TM 1-1520-238-10
7A-23
M01-239
110
100
90
80
70
60
120
40
30
20
50
70
90
80
40
60
50
100
30
70
90
80
40
60
50
100
30
90
20
30
40
50
60
70
80
110
100
130
120
150
800
1000
1200
1400
1200
1000
800
180
1400
170
160
150
140
130
170
160
140
PRESSURE ALTITUDE - SEA LEVEL
TOTAL FUEL FLOW – LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
TOTAL FUEL FLOW – LB/HOUR
CRUISE
FAT=+40C
FAT=+30C
10
0
20
D
F = 10.0 SQ FT
D
Q – %
10
0
20
D
F = 10.0 SQ FT
D
Q – %
AIRSPEED
INDICATED
KNOTS
DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
10
20
30
50
60
100
70
0
90
80
130
40
120
110
160
140
150
170
AH–64A
CRUISE
T700–GE–701C
DATA BASIS:
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
MAX
RANGE
MAX
RANGE
Figure 7A-9.
Cruise Chart, Sea Level, +30 C and +40 C (Sheet 5 of 6)
