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04-26-2008, 06:37 AM
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Join Date: Jan 2007
Location: Picton, Ont., Ft. Myers, Fl
Posts: 294
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flap bearing mod...
I am the new owner of an RV-4 and my inspector here in Canada is asking me to modify the flap rod end bearing with a bolt and washer arrangement to prevent the bearing and housing from separating from each other. My a/c was assembled as per Van's drawings and I am reluctant to change. Is there any history of problems with a separation of this kind resulting in asymetric flap? I feel that as long as I inspect this bearing on a regular basis to check for looseness and wear, It should be safe.
I have asked Van's the same question.
Any comments appreciated. I have a PDF sketch of what he is asking me to do.
Dave
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Dave Main
Membership due Oct., 2020
RV-4 0-360-188 Catto 3-blade C-FTDQ...
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04-26-2008, 06:58 AM
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Join Date: Mar 2005
Location: Dallas area
Posts: 10,762
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No history of problems that I'm aware of.
__________________
Mel Asberry, DAR since the last century.
EAA Flight Advisor/Tech Counselor, Friend of the RV-1
Recipient of Tony Bingelis Award and Wright Brothers Master Pilot Award
USAF Vet, High School E-LSA Project Mentor.
RV-6 Flying since 1993 (sold)
<rvmel(at)icloud.com>
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04-26-2008, 09:17 AM
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Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 10,011
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Old question - easy solution
It is standard design practise to have large diameter capture washers to prevent a total loss of control actuation if a bearing should fail. The design is different in this area due to the use of a bearing with an integral stud.
The Canadians apparently inspect to a higher design standard than the US....
If fact, this question dates back to at least 1996 in Canada, and the fix is easy. See this old Matronics posting... hope the link works...
http://www.matronics.com/searching/g...HOWBUTTONS=YES
Other DARs in the US apparently also agree with the Canadians....
http://www.matronics.com/searching/g...HOWBUTTONS=YES
gil A
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Gil Alexander
EAA Technical Counselor, Airframe Mechanic
Half completed RV-10 QB purchased
RV-6A N61GX - finally flying
Grumman Tiger N12GA - flying
La Cholla Airpark (57AZ) Tucson AZ
Last edited by az_gila : 04-26-2008 at 09:32 AM.
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04-26-2008, 09:18 AM
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Join Date: Jan 2005
Location: Ontario, Canada
Posts: 1,544
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Dave
This has been a constant theme with canadian inspectors over the years. Ususally they just accept that the part is installed per plans and let it go. However it is no big deal to purchase a rod end bearing and use a 1/4" bolt with a capture washer installed. This may mean that you will need a slightly larger hole in the bottom of the fuselage to accomadate the bolt and washer.
__________________
Tom Martin RV1 pilot 4.6hours!
CPL & IFR rated
EVO F1 Rocket 1000 hours,
2010 SARL Rocket 100 race, average speed of 238.6 knots/274.6mph
RV4, RV7, RV10, two HRIIs and five F1 Rockets
RV14 Tail dragger
Fairlea Field
St.Thomas, Ontario Canada, CYQS
fairleafield@gmail.com
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04-26-2008, 05:38 PM
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Join Date: Jan 2007
Location: Picton, Ont., Ft. Myers, Fl
Posts: 294
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Thanks for the info, looks like a call to Van's on Monday for parts...
BTW, is there any down side to this mod other than having to enlarge the cavity in the fuse to accommodate?
Dave
__________________
Dave Main
Membership due Oct., 2020
RV-4 0-360-188 Catto 3-blade C-FTDQ...
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04-26-2008, 08:35 PM
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Join Date: Jan 2005
Location: Ontario, Canada
Posts: 1,544
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Dave
there is a good chance that you can drive in to Leavons and pick up the same parts, give them a call.
__________________
Tom Martin RV1 pilot 4.6hours!
CPL & IFR rated
EVO F1 Rocket 1000 hours,
2010 SARL Rocket 100 race, average speed of 238.6 knots/274.6mph
RV4, RV7, RV10, two HRIIs and five F1 Rockets
RV14 Tail dragger
Fairlea Field
St.Thomas, Ontario Canada, CYQS
fairleafield@gmail.com
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04-27-2008, 07:58 AM
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Join Date: Jan 2007
Location: Picton, Ont., Ft. Myers, Fl
Posts: 294
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parts
Thanks Tom, I will certainly do that.
Off to the a/p.
Dave
__________________
Dave Main
Membership due Oct., 2020
RV-4 0-360-188 Catto 3-blade C-FTDQ...
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