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Figure 7-20. Climb - Two Engines - Flaps 0%
Figure 7-22. Take-Off Climb Gradient - One-Engine Inoperative - Flaps 0%
TM-55-1510-219-10 Army Aviation Maintenance Engineering Manual Weight and Balance
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TM 55-1510-219-10
Figure 7-21. Climb - Two Engines - Flaps 40%
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