TM 1-1520-238-10
7A-50
M01-266
170
180
160
100
140
130
150
110
120
80
90
110
150
140
120
130
80
90
70
100
160
80
110
100
140
120
130
90
150
180
170
800
1400
1000
800
600
1000
1200
1400
1200
170
160
600
40
60
50
100
60
60
30
50
TOTAL FUEL FLOW – LB/HOUR
70
30
TOTAL FUEL FLOW – LB/HOUR
90
80
40
60
50
100
30
PRESSURE ALTITUDE - 10,000 FEET
10
20
70
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
0
CRUISE
40
20
40
50
60
40
50
20
80
70
30
90
70
30
FAT=+20C
FAT=+10C
AIRSPEED
INDICATED
KNOTS
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
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
OR
R/C
MAX
END
MAX
OR
R/C
MAX
END
AH–64A
CRUISE
T700–GE–701C
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-14.
Cruise Chart, 10,000 Feet, +10 C and +20 C (Sheet 4 of 5)
