DA 62 AFM
Normal Operating
Procedures
14. ELECT. MASTER . . . . . . . . . . . . . . . . . . . . . ON
CAUTION
When switching the ELECT. MASTER 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 preparation. There is a malfunction in the
landing gear system.
15. G1000 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . wait until power-up completed.
Press ENT on MFD to
acknowledge.
NOTE
The engine instruments are only available on the MFD after
item 16 has been completed.
16. Fuel temperature . . . . . . . . . . . . . . . . . . . . . . check
END OF CHECKLIST
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019 Page 4A - 21
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