CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Limitations
FAA Approved
Reissue 2
Revision 4
2
−
14
SECONDARY IIDS DISPLAY
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
LEFT ENGINE PARAMETER
DISPLAY
TRANSMISSION PARAMETER
DISPLAY
RIGHT ENGINE PARAMETER
DISPLAY
FUEL QUANTITY
ENGINE OIL
ENGINE OIL
PRESSURE DISPLAY
GENERATOR
%LOAD DISPLAY
GAS PRODUCER
TURBINE SPEED DISPLAY
TEMPERATURE DISPLAY
PRESSURE DISPLAY
TRANSMISSION OIL
TRANSMISSION OIL
TEMPERATURE DISPLAY
F92
−
016
Figure 2
−
11. Secondary IIDS Display
FIRE
CHIPS
%LOAD
GEN
%PSI
°
C
NG
HIGH WARNING: >125
°
C
HIGH CAUTION: >120
°
C
<80% PSI
>2 SEC
<80% PSI
>5 SEC
CAUTION: 100% LOAD
HIGH WARNING: >103.0% N
G
HIGH CAUTION: >99.8% N
G
LOW WARNING: <50% N
G
F927
−
052
LOW CAUTION: <10
°
C WITH N
G
>50%
<-45
°
C WITH N
G
< 50%
>100% PSI
>5 MINUTES
TIME
TIME
NOTE:
``>'' = GREATER THAN
``<'' = LESS THAN
``<'' = EQUAL TO OR LESS THAN
Figure 2
−
12. Engine Display
Summary of Contents for MD900 Explorer
Page 4: ......
