TM 1-1520-238-10
7A-35
M01-251
180
110
150
130
140
100
160
170
120
1300
1100
90
120
180
150
130
140
100
170
160
110
900
700
1100
900
700
170
110
150
140
160
120
130
90
100
1300
100
60
40
80
10
20
30
50
60
70
30
70
80
60
50
40
20
30
90
40
80
50
TOTAL FUEL FLOW – LB/HOUR
30
70
80
90
70
30
50
60
40
80
90
70
0
100
20
60
50
40
TOTAL FUEL FLOW – LB/HOUR
PRESSURE ALTITUDE - 4000 FEET
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
CRUISE
AIRSPEED
INDICATED
KNOTS
10
0
20
D
F = 10.0 SQ FT
D
Q – %
10
0
20
D
F = 10.0 SQ FT
D
Q – %
FAT=+30C
FAT=+40C
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
~
%
Figure 7A-11.
Cruise Chart, 4,000 Feet, +30 C and +40 C (Sheet 5 of 6)
