TM 1-1520-238-10
7A-39
PRESSURE ALTITUDE - 6000 FEET
80
100
140
160
180
150
170
110
120
90
130
80
1300
900
1100
1100
1300
700
100
70
90
130
120
160
140
150
110
170
900
700
170
110
120
130
140
150
160
180
90
100
TOTAL FUEL FLOW – LB/HOUR
30
TOTAL FUEL FLOW – LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
70
80
20
10
50
100
50
60
40
80
90
70
30
20
40
50
60
70
40
CRUISE
60
60
40
80
70
90
20
40
30
60
50
0
30
100
50
30
AH–64A
CRUISE
T700–GE–701C
FAT=–10C
FAT=0C
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
M01-255
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 – %
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-12.
Cruise Chart, 6,000 Feet, –10 C and 0 C (Sheet 3 of 5)
