CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Handling Servicing
and Maintenance
Original
8
−
40
Reissue 2
ÉÉÉÉ
ÉÉÉÉ
ÉÉÉÉ
ÉÉÉÉ
ÉÉÉÉ
ÉÉÉÉ
ÉÉÉÉ
0
20
40
60
80
120
SEC
MIN
1
2
AREA A - RECORD IN ENGINE LOG BOOK (2.5 MINUTE RATING)
AREA B - RECORD IN ENGINE LOG BOOK (CONTINUOUS RATING)
AREA C - RETURN ENGINE FOR OVERHAUL
TIME (MINUTES AND SECONDS)
GAS GENERA
TOR
SPEED
−
%N
G
100
140
2.5
100.0
ÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇÇÇÇ
AREA C
103.0
F927
−
055
98.2
160
180
200
220
240
260
280
300
3
4
5
104.1
AREA B
AREA A
97.2
NO ACTION REQUIRED
99.8
TAKE-OFF
(5 MINUTES)
Figure 8
−
26. Compressor Turbine (N
G
) Speed Vs Time
ÑÑ
ÑÑ
ÑÑ
5
MIN
ÑÑÑ
ÑÑÑ
ÑÑÑ
2.5
MIN
ÓÓ
ÓÓ
ÓÓ
ÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇ
ÇÇÇÇÇÇÇ
ÉÉÉÉ
ÉÉÉÉ
ÉÉÉÉ
f927
−
056A
AREA C
AREA A
AREA B
0
20
30
60
90
120
150
180
210
240
270
300
330
(SEC)
1
2
2.5
3
4
5
(MIN)
100%
88.4%
116.7
112.7%
AREA A
DETERMINE CAUSE AND RECORD IN ENGINE LOG BOOK
AREA B
RETURN ENGINE FOR OVERHAUL
AREA C
RECORD IN ENGINE LOG BOOK EXCEPT OEI CONDITION
TIME (MINUTES AND SECONDS)
TORQUE
IIDS (XMSN)
ENGINE
NOTE:
THE TORQUE DISPLAYED ON
THE IIDS PRIMARY DISPLAY
IS TRANSMISSION TORQUE.
110%
124%
135%
145%
OEI
AEO
100%
MCP
MCP
10
SEC
140%
Figure 8
−
27. Engine Overtorque Limits
−
All Conditions
Summary of Contents for MD900 Explorer
Page 4: ......
