TM 1-1520-238-10
7A-34
M01-250
20
40
50
60
80
100
90
30
130
130
120
160
140
150
170
700
900
1100
1300
1300
900
700
1100
170
180
150
150
160
180
140
170
160
TOTAL FUEL FLOW – LB/HOUR
20
30
100
50
60
40
80
90
140
TOTAL FUEL FLOW – LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
70
CRUISE
100
130
110
30
120
90
70
70
80
60
90
50
40
20
110
40
80
90
70
100
60
50
30
10
PRESSURE ALTITUDE - 4000 FEET
0
30
100
50
110
60
120
40
80
70
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 – %
FAT=+10C
FAT=+20C
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
AH–64A
CRUISE
T700–GE–701C
MAX
RANGE
MAX
RANGE
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
Figure 7A-11.
Cruise Chart, 4,000 Feet, +10 C and +20 C (Sheet 4 of 6)
