TM 1-1520-238-10
7A-62
M01-278
PRESSURE ALTITUDE - 16,000 FEET
100
30
100
50
60
40
80
90
70
30
100
50
60
40
80
90
70
150
20
90
120
110
100
80
50
30
40
60
70
160
130
140
170
180
130
110
120
80
50
40
30
20
90
70
60
110
0
10
20
30
100
TOTAL FUEL FLOW – LB/HOUR
1000
40
150
70
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
90
140
160
1200
170
CRUISE
600
800
1000
1200
60
50
130
120
800
TOTAL FUEL FLOW – LB/HOUR
80
600
140
180
160
170
150
FAT=–50C
FAT=–40C
10
D
F = 10.0 SQ FT
D
Q – %
0
20
MAX
RANGE
MAX
RANGE
MAX
OR
R/C
MAX
END
MAX
OR
R/C
MAX
END
AIRSPEED
INDICATED
KNOTS
AH–64A
CRUISE
T700–GE–701C
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-17.
Cruise Chart, 16,000 Feet, –50 C and –40 C (Sheet 1 of 4)
