What was found
AT FS280.00 UPPER FUSELAGE STR 3 HAS CRACK. REMOVED CRACKED O/B ANGLE CLIP AND INSTALLED NEW ANGLE CLIP AT STGR 3L FS280 IAW SRM 51-42-06 AND 51-42-21 NDT VERIFIED NO CRACK IN LONGERON STGR 3L.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT FS280.00 UPPER FUSELAGE STR 3 HAS CRACK. REMOVED CRACKED O/B ANGLE CLIP AND INSTALLED NEW ANGLE CLIP AT STGR 3L FS280 IAW SRM 51-42-06 AND 51-42-21 NDT VERIFIED NO CRACK IN LONGERON STGR 3L.