TM 1-1520-238-10
7A-36
M01-252
PRESSURE ALTITUDE - 4000 FEET
150
170
180
140
130
160
110
100
120
100
90
130
120
160
140
150
110
170
130
140
110
90
100
120
180
160
150
170
900
1100
700
1300
1300
1100
900
TOTAL FUEL FLOW – LB/HOUR
20
90
40
80
70
40
70
TOTAL FUEL FLOW – LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
700
30
40
80
70
60
70
80
90
70
30
100
50
60
40
80
90
50
30
20
CRUISE
50
60
60
30
80
50
0
30
40
60
100
10
50
20
10
0
20
D
F = 10.0 SQ FT
D
Q – %
FAT=+50C
FAT=+60C
AIRSPEED
INDICATED
KNOTS
AH–64A
CRUISE
T700–GE–701C
MAX
OR
R/C
MAX
END
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
MAX
RANGE
10
0
20
D
F = 10.0 SQ FT
D
Q – %
MAX
RANGE
MAX
OR
R/C
MAX
END
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-11.
Cruise Chart, 4,000 Feet, +50 C and +60 C (Sheet 6 of 6)
