What was found
CRACK ON STRINGER 16L AT BS 500C +16" INTERNAL AREA PAX CABIN FUSELAGE. REPLACED STRINGER 16L LOCATED BETWEEN BS 500C+15" TO BS 540 IAW SRM B737-300 51-10-02 AND 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON STRINGER 16L AT BS 500C +16" INTERNAL AREA PAX CABIN FUSELAGE. REPLACED STRINGER 16L LOCATED BETWEEN BS 500C+15" TO BS 540 IAW SRM B737-300 51-10-02 AND 51-40-02.