What was found
ANGLE CRACKED AT FS 424 NEXT TO RT FWD WING TO FUSELAGE ATTACH FITTING. REMOVED THE ANGLE IAW SRM 51-42-06 AND 51-42-21. INSTALLED REPAIRED ANGLE IAW SRM 51-42-06 & 51-42-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ANGLE CRACKED AT FS 424 NEXT TO RT FWD WING TO FUSELAGE ATTACH FITTING. REMOVED THE ANGLE IAW SRM 51-42-06 AND 51-42-21. INSTALLED REPAIRED ANGLE IAW SRM 51-42-06 & 51-42-21.