What was found
AT MAJOR INSPECTION FOUND CRACK AT BOLT ATTACH ON FRAME P/N 206-032-308-103. SUBMITTER STATED T.B. 206L-94-169 WAS ISSUED TO REDUCE CRACKING OF FRAME P/N 206-032-308-103. THIS IS NOT ADEQUATE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT MAJOR INSPECTION FOUND CRACK AT BOLT ATTACH ON FRAME P/N 206-032-308-103. SUBMITTER STATED T.B. 206L-94-169 WAS ISSUED TO REDUCE CRACKING OF FRAME P/N 206-032-308-103. THIS IS NOT ADEQUATE.