Abnormal Operating
Procedures
DA 62 AFM
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
Page 4B - 32 Rev. 0 11-Jan-2019 Doc. No. 11.01.05-E
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