TM 1-1520-238-10
7A-54
M01-270
PRESSURE ALTITUDE - 12,000 FEET
1400
600
800
1000
1400
1200
1000
800
600
1200
80
90
110
180
170
100
160
150
140
130
120
60
100
70
90
80
130
120
160
140
150
110
170
180
160
150
140
170
110
130
120
100
TOTAL FUEL FLOW – LB/HOUR
30
50
60
50
20
80
40
50
TOTAL FUEL FLOW – LB/HOUR
100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL
30
20
10
90
70
40
80
90
70
30
100
50
60
40
80
90
20
0
30
100
CRUISE
70
60
40
30
70
60
50
40
FAT=–10C
FAT=0C
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 END
OR
MAX R/C
MAX
OR
R/C
MAX
END
AH–64A
CRUISE
T700–GE–701C
DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988
INDICATED TORQUE PER ENGINE
~
%
INDICATED TORQUE PER ENGINE
~
%
Figure 7A-15.
Cruise Chart, 12,000 Feet, –10 C and 0 C (Sheet 3 of 5)
