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|  Slow-Speed Flight, Stall and Spin, and AOA System
T-45A/C TS, E2-C2, ADV & IUT Aero-03
2.03
Landing Configuration
CL
1.38
1.35
Clean
.78
60% of C L
at 17 Units AOA
MAX
AOA in Degrees
8.50
7.25
Figure 13: AOA SYSTEM THEORY
(9-99) Original
Page 3-26
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