
AUXILIARY FUEL TANK
FUEL TRANSFER LINE
FUEL QUANTITY TRANSMITTER
FUEL VENT ROLL OVER VALVE
GRAVITY FILL PORT
AFT RH VENT LINE
FLAME ARRESTOR
AFT VENT FAIRING
AUX FUEL PORT
VENT ROLLOVER VALVE
CABIN FLOOR (REF)
MAIN FUEL TANK
(REF)
LEVEL CONTROL VALVE
STA 230.5 BULKHEAD
CHECK VALVE
FUEL TRANSFER LINE
BAGGAGE COMPARTMENT FLOOR
(REF.)
VENT/ROLLOVER VALVE
CHECK VALVE
AUXILIARY FUEL TANK
FUEL QUANTITY XMITTER FLOAT
TRANSFER PUMP
FUEL TANK DRAIN PLUG
FUEL TRANSFER LINE
FUEL TRANSFER LINE
VENT LINE
(AUXILIARY FUEL TANK ROTATED 90
°
CW FOR CLARITY)
SUPPLEMENTAL FUEL SYSTEM SCHEMATIC
SUPPLEMENTAL FUEL SYSTEM INSTALLATION
F92
−
175b
NEW CHECK VALVE
(IF INSTALLED)
Figure 10
−
13. Supplemental Fuel System
Summary of Contents for MD900 Explorer
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