DA 42 AFM
Performance
Doc. No. 7.01.05-E
Rev. 8
15-Dec-2017
Page 5 - 23
Gradient
ROC fpm
TAS KTAS
[%]
[
]
[
]
.
0 95
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:
Summary of Contents for DA 42
Page 1: ......
Page 20: ...Introduction DA 42 AFM Page 0 18 Rev 8 15 Dec 2017 Doc No 7 01 05 E Intentionally left blank ...
Page 46: ...General DA 42 AFM Page 1 26 Rev 8 15 Dec 2017 Doc No 7 01 05 E Intentionally left blank ...
Page 236: ...Performance DA 42 AFM Page 5 4 Rev 8 15 Dec 2017 Doc No 7 01 05 E ...
Page 237: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 5 ...
Page 247: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 15 ...
Page 251: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 19 ...
Page 257: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 25 ...
Page 268: ...Performance DA 42 AFM Page 5 36 Rev 8 15 Dec 2017 Doc No 7 01 05 E Intentionally left blank ...
Page 277: ...DA 42 AFM Mass and Balance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 6 9 6 4 2 LOADING DIAGRAM ...
Page 390: ...Handling Care Maintenance DA 42 AFM Page 8 12 Rev 8 15 Dec 2017 Doc No 7 01 05 E ...