DA 40 NG AFM
Emergency
Procedures
Doc. # 6.01.15-E
Rev. 3
01-Jul-2014
Page 3 - 19
WARNING
Do not increase the POWER lever past the propeller speed
of 1975 RPM or the setting determined in step 6. An increase
of engine power beyond this setting leads into another power
loss.
NOTE
With this power setting the engine can provide up to 65 %
load at the maximum propeller speed of 1975 RPM.
7. Land at the next suitable airfield.
Otherwise:
Depending on the situation the following attempts can be made to restore normal engine
operation:
3.
Circuit breakers . . . . . . . . . . . . . . . . . . . . . . check / reset if necessary
If normal engine operation is restored continue flight and land as soon as possible.
Otherwise:
4.
VOTER switch . . . . . . . . . . . . . . . . . . . . . . . swap between ECU A and B
If either ECU A or B setting restores normal engine operation then maintain ECU setting
and land as soon as possible.
CONTINUED
Summary of Contents for DA 40 NG
Page 1: ......
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...
Page 322: ...Handling DA 40 NG AFM Page 8 14 Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...
