What was found
FUSELAGE - BS 1860-1880, S-41-42L SKIN CRACK REPAIR. REPAIRED PER SRM 53-30-00 FIG 1, DETAIL 1. REPEAT REQUIREMENT: PERMANENT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE - BS 1860-1880, S-41-42L SKIN CRACK REPAIR. REPAIRED PER SRM 53-30-00 FIG 1, DETAIL 1. REPEAT REQUIREMENT: PERMANENT.