What was found
RIGHT FUSELAGE SURFACE APPROX BS 2154, WHERE ACCESS PANEL NR 347DF CONTACTS WITH FUSELAGE SKIN FOUND CORRODED. REPAIRED IAW SRM 53-70-01, FIG 201, REPAIR 3, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FUSELAGE SURFACE APPROX BS 2154, WHERE ACCESS PANEL NR 347DF CONTACTS WITH FUSELAGE SKIN FOUND CORRODED. REPAIRED IAW SRM 53-70-01, FIG 201, REPAIR 3, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.