TM 1-1520-238-10
7A-44
M01-260
700
170
900
1300
1100
1200
1000
1400
600
800
90
180
150
160
140
130
170
100
110
80
120
100
90
80
130
120
160
140
150
110
150
160
180
170
130
120
110
100
140
TOTAL FUEL FLOW – LB/HOUR
90
30
50
TOTAL FUEL FLOW – LB/HOUR
PRESSURE ALTITUDE - 8000 FEET
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
20
80
70
90
70
30
100
50
60
40
80
90
10
60
20
30
40
CRUISE
50
70
50
70
20
60
30
40
40
60
70
0
30
40
80
100
50
60
AH–64A
CRUISE
T700–GE–701C
FAT=–10C
FAT=0C
10
0
20
D
F = 10.0 SQ FT
D
Q – %
10
0
20
D
F = 10.0 SQ FT
D
Q – %
MAX
RANGE
AIRSPEED
INDICATED
KNOTS
MAX
RANGE
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-13.
Cruise Chart, 8,000 Feet, –10 C and 0 C (Sheet 3 of 5)
