TM 1-1520-238-10
7A-27
M01-243
100
30
100
50
60
40
80
90
70
30
100
50
60
40
80
90
70
140
120
100
90
70
20
30
50
60
150
110
160
170
140
160
150
170
130
90
110
70
30
20
130
80
60
50
110
0
10
20
30
100
TOTAL FUEL FLOW – LB/HOUR
1300
PRESSURE ALTITUDE - 2000 FEET
40
150
70
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
90
140
160
700
170
CRUISE
1100
120
1300
60
50
130
120
1100
TOTAL FUEL FLOW – LB/HOUR
900
700
80
900
40
80
40
FAT=–10C
FAT=0C
DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
AIRSPEED
INDICATED
KNOTS
AH–64A
CRUISE
T700–GE–701C
MAX
RANGE
MAX
RANGE
DATA BASIS:
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
10
0
20
D
F = 10.0 SQ FT
D
Q – %
10
0
20
D
F = 10.0 SQ FT
D
Q – %
Figure 7A-10.
Cruise Chart, 2,000 Feet, –10 C and 0 C (Sheet 3 of 6)
