DA 40 AFM
Performance
Doc. # 6.01.01-E
Rev. 8
01-Dec-2010
Page 5 - 21
5.3.11 LANDING DISTANCE - FLAPS UP
Conditions:
- Throttle . . . . . . . . . . . . . . . . . . IDLE
- RPM lever . . . . . . . . . . . . . . . . HIGH RPM
- Flaps . . . . . . . . . . . . . . . . . . . . UP
- Approach speed . . . . . . . . . . . 73 KIAS (1200 kg, 2646 lb)
%
71 KIAS (1150 kg, 2535 lb)
63 KIAS (1000 kg, 2205 lb)
58 KIAS (850 kg, 1874 lb)
- Runway . . . . . . . . . . . . . . . . . . level, asphalt surface
NOTE
%
A landing mass above 1150 kg (2535 lb) up to 1200 kg
%
(2646 lb) will increase the landing distance over a 50 ft (15 m)
%
obstacle and the landing ground roll distance up to 6%.
%
Values for ISA and MSL, at 1150 kg (2535 lb)
Landing distance over a 50 ft (15 m) obstacle
approx. 775 m (2543 ft)
Ground roll
approx. 471 m (1545 ft)
WARNING
Poor maintenance condition of the airplane, deviation from
the given procedures as well as unfavorable external factors
(high temperature, rain, unfavorable wind conditions, including
cross-wind) will increase the landing distance.
Summary of Contents for DA 40
Page 1: ......
Page 37: ...DA 40 AFM General Doc 6 01 01 E Rev 8 01 Dec 2010 Page 1 21 1 7 THREE VIEW DRAWING ...
Page 182: ...Performance DA 40 AFM Page 5 12 Rev 8 01 Dec 2010 Doc 6 01 01 E ...
Page 184: ...Performance DA 40 AFM Page 5 14 Rev 8 01 Dec 2010 Doc 6 01 01 E ...
Page 186: ...Performance DA 40 AFM Page 5 16 Rev 8 01 Dec 2010 Doc 6 01 01 E ...
Page 190: ...Performance DA 40 AFM Page 5 20 Rev 8 01 Dec 2010 Doc 6 01 01 E ...
Page 288: ...Handling DA 40 AFM Page 8 6 Rev 8 01 Dec 2010 Doc 6 01 01 E ...