Performance |
DA 42 NG AFM |
5.3.7 CLIMB PERFORMANCE |
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Conditions: |
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- |
Power lever . . . . . . . . . . . . . . . . . . . . . . . . . |
both 92% load @ 2100 RPM |
- |
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
UP |
- |
Landing gear . . . . . . . . . . . . . . . . . . . . . . . . |
retracted |
- |
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
90 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:
ROC [fpm]
Gradient [%] = TAS [KTAS] 0.95
ROC [m/s]
Gradient [%] = TAS [KTAS] 190
Page 5 - 14 |
Rev. 1 |
18-Feb-2009 |
Doc. No. 7.01.15-E |
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DA 42 NG AFM |
Performance |
Conditions: Flaps: UP, Power: both @ 92%, Landing gear: retracted, Airspeed: 90 KIAS
Doc. No. 7.01.15-E |
Rev. 1 |
18-Feb-2009 |
Page 5 - 15 |
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Performance |
DA 42 NG AFM |
5.3.8 ONE ENGINE INOPERATIVE CLIMB PERFORMANCE
Conditions: |
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Remaining engine (RH) . . . . . . . . . . . . . . . . |
92% load or maximum 2100 RPM |
- |
Dead engine . . . . . . . . . . . . . . . . . . . . . . . . . |
feathered and secured |
- |
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
UP |
- |
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . |
85 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 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:
ROC [fpm]
Gradient [%] = TAS [KTAS] 0.95
ROC [m/s]
Gradient [%] = TAS [KTAS] 190
Page 5 - 16 |
Rev. 1 |
18-Feb-2009 |
Doc. No. 7.01.15-E |
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DA 42 NG AFM |
Performance |
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Conditions: Flaps: UP, Power: remaining engine @ 92% / dead engine: feathered and secured, Airspeed: 85 KIAS
Doc. No. 7.01.15-E |
Rev. 1 |
18-Feb-2009 |
Page 5 - 17 |
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