TM 1-1520-238-10
7A-25
M01-241
70
90
80
40
60
50
100
70
90
80
40
60
50
100
30
60
100
90
70
40
80
50
30
20
10
20
30
50
60
100
70
0
90
80
40
110
30
150
130
140
100
110
120
90
60
30
80
70
50
40
20
900
130
120
160
140
150
170
700
1300
160
900
1100
1300
1100
700
130
150
140
120
110
PRESSURE ALTITUDE - 2000 FEET
TOTAL FUEL FLOW – LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
TOTAL FUEL FLOW – LB/HOUR
CRUISE
FAT=–50C
FAT=–40C
AIRSPEED
INDICATED
KNOTS
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
AH–64A
CRUISE
T700–GE–701C
MAX
RANGE
MAX
RANGE
DATA BASIS:
VNE
VNE
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-10.
Cruise Chart, 2,000 Feet, –50 C and –40 C (Sheet 1 of 6)
