What was found
DISCOVERED FUSELAGE SKIN CRACK AT BS 882 AND STRINGER 24R. APPROXIMATELY 3.5 INCHES IN LENGTH. HFEC CONFIRMED CRACK. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DISCOVERED FUSELAGE SKIN CRACK AT BS 882 AND STRINGER 24R. APPROXIMATELY 3.5 INCHES IN LENGTH. HFEC CONFIRMED CRACK. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M)