What was found
FUSELAGE EXTERIOR SKIN HAD NUMEROUS NICKS & SCRATCHES BETWEEN STRINGERS 26L & 26R AT BS 600 - 620. BLENDED AND FOUND OUT OF LMITS IAW SRM 53-00-01 FIG.101 DETAIL II, REV.110. REPAIRED IAW EA 757-5331-08-08-E2502 REV-. REPAIR IS MAJOR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERIOR SKIN HAD NUMEROUS NICKS & SCRATCHES BETWEEN STRINGERS 26L & 26R AT BS 600 - 620. BLENDED AND FOUND OUT OF LMITS IAW SRM 53-00-01 FIG.101 DETAIL II, REV.110. REPAIRED IAW EA 757-5331-08-08-E2502 REV-. REPAIR IS MAJOR.