What was found
EXFOLIATION CORROSION BS 674 BETWEEN LONGERON 30 RT AND 29 RT AT FUSELAGE SKIN. REPAIR FUSELAGE SKIN AT BS 674 BETWEEN LONGERON 30 RT AND 29 RT WAS ACCOMPLISHED IAW ER/A 541626-14, REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXFOLIATION CORROSION BS 674 BETWEEN LONGERON 30 RT AND 29 RT AT FUSELAGE SKIN. REPAIR FUSELAGE SKIN AT BS 674 BETWEEN LONGERON 30 RT AND 29 RT WAS ACCOMPLISHED IAW ER/A 541626-14, REV ORIGINAL.