PPRuNe Forums - View Single Post - Less airspeed effect on single engine performanceof Bell-412 helicopter
Old 1st Nov 2018, 18:46
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switch_on_lofty
 
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If you've calculated that the best oei rate of climb was -200'/min in the circumstances of the engine shutdown then it was not possible to level flight at any speed at this altitude. I.e the helicopter had to descend to a lower density altitude to achieve level flight performance.
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