TM 1-1520-238-10
7A-20
M01-236
PRESSURE ALTITUDE - SEA LEVEL
30
100
90
80
60
50
40
70
20
10
20
30
50
60
100
70
0
90
80
40
110
70
90
80
40
60
50
100
70
90
80
40
60
50
100
30
30
100
90
80
60
50
40
70
20
30
130
120
160
140
150
170
700
900
1100
1300
900
1100
1300
160
700
150
130
120
140
110
160
140
130
120
150
110
TOTAL FUEL FLOW – LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
FAT=–30C
TOTAL FUEL FLOW – LB/HOUR
FAT=-20C
CRUISE
10
D
F = 10.0 SQ FT
D
Q – %
0
20
AIRSPEED
INDICATED
KNOTS
MAX
RANGE
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
AH–64A
CRUISE
T700–GE–701C
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
Figure 7A-9.
Cruise Chart, Sea Level, –30 C and –20 C (Sheet 2 of 6)
