TM 1-1520-238-10
7A-47
M01-263
170
160
150
30
40
50
60
70
80
90
100
130
110
0
10
20
140
800
1200
1000
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
180
600
140
170
160
150
120
130
70
110
100
90
80
40
30
60
50
20
120
1400
1200
100
90
80
70
60
50
110
100
90
600
CRUISE
800
1000
70
TOTAL FUEL FLOW – LB/HOUR
130
140
120
30
20
80
40
40
30
60
60
50
TOTAL FUEL FLOW – LB/HOUR
150
100
70
170
160
180
30
PRESSURE ALTITUDE - 10,000 FEET
80
50
90
40
AIRSPEED
INDICATED
KNOTS
10
0
20
D
F = 10.0 SQ FT
D
Q – %
MAX
RANGE
MAX
RANGE
FAT=–50C
FAT=–40C
MAX END
OR
MAX R/C
AH–64A
CRUISE
T700–GE–701C
MAX END
OR
MAX R/C
1400
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
VNE
VNE
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-14.
Cruise Chart, 10,000 Feet, –50 C and –40 C (Sheet 1 of 5)
