130
TRUE AIRSPEED ~ KTS
120
TRUE AIRSPEED ~ KTS
120
110
110
100
100
50
50
10
10
20 30 40 50 60 70 80 90100 TORQUE PER ENGINE ~ % TORQUE PER ENGINE ~ % AA0424
DATA BASE:FLIGHT TEST SA
CRUISE
CRUISE 12000 FT
CLEAN CONFIGURATION T700 (2) PRESS ALT: 12000 FT
.10OC0OC
TOTAL FUEL FLOW ~ 100 LB/HR IAS ~ KTS TOTAL FUEL FLOW ~ 100 LB/HR
5 6 7 8 910 11 12 13 5 6 7 8 910 11 12 13
TRUE AIRSPEED ~ KTS
TRUE AIRSPEED ~ KTS
20
20
10
10
20 30 40 50 60 70 80 90100 TORQUE PER ENGINE ~ % TORQUE PER ENGINE ~ % AA0423
DATA BASE:FLIGHT TEST SA
CRUISE
CRUISE 12000 FT
CLEAN CONFIGURATION T700 (2) PRESS ALT: 12000 FT
10OC20OC
TOTAL FUEL FLOW ~ 100 LB/HR IAS ~ KTS TOTAL FUEL FLOW ~ 100 LB/HR
5 6 7 8 910 11 12 13 5 6 7 8 910 11 12 13
170
60
40
60
160 150
140
130
120
110
TRUE AIRSPEED ~ KTS
TRUE AIRSPEED ~ KTS
100
90
80
70
60
50
30
20
30 30
20 20
10
10 10
0 0
0
TORQUE PER ENGINE ~ % TORQUE PER ENGINE ~ % AA0426
DATA BASE:FLIGHT TEST SA
Figure 7-19. Cruise -Pressure Altitude 12,000 Feet (Sheet 4 of 5)
7-88
CRUISE
CRUISE 12000 FT
CLEAN CONFIGURATION T700 (2) PRESS ALT: 12000 FT
30oC
4
180 170 160 150 140 130 120 110 100 90 80 70 60
50 40 30 20 10 0 10
TOTAL FUEL FLOW ~ 100 LB/HR 5 6 7 8910
TRUE AIRSPEED ~ KTS
20
30 40 50 60 70 TORQUE PER ENGINE ~ %
11
80
IAS ~ KTS 12
170 160 150 140 130 120 110 100 90 80 70 60 50 40 30 20 10 0
90
AA0427A
DATA BASIS: FLIGHT TEST
SA
CRUISE
PRESS ALT: 12000 FT
.50oC .40oC
TOTAL FUEL FLOW ~ 100 LB/HR IAS ~ KTS TOTAL FUEL FLOW ~ 100 LB/HR
4 5 6 7891011 4 5 6 7891011
130
TRUE AIRSPEED ~ KTS
TRUE AIRSPEED ~ KTS
120
110
120
110
100
100
90
90
80
80
60
60
40
40
10
10
10 20 30 40 50 60 70 80 90 10 20 30 40 50 60 70 80 90
TORQUE PER ENGINE ~ % TORQUE PER ENGINE ~ %
DATA BASE:FLIGHT TEST Figure 7-20. Cruise High Drag -Pressure Altitude 12,000 Feet (Sheet 1 of 5) 7-90 SA AA0569
CRUISE
PRESS ALT: 12000 FT
.30oC .20oC
TOTAL FUEL FLOW ~ 100 LB/HR IAS ~ KTS TOTAL FUEL FLOW ~ 100 LB/HR
4 5 6 7891011 4 5 6 7891011
TRUE AIRSPEED ~ KTS
130
120
110
100
130
120
110
100
TRUE AIRSPEED ~ KTS
40
40
30
30
10
10
10 20 30 40 50 60 70 80 90 10 20 30 40 50 60 70 80 90
TORQUE PER ENGINE ~ % TORQUE PER ENGINE ~ %
DATA BASE:FLIGHT TEST Figure 7-20. Cruise High Drag -Pressure Altitude 12,000 Feet (Sheet 2 of 5) SA AA0570
7-91
CRUISE
PRESS ALT: 12000 FT
.10OC 0OC
TOTAL FUEL FLOW ~ 100 LB/HR IAS ~ KTS TOTAL FUEL FLOW ~ 100 LB/HR 4
5 6 7891011 4 5 6 7891011
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