TM 1-1520-238-10
7A-33
M01-249
100
130
110
60
20
80
90
700
160
140
150
170
160
140
150
1300
170
1100
900
900
700
1100
1300
170
150
180
140
160
TOTAL FUEL FLOW – LB/HOUR
TOTAL FUEL FLOW – LB/HOUR
PRESSURE ALTITUDE - 4000 FEET
130
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
70
110
120
40
80
90
20
70
100
60
50
30
20
CRUISE
120
30
130
10
30
100
50
80
60
40
80
90
70
30
70
100
60
100
110
50
40
50
90
60
40
80
90
70
120
30
40
50
0
FAT=–10C
FAT=0C
10
0
20
D
F = 10.0 SQ FT
D
Q – %
AIRSPEED
INDICATED
KNOTS
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
10
0
20
D
F = 10.0 SQ FT
D
Q – %
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-11.
Cruise Chart, 4,000 Feet, –10 C and 0 C (Sheet 3 of 6)
