Performance DA 62 AFM
5.3.8 CLIMB PERFORMANCE - CRUISE CLIMB
Conditions:
- Power lever . . . . . . . . . . . . . . . . . . . . . . . . . . both 95%
- Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
- Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . retracted
- Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . according table
The climb performance tables show the rate of climb. The gradient of climb can be
calculated using the following formula:
Page 5 - 44 Rev. 0
11-Jan-2019
Doc. No. 11.01.05-E