AIRPLANE
FLIGHT
MANUAL
PERFORMANCE
ANAC APPROVED 5-01
REVISION 8 code 01 Page 21
AFM-1385
The effect of the overspeed required by AFM procedures for landing in
emergency or abnormal configurations has been already taken into
account in the landing distance factors therein presented. Therefore,
the CAFM V
REF
OVERSPEED feature is not to be used for calculation
of the landing performance for the AFM emergency or abnormal
cases, due to the different airplane configurations involved.
DEMONSTRATED CROSSWIND
The maximum demonstrated crosswind component for takeoff and
landing is 28 kt. This maximum demonstrated value is not considered
to be limiting.
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