MD Helicopters MD900 with PW206E, Flight Manual

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CSP–900RFM206E–1
Emergency and
Malfunction Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
3–31
3–13.FUEL SYSTEM DISPLAY ADVISORIES
CAB HEAT
BAT HOT
BAT WRM
ROTOR
BRAKE
CABIN
DOOR
BAGGAGE
DOOR
1 HYD 2
IIDS
FIRE
CHIPS
%LOAD
FUEL
GEN
LB
OAT
°
C
%PSI
°
C
FIRE
CHIPS
FIRE
CHIPS
NG
%PSI
°
C %PSI
°
C
%LOAD
NG
GEN
ÇÇÇÇ ÉÉÉÉ
FUEL
LB
ÇÇ
YELLOW
WHITE
B. NORMAL FUEL FLOW WITH IMPENDING ENGINE FUEL FILTERS BY−PASS
E. INDICATES BOTH FUEL SHUTOFF VALVES IN CLOSED POSITION (NOTE 1)
FUEL FILTER
IMPENDING
BY−PASS CAUTION
(YELLOW)
FUEL FILTER
IMPENDING BY−PASS
CAUTION
FUEL SHUTOFF
VALVE (YELLOW)
(NOTE 1)
FUEL SHUTOFF
VALVE (YELLOW)
(NOTE 1)
ÉÉ ÂÂ
ÂÂ
C. INDICATES LOW FUEL PRESSURE ON BOTH FUEL BOOST PUMPS
OR BOTH BOOSTER PUMPS IN OFF POSITION
RED
GREEN
LOW FUEL CAUTION
SEGMENT
(YELLOW)
FUEL QUANTITY DIGITAL
DISPLAY (WHITE)
D. LOW FUEL PRESSURE LEFT BOOST PUMP WITH NORMAL FUEL
PRESSURE ON RIGHT BOOSTER PUMP
A. NORMAL FUEL PRESSURE
NOTE:
1. THE LIGHT SEGMENT BAR(S) WILL FLASH ON THE IIDS PANEL WHEN
THE VALVE IS IN TRANSIT BETWEEN THE OPEN AND CLOSED POSITION.
LOW FUEL WARNING
SEGMENT (RED)
F92E–027
LOW FUEL
WARNING
TICK MARK
(RED)
FUEL QUANTITY
SEGMENTS
Figure 3–7. Fuel System Advisory Indicators