TM 1-1520-238-10
7A-28
M01-244
PRESSURE ALTITUDE - 2000 FEET
700
1300
900
1100
1300
130
150
140
120
100
90
70
110
80
160
900
1100
170
700
170
110
150
140
160
120
130
80
90
70
100
60
90
80
100
120
130
150
110
170
160
140
180
TOTAL FUEL FLOW LB/HOUR
20
10
20
TOTAL FUEL FLOW LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
60
30
50
40
40
20
60
50
30
70
90
80
90
80
30
40
60
50
100
50
30
40
CRUISE
60
50
100
40
30
0
70
70
FAT=+10C
FAT=+20C
AIRSPEED
INDICATED
KNOTS
10
0
20
10
0
20
DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
AH64A
CRUISE
T700GE701C
DATA BASIS:
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
MAX
RANGE
MAX
RANGE
D
Q %
D
Q %
D
F = 10.0 SQ FT
D
F = 10.0 SQ FT
Figure 7A-10.
Cruise Chart, 2,000 Feet, +10 C and +20 C (Sheet 4 of 6)