TM 1-1520-238-10
7A-24
M01-240
PRESSURE ALTITUDE - SEA LEVEL
CRUISE
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
1200
1400
1000
800
1400
1200
1000
800
170
160
TOTAL FUEL FLOW – LB/HOUR
TOTAL FUEL FLOW – LB/HOUR
160
30
40
50
60
70
80
90
100
110
120
130
140
150
170
180
120
130
110
150
140
40
80
90
0
70
100
60
50
30
20
10
180
170
160
150
140
130
120
110
100
90
80
70
60
50
40
30
20
30
100
50
60
40
80
90
70
30
100
50
60
40
80
90
70
20
FAT=+50C
FAT=+60C
AIRSPEED
INDICATED
KNOTS
DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
AH–64A
CRUISE
T700–GE–701C
DATA BASIS:
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
RANGE
MAX
RANGE
MAX R/C
OR
MAX END
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-9.
Cruise Chart, Sea Level, +50 C and +60 C (Sheet 6 of 6)
