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REFLECTOR: Bearing AD (Duane Swing)
Duane has email working now. I'll add him to the reflector
list so his email won't bounce anymore.
Forwarded message:
> -----Original Message-----
> From: Duane Swing
> Sent: Monday, January 11, 1999 11:36 AM
> To: 'Michalk@awpi.com'
> Subject: FW: front bearing questions
>
>
>
> -----Original Message-----
> From: Duane Swing
> Sent: Friday, January 08, 1999 9:56 AM
> To: 'reflector@awpi.com'
> Subject: front bearing questions
>
> To all Reflectorites:
> Scott and I have been looking at the front bearing support and are
> working on a solution. One of the problems that any wide area washer type
> retainer or the reversal of the bearing in the holder, or even the
> replacement of the countersink screws with standard flat head screws, is
> that unless the control stick is restricted from being pulled back further
> than the full down elevator will allow (26 degrees) the possibility of a
> total bearing failure or the attach aluminum bracket breaking as a result
> of constant flexing is still an issue. It would be my initial thought that
> the control stick full aft movement should be restricted by placing an
> aluminum stop on the keel where the control stick would normally contact
> the aft end of the control stick hole when fully deflected. On all the
> airplanes we have built, the total available movement of the control stick
> was always determined by the control stick contacting the fiberglass keel
> once the 26 degree down elevator was reached. This does not eliminate all
> the loads on the bearing but does prevent "excessive" loads as a result of
> the elevator reaching it's maximum 26 degrees with still another 5 degrees
> or so of stick travel available to the pilot. This added pressure is what
> can cause the bearing, attach bracket or screws to fail in time.
> This is at this time just some thoughts on the subject. We will
> continue to monitor the Reflector for answers and solutions to this
> problem.
> Sincerely, Duane Swing Velocity Inc.
> [Duane Swing] This message was originally sent on January 11th. My
> computer e-mail server was holding all my e-mail for some reason and
> nothing has been going out since December. Sorry for all the delays in
> answering those of you who have been asking about the AD on the front
> bearing. Everyone should also be aware that no standard ball bearing is
> designed for heavy for/aft thrust loads that we have all been talking
> about. Adding wide area washers and other means of bearing retention is
> NOT the total answer. We tested the round head screw (AD note) and found
> it takes at least 800 lbs. of load before anything happens and then the
> flange ring around the bearing failed leaving the screws intact and
> virtually destroyed the attach bracket. Reversing the bearing in the
> bracket is certainly a good idea if the airplane is not already built but
> is not necessary assuming some other means of restricting the aft load on
> the control stick is made.
> Sincerely, Duane Swing
>
--
Brian Michalk <http://www.awpi.com/michalk>
Life is what you make of it ... never wish you had done something.
Aviator, experimental aircraft builder, motorcyclist, SCUBA diver
musician, home-brewer, entrepenuer and SINGLE!