CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Emergency and
Malfunction Procedures
FAA Approved
Reissue 2
Original
3
−
34
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
ÇÇÇ
ÉÉÉ
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
WARNING
TICK MARK (RED)
(LEFT SHOWN,
(RIGHT OPPOSITE)
LOW FUEL CAUTION
SEGMENT
(YELLOW)
FUEL QUANTITY
SEGMENTS
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)
f92
−
027
Figure 3
−
7. Fuel System Advisory Indicators
Summary of Contents for MD900 Explorer
Page 4: ......