DA 62 AFM General
Modification Source Installed
WX-500 Storm Scope OÄM 62-021 9 yes 9 no
Continuous Flow Oxygen
System (50 cuft cylinder)
OÄM 62-028 9 yes 9 no
Removal of Unfeathering
Akkumulator
OÄM 62-030 9 yes 9 no
Heated Static Ports OÄM 62-037 9 yes 9 no
On Top Exhaust System OÄM 62-038 9 yes 9 no
28V Power Outlet Option OÄM 62-1002 9 yes 9 no
* Or later approved software
This Airplane Flight Manual must be kept on board the airplane at all times. Its designated
place is the side bag of the forward left seat. The designated place for the Garmin G1000
Cockpit Reference Guide is the bag on the rear side of the forward right seat.
CAUTION
The DA 62 is a twin engine airplane. When the operating
limitations and maintenance requirements are complied with,
it has the high degree of reliability which is required by the
certification basis. Nevertheless, an engine failure is not
completely impossible. For this reason it is highly
recommended for flights during the night, on top, under IMC,
or above terrain which is unsuitable for a landing, to select
flight times and flight routes such that reduced performance
in case of single engine operation does not constitute a risk.
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019 Page 1 - 3
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