DA 40 NG AFM
Abnormal Operating
Procedures
Doc. # 6.01.15-E
Rev. 3
01-Jul-2014
Page 4B - 15
1. ALTERNATE AIR . . . . . . . . . . . . . . . . . . . OPEN
%
2. Fuel pump . . . . . . . . . . . . . . . . . . . . . . . . ON
%
3. Circuit breakers . . . . . . . . . . . . . . . . . . . . check / reset if necessary
%
4. VOTER switch . . . . . . . . . . . . . . . . . . . . . AUTO
%
%
If the ECU B caution persists:
- land at the next suitable airfield. After landing, you
%
may use (a) ECU B Caution on the ground as ECU
%
caution clearing procedure.
%
NOTE
%
An ECU FAIL caution is caused by various types of
%
malfunctions. These include internal ECU problems, sensor
%
failure or insufficient performance of air-, fuel- or electrical
%
supply system (e.g. air filter icing).
%
NOTE
If additional engine problems are observed refer to Section
3.3.3 - ENGINE TROUBLESHOOTING IN FLIGHT.
END OF CHECKLIST
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...
