Diamond DA 42 - Page 227

DA 42 AFM
Abnormal Operating
Procedures
Doc. No. 7.01.05-E Rev. 8 15-Dec-2017 Page 4B - 29
CAUTION
When switching the external power unit ON, the electrically
driven hydraulic gear pump may activate itself for 5 to
20 seconds in order to restore the system pressure. Should
the pump continue to operate continuously or periodically,
terminate flight. There is a malfunction in the landing gear
system.
NOTE
When switching the external power unit ON, all electrical
equipment, connected to the LH and RH main busses is
powered.
17. G1000 .............................. wait until power-up completed.
Press ENT on MFD to
acknowledge.
NOTE
The engine instruments are only available on the MFD after
item 17 has been completed.
END OF CHECKLIST