TM 1-1520-238-10
7A-59
M01-275
180
170
100
150
140
160
120
30
130
80
90
70
110
60
50
40
20
30
100
50
60
40
80
90
70
100
50
60
40
80
90
30
180
150
20
30
70
40
10
170
150
140
160
1400
600
1000
800
800
1000
1200
1400
1200
600
TOTAL FUEL FLOW LB/HOUR
60
160
170
80
120
110
130
50
60
70
0
80
40
120
140
20
130
30
PRESSURE ALTITUDE - 14,000 FEET
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
TOTAL FUEL FLOW LB/HOUR
CRUISE
70
50
100
100
110
90
90
10
0
20
D
F = 10.0 SQ FT
D
Q %
10
0
20
D
F = 10.0 SQ FT
D
Q %
AH64A
CRUISE
T700GE701C
FAT=10C
FAT=0C
MAX
RANGE
MAX
RANGE
MAX
OR
R/C
MAX
END
MAX
OR
R/C
MAX
END
AIRSPEED
INDICATED
KNOTS
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-16.
Cruise Chart, 14,000 Feet, 10 C and 0 C (Sheet 3 of 5)