TM 1-1520-238-10
7A-30
M01-246
PRESSURE ALTITUDE - 2000 FEET
700
1300
800
1100
900
1400
1200
1000
180
170
150
120
160
140
130
90
110
100
80
100
70
90
80
130
120
20
140
150
110
120
180
170
160
150
140
130
110
100
90
TOTAL FUEL FLOW LB/HOUR
20
10
60
40
70
50
30
TOTAL FUEL FLOW LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
160
70
20
40
50
70
30
60
0
30
100
50
80
60
40
80
90
CRUISE
30
100
50
60
40
80
90
70
40
60
50
30
170
AIRSPEED
INDICATED
KNOTS
FAT=+50C
FAT=+60C
MAX
OR
R/C
MAX
END
MAX
OR
R/C
MAX
END
DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
AH64A
CRUISE
T700GE701C
MAX
RANGE
10
0
20
D
F = 10.0 SQ FT
D
Q %
10
0
20
D
F = 10.0 SQ FT
D
Q %
DATA BASIS:
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-10.
Cruise Chart, 2,000 Feet, +50 C and +60 C (Sheet 6 of 6)