TM 1-1520-238-10
7A-51
M01-267
PRESSURE ALTITUDE - 10,000 FEET
180
170
100
150
140
160
120
130
110
180
150
130
110
120
140
170
160
110
150
140
120
130
80
90
70
100
1400
1000
800
800
1000
1200
1400
1200
170
160
600
TOTAL FUEL FLOW – LB/HOUR
50
TOTAL FUEL FLOW – LB/HOUR
60
0
40
30
50
60
70
90
80
40
20
90
80
40
60
50
100
30
10
100
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
600
CRUISE
90
80
40
60
50
100
30
20
90
80
70
60
40
50
70
30
20
30
70
FAT=+30C
FAT=+40C
AH–64A
CRUISE
T700–GE–701C
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
MAX
RANGE
MAX
RANGE
MAX
OR
R/C
MAX
END
MAX
OR
R/C
MAX
END
10
0
20
D
F = 10.0 SQ FT
D
Q – %
AIRSPEED
INDICATED
KNOTS
10
0
20
D
F = 10.0 SQ FT
D
Q – %
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-14.
Cruise Chart, 10,000 Feet, +30 C and +40 C (Sheet 5 of 5)
