DA 40 NG AFM
Abnormal Operating
Procedures
Doc. # 6.01.15-E
Rev. 3
01-Jul-2014
Page 4B - 21
4B.5
FAILURES IN FLAP OPERATING SYSTEM
Failure in Position Indication or Function
1.
FLAPS position . . . . . . . . . . . . . . . . . . . . . . . check visually
2.
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . keep in white range
(max. 98 KIAS)
3.
FLAPS switch . . . . . . . . . . . . . . . . . . . . . . . . re-check all positions
Modified Approach Procedure Depending on the Available Flap Setting
%
NOTE
For landing distances with an abnormal flap position refer to
5.3.12 - LANDING DISTANCE - ABNORMAL FLAP
POSITION.
(a) Only UP Available:
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . see table below:
940 kg
(2072 lb)
1000 kg
(2205 lb)
1100 kg
%
(2425 lb)
%
1200 kg
%
(2646 lb)
%
1216 kg
(2681 lb)
1280 kg
(2822 lb)
and
%
above
%
71 KIAS
73 KIAS
78 KIAS
82 KIAS
%
82 KIAS
83 KIAS
%
Land at a flat approach angle, use POWER lever to control airplane speed and rate
of descent.
CONTINUED
Summary of Contents for DA 40 NG
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Page 2: ...DA 40 NG AFM Introduction Page 0 0a Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...
Page 240: ...Mass Balance DA 40 NG AFM Page 6 8 Rev 3 01 Jul 2014 Doc 6 01 15 E 6 4 2 LOADING DIAGRAM...
Page 316: ...Handling DA 40 NG AFM Page 8 8 Rev 3 01 Jul 2014 Doc 6 01 15 E...
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