Emergency
Procedures
DA 40 NG AFM
Page 3 - 18
Rev. 3
01-Jul-2014
Doc. # 6.01.15-E
3.3.3 ENGINE TROUBLESHOOTING IN FLIGHT
WARNING
Control over the flight attitude has priority over attempts to
solve the current problem ("first fly the airplane").
1.
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . 88 KIAS
2.
POWER lever . . . . . . . . . . . . . . . . . . . . . . . . MAX
NOTE
If the loss of power was due to unintentional setting of the
POWER lever, you may adjust the friction lock and continue
your flight.
If ECU A and ECU B Cautions Appear Simultaneously
- If the indicated LOAD remains unchanged, and
- if the perceived thrust is reduced, and
- if the engine noise level changes or the engine is running rough:
3. POWER lever . . . . . . . . . . . . . . . . . . . . . . . . . IDLE for 1 second
4. POWER lever . . . . . . . . . . . . . . . . . . . . . . . . . slowly increase to 1975 RPM
If the engine shows a power loss during the POWER lever increase:
5. POWER lever . . . . . . . . . . . . . . . . . . . . . . . . . IDLE for 1 second
6. POWER lever . . . . . . . . . . . . . . . . . . . . . . . . . slowly increase, stop prior to the
previously observed engine
power loss RPM
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...
