DA 42 NG AFM
Abnormal Operating
Procedures
Doc. No. 7.01.16-E Rev. 3 01-Apr-2014 Page 4B - 31
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 buses 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
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