What was found
C5 PDX - RIGHT DRAG STRUT INBOARD ATTACH POINT IS CHAFED. REPAIRED IAW SRM 51-20-26.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C5 PDX - RIGHT DRAG STRUT INBOARD ATTACH POINT IS CHAFED. REPAIRED IAW SRM 51-20-26.