Originally Posted by woodmanrog
We just finished our 1st Conditional Inspection at 150 hours on N199MJ. I'm happy to report everything looks like new except for this glitch with P/N FF-00003A (bottom cowl closeout). I would suggest using a doubler to strengthen this thin aluminum where the bracket is riveted. Happy New Year to our RV family from Roger and Myra.
Has this airplane had a dynamic propeller balance done?
This is the first instance of this that i am aware of.
The RV-14A prototype is approaching 900 Hrs and still has the original part installed.