Emergency
Procedures
DA 40 AFM
Page 3 - 14
Rev. 8
01-Dec-2010
Doc. # 6.01.01-E
(g) Loss of RPM
1.
Electrical fuel pump . . . . . . . . . . . . . . . . . . . check ON
2.
Fuel tank selector . . . . . . . . . . . . . . . . . . . . check
3.
Friction adjuster for throttle quadrant . . . . . . check sufficiently tight
4.
RPM lever . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPM
*
Listen for rise in RPM.
-
If there is no audible rise in RPM, it is probable that the governor system
is defective. In this case the RPM can be regulated within certain limits
using the throttle.
-
Land at the nearest appropriate airfield.
-
Be prepared for possible emergency landing.
-
If the indication does not change in spite of an audible rise in RPM, it is
probable that the RPM indication is defective, which should thus be
ignored (the airplane should be serviced).
END OF CHECKLIST
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 ...