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Thanks very much Steve.
Much appreciated.
Steve
> On 9 Jan 2025, at 3:31 pm, Steven W. Boese SBoese@uwyo.edu <flyrotary@lancaironline.net> wrote:
>
> Steve,
>
> I didn’t see the cracks prior to disassembly and doubt that they could have been seen on the counterweight side very well -if at all- when assembled.
>
> I replaced the Flexplate with a steel flywheel about a year ago. Since then, I replaced the four rubber dampers with machined aluminum discs giving a solid connection and then dynamically balanced the system. This was done because maintaining a dynamic balance wasn’t possible with the dampers. Only a few hours of flight have occurred in this configuration so far and there has been no indication of problems resulting from this change.
>
> Steve Boese
>
>> On Jan 8, 2025, at 11:03 PM, Stephen Izett stephen.izett@gmail.com <flyrotary@lancaironline.net> wrote:
>>
>> ◆ This message was sent from a non-UWYO address. Please exercise caution when clicking links or opening attachments from external sources.
>>
>>
>> Hi Steve
>>
>> Is this recent then?
>>
>> I’m not able to get to my aircraft at present to check my flex plate which has probably seen 50 hours of service.
>>
>> Was it possible to see these cracks assembled?
>>
>> I would appreciate your reflections on Tracys latter choice to remove the damper, and particularly when using a timber/glass prop such as an MT.
>>
>> It would be great to have an update and current info from Tracy regarding his no damper hours if anyone can contact him.
>>
>> Very helpful, thanks again Steve
>>
>> Steve
>
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