What was found
C CHECK 1, PREVIOUS BLEND OUT ON FUSELAGE SKIN LAP JOINT AT STRINGER 29R, BETWEEN FRAME 20 & 21. REPAIRED SKIN IAW SRM 53-00-201 PARA 4AA FIG 247.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C CHECK 1, PREVIOUS BLEND OUT ON FUSELAGE SKIN LAP JOINT AT STRINGER 29R, BETWEEN FRAME 20 & 21. REPAIRED SKIN IAW SRM 53-00-201 PARA 4AA FIG 247.