TM 1-1520-238-10
7A-22
M01-238
130
120
100
110
90
30
70
60
80
50
40
20
10
20
30
50
60
100
70
0
90
80
130
40
120
110
70
90
40
60
50
100
30
70
90
80
40
60
50
100
30
90
110
130
120
100
70
60
80
50
30
40
20
800
160
140
150
170
170
800
1200
150
160
1000
1400
140
1000
170
1400
1200
150
160
140
PRESSURE ALTITUDE - SEA LEVEL
TOTAL FUEL FLOW – LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
TOTAL FUEL FLOW – LB/HOUR
CRUISE
FAT=+10C
FAT=+20C
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 – %
DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
AH–64A
CRUISE
T700–GE–701C
MAX
RANGE
MAX
RANGE
DATA BASIS:
80
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
Figure 7A-9.
Cruise Chart, Sea Level, +10 C and +20 C (Sheet 4 of 6)
