Diamond DA 40 Flight Manual page 139

DA 40 AFM
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10. Fuel pressure indicator . . . . . . . . . . . . . . . . check (approx. 14 - 35 PSI)
11. Electrical fuel pump . . . . . . . . . . . . . . . . . . . ON
12. Mixture control lever . . . . . . . . . . . . . . . . . . RICH (below 5000 ft)
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
16. Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2000 RPM
17. RPM lever . . . . . . . . . . . . . . . . . . . . . . . . . . pull back until a drop of
18. Magneto check . . . . . . . . . . . . . . . . . . . . . . L - BOTH - R - BOTH
CONTINUED
Doc. # 6.01.01-E
NOTE
Rev. 8 01-Dec-2010
Normal Operating
Procedures
sense
250 to 500 RPM is reached -
HIGH RPM; cycle 3 times
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
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