TM 1-1520-238-10
7A-64
M01-280
600
120
30
100
50
60
40
80
90
70
30
100
50
60
40
80
90
70
170
30
130
120
110
90
60
40
50
70
80
150
140
160
170
150
140
180
160
110
130
90
60
50
40
30
100
80
70
110
0
10
20
30
100
TOTAL FUEL FLOW – LB/HOUR
1200
40
150
70
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
90
140
160
170
CRUISE
800
1000
1200
60
50
130
120
800
TOTAL FUEL FLOW – LB/HOUR
1000
80
PRESSURE ALTITUDE - 16,000 FEET
180
100
20
600
20
FAT=–10C
FAT=0C
10
D
F = 10.0 SQ FT
D
Q – %
0
20
10
0
20
D
F = 10.0 SQ FT
D
Q – %
MAX
RANGE
MAX
RANGE
MAX
OR
R/C
MAX
END
MAX
OR
R/C
MAX
END
AH–64A
CRUISE
T700–GE–701C
AIRSPEED
INDICATED
KNOTS
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-17.
Cruise Chart, 16,000 Feet, –10 C and 0 C (Sheet 3 of 4)
