TM 1-1520-238-10
7A-46
M01-262
PRESSURE ALTITUDE - 8000 FEET
700
1300
700
1100
900
1100
1300
900
130
180
160
150
170
120
110
100
140
80
90
100
70
90
80
130
120
160
140
150
110
170
90
120
170
140
150
160
180
110
100
130
TOTAL FUEL FLOW – LB/HOUR
0
TOTAL FUEL FLOW – LB/HOUR
60
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
80
60
70
30
40
50
60
70
20
50
40
30
100
CRUISE
50
60
40
80
20
90
70
30
100
50
60
40
80
90
30
20
30
10
70
40
50
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
MAX
OR
R/C
MAX
END
MAX
OR
R/C
MAX
END
AH–64A
CRUISE
T700–GE–701C
AIRSPEED
INDICATED
KNOTS
FAT=+30C
FAT=+40C
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-13.
Cruise Chart, 8,000 Feet, +30 C and +40 C (Sheet 5 of 5)
