DV 20 E AFM Operating Limitations
Doc. No. 4.01.25-E Rev. 2 22-Mar-2022
EASA
approved
Page 2 - 13
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 Operator’s Manual for the engine.
at v
A
at v
NE
with flaps in APP
or LDG position
Positive 4.4 4.4 2.0
Negative -2.2 -1.53 0.0
WARNING
Exceeding the maximum structural load factors will lead to
overstressing of the airplane.
CAUTION
Intentional negative g-maneuvers are not permitted.
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