TM 1-1520-238-10
7A-45
M01-261
PRESSURE ALTITUDE - 8000 FEET
700
170
900
1100
1300
900
700
1100
1300
150
160
180
140
130
170
110
100
90
80
120
100
70
90
80
130
120
160
140
150
110
180
160
150
170
130
120
110
140
TOTAL FUEL FLOW LB/HOUR
30
100
TOTAL FUEL FLOW LB/HOUR
50
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
40
50
60
40
80
90
70
30
CRUISE
20
40
10
0
50
30
100
50
60
40
80
90
70
30
100
90
20
30
60
60
40
70
20
50
60
70
80
AH64A
CRUISE
T700GE701C
FAT=+10C
FAT=+20C
10
0
20
D
F = 10.0 SQ FT
D
Q %
10
0
20
D
F = 10.0 SQ FT
D
Q %
MAX
OR
R/C
MAX
END
MAX
OR
R/C
MAX
END
MAX
RANGE
MAX
RANGE
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-13.
Cruise Chart, 8,000 Feet, +10 C and +20 C (Sheet 4 of 5)