TM 1-1520-238-10
7A-38
M01-254
MAX
RANGE
PRESSURE ALTITUDE - 6000 FEET
80
70
160
100
110
120
140
150
130
90
700
1300
1100
900
700
900
1100
1300
170
60
100
70
90
80
130
120
160
140
150
110
170
110
100
160
130
140
170
150
90
120
80
TOTAL FUEL FLOW – LB/HOUR
TOTAL FUEL FLOW – LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
60
180
0
30
100
50
70
50
60
40
80
90
70
CRUISE
60
40
80
90
70
30
60
30
40
50
20
40
50
30
20
10
100
20
30
40
50
AH–64A
CRUISE
T700–GE–701C
FAT=–30C
FAT=–20C
10
0
20
D
F = 10.0 SQ FT
D
Q – %
10
0
20
D
F = 10.0 SQ FT
D
Q – %
MAX
RANGE
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
AIRSPEED
INDICATED
KNOTS
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-12.
Cruise Chart, 6,000 Feet, –30 C and –20 C (Sheet 2 of 5)
