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Dual Engine Failure
Engine Alternator Malfunction
TM-1-1520-238-10 Helicopter Attack AH-64A Apache Manual
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TM 1-1520-238-10
9
-10
Change 9
M01–047
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POWER OFF
AUTOROTATIONAL DESCENT
N
r
= 100%
INDICATED AIRSPEED KNOTS
~
Figure 9-3.
Autorotative Glide Chart
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