What was found
FUSELAGE FRAME AT STA 236 WAS FOUND TO BE CRACKED AT THE END OF A PREVIOUS REPAIR. REMOVED THE PREVIOUS REPAIR, EXTENDED THE CUT OUT TO REMOVE THE CRACK. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME AT STA 236 WAS FOUND TO BE CRACKED AT THE END OF A PREVIOUS REPAIR. REMOVED THE PREVIOUS REPAIR, EXTENDED THE CUT OUT TO REMOVE THE CRACK. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)