Performance |
DA 40 NG AFM |
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5.3.8 CLIMB PERFORMANCE - TAKE-OFF CLIMB
Conditions: - POWER lever . . . . . . . . . . . . . . |
92% or max. 2100 RPM |
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- |
Flaps . . . . . . . . . . . . . . . . . . . . |
T/O |
- |
Airspeed . . . . . . . . . . . . . . . . . . |
72 KIAS |
NOTE
The graph on the following page shows the rate of climb. The gradient of climb cannot easily be determined with a graph, but it can be calculated using the following formulae:
ROC [fpm]
Gradient [%] TAS [KTAS] 0.95
ROC [m/s]
Gradient [%] TAS [KTAS] 190
% |
NOTE |
% |
For operation without wheel fairings a climb rate decreased |
% |
by 20 ft/min must be expected. |
Page 5 - 16 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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DA 40 NG AFM |
Performance |
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Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 5 - 17 |
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Performance |
DA 40 NG AFM |
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5.3.9 CLIMB PERFORMANCE - CRUISE CLIMB |
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Conditions: - POWER lever . . . . . . . . . . . . . . |
92% or max. 2100 RPM |
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- |
Flaps . . . . . . . . . . . . . . . . . . . . |
UP |
- |
Airspeed . . . . . . . . . . . . . . . . . . |
88 KIAS |
NOTE
The graph on the following page shows the rate of climb. The gradient of climb cannot easily be determined with a graph, but it can be calculated using the following formulae:
ROC [fpm]
Gradient [%] TAS [KTAS] 0.95
ROC [m/s]
Gradient [%] TAS [KTAS] 190
% |
NOTE |
% |
For operation without wheel fairings a climb rate decreased |
% |
by 40 ft/min must be expected. |
Page 5 - 18 |
Rev. 1 |
15-Mar-2011 |
Doc. # 6.01.15-E |
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DA 40 NG AFM |
Performance |
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Doc. # 6.01.15-E |
Rev. 1 |
15-Mar-2011 |
Page 5 - 19 |
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