TM 1-1520-238-10
7A-49
M01-265
10
20
30
50
40
80
120
130
60
1000
800
150
160
1400
170
800
1000
1200
90
50
180
140
40
600
100
120
130
50
140
90
100
80
70
0
100
80
60
40
80
90
70
600
150
170
160
150
140
PRESSURE ALTITUDE-10000 FEET
130
120
TOTAL FUEL FLOW – LB/HOUR
110
160
170
180
110
70
60
40
30
20
100
20
30
50
60
40
70
80
90
70
30
100
90
60
1200
1400
CRUISE
30
110
50
TOTAL FUEL FLOW – LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
FAT=–10C
FAT=0C
AIRSPEED
INDICATED
KNOTS
AH–64A
CRUISE
T700–GE–701C
10
0
20
D
F = 10.0 SQ FT
D
Q – %
MAX
RANGE
MAX
RANGE
MAX
OR
R/C
MAX
END
10
0
20
D
F = 10.0 SQ FT
D
Q – %
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
MAX R/C
OR
MAX END
Figure 7A-14.
Cruise Chart, 10,000 Feet, –10 C and 0 C (Sheet 3 of 5)
