What was found
CRACK WAS FOUND IN THE FUSELAGE SKIN AT BS 540 AND JUST BELOW LAP SPLICE AT S-14L. INSTALLED DOUBLER PER ER/A 451595-14AD AND SRM 53-30-3. REF AD 2004-18-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK WAS FOUND IN THE FUSELAGE SKIN AT BS 540 AND JUST BELOW LAP SPLICE AT S-14L. INSTALLED DOUBLER PER ER/A 451595-14AD AND SRM 53-30-3. REF AD 2004-18-06.