TM 1-1520-238-10
7A-19
M01-235
30
20
40
50
70
60
100
80
90
110
120
130
30
20
40
90
140
120
110
80
100
70
50
60
130
70
90
80
40
60
50
100
30
30
100
50
60
40
80
90
70
110
150
140
120
40
130
80
90
0
70
100
60
50
30
20
10
700
140
900
150
1100
700
1300
900
1100
150
170
160
1300
PRESSURE ALTITUDE - SEA LEVEL
FAT=–40C
FAT=–50C
TOTAL FUEL FLOW – LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
TOTAL FUEL FLOW – LB/HOUR
CRUISE
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
AIRSPEED
INDICATED
KNOTS
10
D
F = 10.0 SQ FT
D
Q – %
0
20
10
0
20
D
F = 10.0 SQ FT
D
Q – %
MAX
RANGE
AH–64A
CRUISE
T700–GE–701C
VNE
MAX R/C
OR
MAX END
VNE
MAX
RANGE
MAX R/C
OR
MAX END
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-9.
Cruise Chart, Sea Level, –50 C and –40 C (Sheet 1 of 6)
