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
Summary of Contents for DA 42
Page 1: ......
Page 20: ...Introduction DA 42 AFM Page 0 18 Rev 8 15 Dec 2017 Doc No 7 01 05 E Intentionally left blank ...
Page 46: ...General DA 42 AFM Page 1 26 Rev 8 15 Dec 2017 Doc No 7 01 05 E Intentionally left blank ...
Page 236: ...Performance DA 42 AFM Page 5 4 Rev 8 15 Dec 2017 Doc No 7 01 05 E ...
Page 237: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 5 ...
Page 247: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 15 ...
Page 251: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 19 ...
Page 257: ...DA 42 AFM Performance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 5 25 ...
Page 268: ...Performance DA 42 AFM Page 5 36 Rev 8 15 Dec 2017 Doc No 7 01 05 E Intentionally left blank ...
Page 277: ...DA 42 AFM Mass and Balance Doc No 7 01 05 E Rev 8 15 Dec 2017 Page 6 9 6 4 2 LOADING DIAGRAM ...
Page 390: ...Handling Care Maintenance DA 42 AFM Page 8 12 Rev 8 15 Dec 2017 Doc No 7 01 05 E ...