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dlm34077(at)gmail.com Guest
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Posted: Fri Apr 26, 2019 5:11 am Post subject: door pins |
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Aircraft TT is about 1400. Upon inspection I notice that the door pins are wearing a little from the opening and closing of the doors. pins wear as they exit the doors and engage the fuselage bulkhead. Current circumference of the pins are about .435-.437. what level of wear is acceptable? Has anyone inserted short aluminum rods near the ends to provide extra safety for a pin fracture?
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rjones560xl@gmail.com
Joined: 29 Jul 2015 Posts: 64 Location: Las Vegas, NV
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Posted: Fri Apr 26, 2019 7:01 am Post subject: door pins |
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You might consider going to the stainless door pins. They can be easily retrofitted by cutting off the ends of the aluminum rods and threading them on the inside. A threaded rod screws in (I used Red Loctite on it) them screw the new pins on the protruding threaded rod.
Robert Jones
Quote: | On Apr 26, 2019, at 06:04, dlm <dlm34077(at)gmail.com> wrote:
Aircraft TT is about 1400. Upon inspection I notice that the door pins are wearing a little from the opening and closing of the doors. pins wear as they exit the doors and engage the fuselage bulkhead. Current circumference of the pins are about .435-.437. what level of wear is acceptable? Has anyone inserted short aluminum rods near the ends to provide extra safety for a pin fracture?
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| - The Matronics RV10-List Email Forum - | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
http://www.matronics.com/Navigator?RV10-List |
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_________________ Robert J Jones
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