MD Helicopters MD900 with PW206E, Flight Manual

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CSP–900RFM206E–1
Limitations
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
2–11
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 2–10. Secondary IIDS Display
FIRE
CHIPS
%LOAD
GEN
%PSI
°
C
NG
HIGH WARNING: 110 ° C
HIGH CAUTION: 105 ° C
<80% PSI >2 SEC
<80% PSI >5 SEC
CAUTION: 100% LOAD
HIGH WARNING: 102.4% N
G
HIGH CAUTION: 98.7% N
G
LOW WARNING: 50% N
G
F92–017
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 2–11. Engine Display