Operating Limitations DA 42 AFM
Page 2 - 20 Rev. 8 15-Dec-2017
EASA
approved
Doc. No. 7.01.05-E
2.10 MANEUVERING LOAD FACTORS
NOTE
The tables below show structural limitations. The load factor
limits for the TAE 125 engine must also be observed. Refer
to the corresponding Operation & Maintenance Manual for
the engine.
CAUTION
Avoid extended negative g-loads duration. Extended negative
g-loads can cause propeller control problems and engine
surging.
at v
A
at v
NE
With Flaps in APP
or LDG Position
Positive 3.8 3.8 2.0
Negative -1.52 0
WARNING
Exceeding the maximum structural load factors will lead to
overstressing of the airplane.
CAUTION
Exceeding the maximum powerplant load factors and time
limits listed below will lead to a L/R OIL PRES warning.
Load Factor Time Limit
-0.2 5 seconds
-0.3 4 seconds
-0.4 3 seconds
-0.5 2 seconds
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