TM 1-1520-238-10
7A-40
M01-256
PRESSURE ALTITUDE - 6000 FEET
700
1300
900
1100
900
1300
700
1100
170
90
120
160
150
140
130
110
100
80
180
170
110
150
140
160
120
130
80
90
70
100
60
180
170
150
140
130
120
110
100
160
90
TOTAL FUEL FLOW – LB/HOUR
90
80
50
40
20
30
50
40
30
50
10
70
60
60
30
70
20
40
20
70
90
80
40
40
60
50
100
30
0
80
60
50
100
30
70
TOTAL FUEL FLOW – LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
CRUISE
AH–64A
CRUISE
T700–GE–701C
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
FAT=+10C
FAT=+20C
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 – %
MAX
RANGE
MAX
RANGE
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, +10 C and +20 C (Sheet 4 of 5)
