TM 1-1520-238-10
7A-55
M01-271
90
30
100
50
60
40
80
90
70
30
100
50
60
40
80
90
70
150
80
110
90
70
20
30
50
60
150
120
130
160
170
140
160
110
170
130
100
120
80
40
30
20
60
50
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
1400
170
CRUISE
800
1000
1200
1400
60
50
130
120
800
TOTAL FUEL FLOW – LB/HOUR
1000
70
80
600
PRESSURE ALTITUDE - 12,000 FEET
100
180
140
180
40
600
FAT=+10C
FAT=+20C
10
0
20
D
F = 10.0 SQ FT
D
Q – %
10
0
20
D
F = 10.0 SQ FT
D
Q – %
MAX
RANGE
MAX
RANGE
MAX END
OR
MAX R/C
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-15.
Cruise Chart, 12,000 Feet, +10 C and +20 C (Sheet 4 of 5)
