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AOA system is subject to failure |
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|  Slow-Speed Flight, Stall and Spin, and AOA System
T-45A/C TS, E2-C2, ADV & IUT Aero-03
G. AOA system is subject to failure
1.
Perform an AOA check prior to landings
2.
If system fails, IAS is then used to fly the approach
and landing
a.
Proper speed for T-45 in landing configuration
is approximately 117 KIAS with 1,000 pounds of
fuel; this speed is increased 5 knots per
1,000 pounds of fuel
b.
Stall, glide, and other speeds vary
approximately 5 knots per 1,000 pounds of
weight
(9-99) Original
Page 3-30
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