TM 1-1520-238-10
7A-26
M01-242
PRESSURE ALTITUDE - 2000 FEET
900
1100
1300
1100
1300
900
700
90
70
80
150
100
110
120
130
140
160
700
100
90
80
130
120
160
140
150
110
170
90
160
140
130
150
110
100
120
80
TOTAL FUEL FLOW – LB/HOUR
40
80
90
70
40
50
30
60
0
30
100
50
60
40
80
20
TOTAL FUEL FLOW – LB/HOUR
90
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
70
70
40
60
50
70
30
20
10
60
50
40
20
30
30
100
50
60
CRUISE
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 – %
DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
AIRSPEED
INDICATED
KNOTS
AH–64A
CRUISE
T700–GE–701C
MAX
RANGE
MAX
RANGE
DATA BASIS:
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
MAX R/C
OR
MAX END
MAX R/C
OR
MAX END
Figure 7A-10.
Cruise Chart, 2,000 Feet, –30 C and –20 C (Sheet 2 of 6)
