Diamond DA 40 Flight Manual page 194

Performance
5.3.12 GRADIENT OF CLIMB ON GO-AROUND
The DA 40 reaches a constant gradient of climb of 7.0 % in the following condition:
- Mass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . max. flight mass (1150 kg,
- Power setting . . . . . . . . . . . . . . . . . . . . . . . . Take-off
- Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LDG
- Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 KIAS
- ISA, MSL
%
If MÄM 40-227 is carried out:
%
The DA 40 reaches a constant gradient of climb of 7.0 % in the following condition:
%
- Mass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . max. flight mass (1200 kg,
%
%
- Power setting . . . . . . . . . . . . . . . . . . . . . . . . Take-off
%
- Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LDG
%
- Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . 73 KIAS
%
- ISA, MSL
5.3.13 APPROVED NOISE DATA
ICAO Annex 16 Chapter X : 69.28 dB(A)
JAR-36 Subpart C
%
If MÄM 40-227 is carried out:
%
ICAO Annex 16 Chapter X : 78.4 dB(A)
%
JAR-36 Subpart C
Page 5 - 24
: 69.28 dB(A)
: 78.4 dB(A)
Rev. 8 01-Dec-2010
DA 40 AFM
2535 lb)
2646 lb)
Doc. # 6.01.01-E