What was found
INSPECTION FOUND FUSELAGE SKIN NICKED AT BS 626, S3L. A FLUSH REPAIR WAS INSTALLED IAW SRM 53-00-01, REPAIR 2, FIGURE 202.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN NICKED AT BS 626, S3L. A FLUSH REPAIR WAS INSTALLED IAW SRM 53-00-01, REPAIR 2, FIGURE 202.