Diamond DA 42 - 5.3.8 Climb Performance - Cruise Climb

Performance DA 42 AFM
Page 5 - 20 Rev. 8 15-Dec-2017 Doc. No. 7.01.05-E
Gradient
ROC m s
TAS KTAS
[%]
[/]
[]
 190
Gradient
ROC fpm
TAS KTAS
[%]
[]
[]
.  095
5.3.8 CLIMB PERFORMANCE - CRUISE CLIMB
Conditions:
- POWER lever........................ both MAX @ 2300 RPM
- Flaps .............................. UP
- Airspeed
up to 1700 kg (3748 lb) .............. 85 KIAS
above 1700 kg (3748 lb) ............. 86 KIAS
NOTE
The graphs on the following pages show the rate of climb.
The gradient of climb cannot easily be determined with a
graph, but it can be calculated using the following formulae: