TM 1-1520-238-10
7A-37
PRESSURE ALTITUDE - 6000 FEET
60
70
90
80
90
80
90
80
70
800
100
130
120
160
140
150
110
170
600
100
1200
1000
900
1100
700
1300
140
130
120
170
150
110
150
160
170
140
130
120
110
100
TOTAL FUEL FLOW – LB/HOUR
0
30
TOTAL FUEL FLOW – LB/HOUR
100
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
160
50
60
40
80
90
70
40
70
30
100
50
60
40
80
90
70
CRUISE
20
30
40
50
50
30
20
10
60
20
30
60
50
40
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 – %
FAT=–50C
FAT=-40C
AH–64A
CRUISE
T700–GE–701C
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
M01-253
MAX
RANGE
MAX
RANGE
MAX END
OR
MAX R/C
MAX END
OR
MAX R/C
VNE
VNE
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-12.
Cruise Chart, 6,000 Feet, –50 C and –40 C (Sheet 1 of 5)
