Diamond Aircraft DV 20 E - Engine Management System Failures; Erroneous Indication or Failure of Engine Displays

Emergency
Procedures
DV 20 E AFM
Page 3 - 20 Rev. 2 22-Mar-2022
EASA
approved
Doc. No. 4.01.25-E
3.6 ENGINE MANAGEMENT SYSTEM FAILURES
3.6.1 ERRONEOUS INDICATION OR FAILURE OF ENGINE DISPLAYS
NOTE
Loss of an engine parameter on the engine instrument is
indicated by a white “---” instead of values in the data field.
Erroneous indications may be determined by comparing a
display with other displays and other system information.
1. Set power based on throttle lever position, engine noise and speed.
'
2. Monitor other indications to determine the health of the engine.
3. Use known power lever settings.
4. Use other system information, such as annunciator messages, fuel quantity and
consumption.
5. Land on the next suitable airfield.
END OF CHECKLIST