DA 62 AFM Performance
5.3.9 ONE ENGINE INOPERATIVE CLIMB PERFORMANCE
Conditions:
- Remaining engine . . . . . . . . . . . . . . . . . . . . 95% load
- Dead engine . . . . . . . . . . . . . . . . . . . . . . . . . feathered and secured
- Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
- Landing gear. . . . . . . . . . . . . . . . . . . . . . . . . retracted
- Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . v
YSE
- Sideslip . . . . . . . . . . . . . . . . . . . . . . . . . . . . . one ball out, max. 5° bank
NOTE
With respect to handling and performance, the left-hand
engine (pilots view) is considered the "critical" engine.
The climb performance tables show the rate of climb. The gradient of climb can be
calculated using the following formula:
Doc. No. 11.01.05-E Rev. 0
11-Jan-2019
Page 5 - 49
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