TM 1-1520-238-10
7A-41
M01-257
1100
700
900
1100
700
1300
900
1300
180
170
90
130
160
150
140
120
110
100
80
60
100
70
90
80
130
120
160
140
150
110
170
180
140
100
170
160
150
130
120
110
90
TOTAL FUEL FLOW – LB/HOUR
70
30
60
40
20
50
40
50
TOTAL FUEL FLOW – LB/HOUR
PRESSURE ALTITUDE - 6000 FEET
20
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
10
80
90
70
30
100
50
60
40
80
90
70
50
60
0
40
80
CRUISE
20
30
50
60
70
40
30
100
30
AH–64A
CRUISE
T700–GE–701C
FAT=+40C
FAT=+30C
AIRSPEED
INDICATED
KNOTS
MAX
RANGE
MAX
RANGE
MAX
OR
R/C
MAX
END
MAX
OR
R/C
MAX
END
10
0
20
D
F = 10.0 SQ FT
D
Q – %
10
0
20
D
F = 10.0 SQ FT
D
Q – %
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-12.
Cruise Chart, 6,000 Feet, +30 C and +40 C (Sheet 5 of 5)
