Diamond DA20-C1 - 2.10. MANEUVERING LOAD FACTORS

DA20-C1 Flight Manual Limitations
Doc # DA202-C1 April 16, 2009 Page 2 - 8
Revision 24 DOT Approved
2.10. MANEUVERING LOAD FACTORS
Table of structural maximum permissible load factors:
at v
A
: at v
NE
:
with flaps in
T/O or LDG
position
Positive
+ 4.4 + 4.4 + 2.0
Negative
- 2.2 - 2.2 0
WARNING
EXCEEDING THE MAXIMUM LOAD FACTORS WILL RESULT IN
OVERSTRESSING OF THE AIRPLANE. SIMULTANEOUS FULL
DEFLECTION OF MORE THAN ONE CONTROL SURFACE CAN
RESULT IN OVERSTRESSING OF THE STRUCTURE, EVEN AT
SPEEDS BELOW THE MANEUVERING SPEED.