Diamond DA 42 - 5.3.9 One Engine Inoperative Climb Performance

DA 42 AFM Performance
Doc. No. 7.01.05-E Rev. 8 15-Dec-2017 Page 5 - 23
Gradient
ROC fpm
TAS KTAS
[%]
[]
[]
.  095
Gradient
ROC m s
TAS KTAS
[%]
[/]
[]
 190
5.3.9 ONE ENGINE INOPERATIVE CLIMB PERFORMANCE
Conditions:
- Remaining engine (RH) ................ MAX @ 2300 RPM
- Dead engine ........................ feathered and secured
- Flaps .............................. UP
- Airspeed ............................ 82 KIAS
- Landing gear ........................ retracted
- Zero sideslip ........................ established
NOTE
With respect to handling and performance, the left-hand
engine (pilots view) is considered the "critical" engine.
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: