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2nd Nov 2007, 23:49

#5 (permalink)

Short_Circuit

Join Date: Sep 2007

Location: Up left - Down right

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Please do not hang me on this one, however, from what I understand
as a non Airbus Avionic LAME is.

There are 3 ailerons per wing outboard of the flaps.
Each has 2 sources of power, hyd – hyd or hyd – elect/hyd (act with an elect pump generating it’s own internal Hyd power.
Each segment driven by dedicated actuator, commanded by a dedicated Flight Control Computer Primary & Secondary (PRIM 1,2 or 3 & SEC1, 2 or 3).
If one surface fails to operate correctly the other 2 can compensate by moving more or less to keep normal feel & control.

With all ailerons on the end of the wings, flight control inversion is probably of great concern, hence 3 separate control surfaces that
are able to modify their control output.

I would love to do a course, sounds like a cleaver A/C.

Can someone lend me $30,000.00 for the bond.

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