TM 1-1520-238-10
7A-29
M01-245
20
PRESSURE ALTITUDE - 2000 FEET
60
1100
1100
700
900
1300
700
900
1300
180
170
160
150
90
140
130
120
110
100
80
100
70
90
80
130
120
160
140
150
110
170
130
180
160
170
150
140
120
100
90
110
TOTAL FUEL FLOW – LB/HOUR
50
60
40
30
20
10
20
30
80
90
TOTAL FUEL FLOW – LB/HOUR
30
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
50
60
70
40
60
70
0
30
100
50
40
CRUISE
60
70
40
50
80
40
80
90
70
30
100
50
DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
FAT=+40C
FAT=+30C
AIRSPEED
INDICATED
KNOTS
10
0
20
D
F = 10.0 SQ FT
D
Q – %
10
0
20
D
F = 10.0 SQ FT
D
Q – %
MAX
RANGE
MAX
RANGE
AH–64A
CRUISE
T700–GE–701C
DATA BASIS:
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-10.
Cruise Chart, 2,000 Feet, +30 C and +40 C (Sheet 5 of 6)
