TM 1-1520-238-10
7A-21
90
100
110
80
60
50
70
30
20
40
10
20
30
50
60
100
70
90
80
40
110
70
90
80
40
60
50
100
30
70
90
80
40
60
50
100
30
30
100
80
90
110
60
70
50
40
20
1000
130
120
160
140
150
170
700
160
1100
900
150
800
1300
160
1400
1200
150
140
120
130
140
130
120
M01-237
PRESSURE ALTITUDE - SEA LEVEL
TOTAL FUEL FLOW – LB/HOUR
FAT=–10C
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
FAT=0C
TOTAL FUEL FLOW – LB/HOUR
CRUISE
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
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
AH–64A
CRUISE
T700–GE–701C
MAX
RANGE
MAX
RANGE
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
0
Figure 7A-9.
Cruise Chart, Sea Level, –10 C and 0 C (Sheet 3 of 6)
