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Figure 9-1-6. 714A Height Velocity Diagram for Safe Landing After Single-Engine Failure (Sheet 2 of 3)
Figure 9-1-7. Maximum Glide Distance / Minimum Rate of Decent in Autorotation
TM-1-1520-240-10 Army CH-47D Heilcopter (EIC:RCD) Manual
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TM 1-1520-240-10
9-1-14
Figure 9-1-6.
714A
Height Velocity Diagram for Safe Landing After Single-Engine Failure (Sheet 3 of 3)