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Diamond DA 42 - Page 63

Diamond DA 42
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DA 42 AFM Operating Limitations
Doc. No. 7.01.05-E Rev. 8 15-Dec-2017
EASA
approved
Page 2 - 17
NOTE
In some countries the beginning of a flight is defined by
starting the powerplant. In those countries a ramp mass of
maximal MTOM + 8 kg (MTOM + 18 lb) is approved. At the
time of lift-off the maximum permitted take-off mass must not
be exceeded.
NOTE
If MÄM 42-088 is carried out and OÄM 42-195 is not carried
out, a landing with a mass between 1700 kg (3748 lb) and
1785 kg (3935 lb) constitutes an abnormal operating
procedure.
NOTE
For a zero fuel mass above 1650 kg (3638 lb) a structural
temperature limit has been established which must be
observed before flight.

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