Secondary Iids Display; Engine Display - MD Helicopters MD900 Flight Manual

CSP−902RFM207E−1
Limitations
LEFT ENGINE PARAMETER
DISPLAY
ENGINE OIL
TEMPERATURE DISPLAY
TRANSMISSION OIL
TEMPERATURE DISPLAY
GAS PRODUCER
TURBINE SPEED DISPLAY
HIGH WARNING: >125°C
HIGH CAUTION: >120°C
LOW CAUTION: <10°C WITH N
<-45°C WITH N
CAUTION: 100% LOAD
HIGH WARNING: >103.0% N
HIGH CAUTION: >99.8% N
LOW WARNING: <50% N
2−14
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)

SECONDARY IIDS DISPLAY

TRANSMISSION OIL
TRANSMISSION PARAMETER
PRESSURE DISPLAY
FIRE FIRE
CHIPS CHIPS
° C ° C
%PSI %PSI
FUEL
%LOAD
GEN
NG
LB
FUEL QUANTITY
Figure 2−11. Secondary IIDS Display
FIRE
CHIPS
° C
%PSI
>50%
G
< 50%
G
%LOAD
GEN
G
G
NG
G
Figure 2−12. Engine Display
FAA Approved
Reissue 2
Revision 4
RIGHT ENGINE PARAMETER
DISPLAY
CAB HEAT
FIRE
CHIPS BAT HOT
BAT WRM
° C
ROTOR
%PSI
BRAKE
CABIN
DOOR
BAGGAGE
%LOAD
DOOR
GEN
1 HYD 2
IIDS
NG
OAT ° C
>100% PSI
<80% PSI
<80% PSI
NOTE: ``>'' = GREATER THAN
``<'' = LESS THAN
``<'' = EQUAL TO OR LESS THAN
DISPLAY
ENGINE OIL
PRESSURE DISPLAY
GENERATOR
%LOAD DISPLAY
F92−016
TIME
>5 MINUTES
TIME
>2 SEC
>5 SEC
F927−052