What was found
FUSELAGE EXTERNAL SKIN AT LT BS 2390 - 2400, STRINGER 50 - 51, EXISTING BLEND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 REV 96. PERFORMED DOUBLER REPAIR IAW SRM 53-00-01 REPAIR 1 DETAIL 3 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERNAL SKIN AT LT BS 2390 - 2400, STRINGER 50 - 51, EXISTING BLEND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 REV 96. PERFORMED DOUBLER REPAIR IAW SRM 53-00-01 REPAIR 1 DETAIL 3 FIG 201.