Diamond DA 42 - 5.3.7 Climb Performance - Take-off Climb

DA 42 AFM Performance
Doc. No. 7.01.05-E Rev. 8 15-Dec-2017 Page 5 - 17
Gradient
ROC fpm
TAS KTAS
[%]
[]
[]
.  095
Gradient
ROC m s
TAS KTAS
[%]
[/]
[]
 190
5.3.7 CLIMB PERFORMANCE - TAKE-OFF CLIMB
Conditions:
- POWER lever ....................... both MAX @ 2300 RPM
- Flaps .............................. UP
- Landing gear ........................ retracted
- Airspeed
up to 1700 kg (3748 lb) .............. 77 KIAS
above 1700 kg (3748 lb) ............. 79 KIAS
NOTE
The charts on the following pages show the rate of climb. The
gradient of climb cannot easily be determined with a chart,
but it can be calculated using the following formulae: