What was found
EXTERNAL FUSELAGE SKIN HAS A PREVIOUS BLEND AT BS 380+14",3.0" ABOVE STRINGER 23 R/H. / PREVIOUS BLEND ON EXTERNAL FUSELAGE SKIN AT BS 380+14" 3.0" ABOVE STRINGER 23 R/H REPAIRED IAW EA 1-753-36551 REV IR AND ATS ER 20-01538 REV IR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXTERNAL FUSELAGE SKIN HAS A PREVIOUS BLEND AT BS 380+14",3.0" ABOVE STRINGER 23 R/H. / PREVIOUS BLEND ON EXTERNAL FUSELAGE SKIN AT BS 380+14" 3.0" ABOVE STRINGER 23 R/H REPAIRED IAW EA 1-753-36551 REV IR AND ATS ER 20-01538 REV IR.