What was found
FUSELAGE EXTERIOR CORROSION, POST CLEAN UP EXCEED LIMITS. REPAIRED PER SRM 53-20-03 FIG 1 CAT B REPAIR DUE INSPECTION AT (THRESHOLD) 15,000 CYCLES LFEC.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERIOR CORROSION, POST CLEAN UP EXCEED LIMITS. REPAIRED PER SRM 53-20-03 FIG 1 CAT B REPAIR DUE INSPECTION AT (THRESHOLD) 15,000 CYCLES LFEC.