TM 1-1520-238-10
7A-32
M01-248
70
90
80
40
60
50
130
50
160
140
150
170
700
900
1100
1300
700
900
1100
1300
170
160
150
130
140
120
110
110
160
120
150
170
130
140
TOTAL FUEL FLOW – LB/HOUR
TOTAL FUEL FLOW – LB/HOUR
PRESSURE ALTITUDE - 4000 FEET
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
CRUISE
30
40
20
20
110
60
70
80
100
90
40
30
90
70
100
60
50
30
10
80
80
100
90
70
40
20
60
50
30
0
120
100
50
60
40
80
90
70
30
100
FAT=-30C
FAT=-20C
10
0
20
D
F = 10.0 SQ FT
D
Q – %
10
0
20
D
F = 10.0 SQ FT
D
Q – %
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
~
%
Figure 7A-11.
Cruise Chart, 4,000 Feet, –30 C and –20 C (Sheet 2 of 6)
