Maneuvering Load Factors - Diamond DA 40 Flight Manual

Operating
Limitations

2.10 MANEUVERING LOAD FACTORS

Table of maximum structural load factors:
Normal Category
Positive
Negative
Utility Category
Positive
Negative
Exceeding the maximum load factors will lead to an
overstressing of the airplane.
Page 2 - 16
at v
A
3.8
-1.52
at v
A
4.4
-1.76
WARNING
Rev. 8 01-Dec-2010
With Flaps in T/O
at v
NE
or LDG Position
3.8
0
With Flaps in T/O
at v
NE
or LDG Position
4.4
-1
EASA
Doc. # 6.01.01-E
approved
DA 40 AFM
2.0
2.0