Second and final pass of Port top wingskin bond on 5.
Date: 09/13/2010
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EAA SITE
Date: 08/23/2023
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The fuel flow transmitter was relocated such that it would be level when when the aircraft was level and the wires are up. There should be sufficient area fore and aft to allow a straight run into and out of the sensor.
The holes previously poked in the firewall for various applications and now no longer required were filled. The big "heater" hole will be closed with a stainless steel plate. SS on order from ACS.