Operating Limitations DA 62 AFM
2.10 MANEUVERING LOAD FACTORS
NOTE
The tables below show structural limitations. The load factor
limits for the engine must also be observed. Refer to the
corresponding operation manual for the engine.
at v
O
at v
NE
with flaps in APP
or LDG position
Positive 3.8 3.8 2.0
Negative -1.52 0.0 0.0
WARNING
Exceeding the maximum structural load factors will lead to
overstressing of the airplane.
CAUTION
Intentional negative-g maneuvers are not permitted.
Page 2 - 22 Rev. 0 11-Jan-2019
DOT
approved
Doc. No. 11.01.05-E
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