DA 40 AFM
Normal Operating
Procedures
Doc. # 6.01.01-E
Rev. 8
01-Dec-2010
Page 4A - 23
10.
Fuel pressure indicator . . . . . . . . . . . . . . . . check (approx. 14 - 35 PSI)
%
11.
Electrical fuel pump . . . . . . . . . . . . . . . . . . . ON
12.
Mixture control lever . . . . . . . . . . . . . . . . . . RICH (below 5000 ft)
NOTE
At a density altitude of 5000 ft or above or at high ambient
temperatures a fully rich mixture can cause rough running
of the engine or a loss of performance. The mixture should
be set for smooth running of the engine.
13.
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . check T/O
14.
Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . check T/O
15.
Flight controls . . . . . . . . . . . . . . . . . . . . . . . free movement, correct
sense
16.
Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2000 RPM
17.
RPM lever . . . . . . . . . . . . . . . . . . . . . . . . . . pull back until a drop of
250 to 500 RPM is reached -
HIGH RPM; cycle 3 times
18.
Magneto check . . . . . . . . . . . . . . . . . . . . . . L - BOTH - R - BOTH
Max. RPM drop . . 175 RPM
Max. difference . . . 50 RPM
If the electronic ignition
control unit is installed, the
ignition status light must
illuminate and extinguish
after approximately 20 to
30 sec
CONTINUED
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 ...