Performance |
DA 40 NG AFM |
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5.3.14 GLIDE
The following table shows the glide ratio and the resulting maximum horizontal distance in nautical miles per 1000 ft (305 m) of altitude loss in a glide traveled in still air.
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Glide ratio |
Maximum horizontal distance |
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per 1000 ft (305 m) altitude loss |
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Windmilling |
1 : 9.7 |
1.59 NM (2.94 km) |
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propeller |
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Conditions:
- Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
- Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . 88 KIAS
CAUTION
The propeller will keep windmilling under all expected
conditions. Do not attempt to stop the propeller intentionally.
NOTE
In case of stationary propeller the given numbers are conservative.
NOTE
For operation without wheel fairings the glide ratio is reduced to 9.4; i.e., for every 1000 ft (305m) of altitude loss the maximum horizontal distance traveled in still air is 1.54 NM
(2.85 km). During this the propeller will continue to windmill.
Page 5 - 30 |
Rev. 2 |
15-Jun-2011 |
Doc. # 6.01.15-E |
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DA 40 NG AFM |
Performance |
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5.3.15 APPROVED NOISE DATA
ICAO Annex 16 Chapter X . . . . . . . . . . . . . . . . . . 74.5 dB(A)
CS-36 Subpart C . . . . . . . . . . . . . . . . . . . . . . . . . 74.5 dB(A)
% If the Exhaust Pipe with Muffler MÄM 40-434 or OÄM 40-310 is installed:
% ICAO Annex 16, Chapter X . . . . . . . . . . . . . . . . . . 71.5 dB(A)
% CS-36 Subpart C . . . . . . . . . . . . . . . . . . . . . . . . . 71.5 dB(A)
Doc. # 6.01.15-E |
Rev. 2 |
15-Jun-2011 |
Page 5 - 31 |
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Performance |
DA 40 NG AFM |
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% |
Intentionally left blank. |
Page 5 - 32 |
Rev. 2 |
15-Jun-2011 |
Doc. # 6.01.15-E |
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