What was found
TAIL INTERIOR, AFT CANTED FRAME AT BS 1510 HAS .5 INCH LONG CRACK AT CONE ALIGN PIN, 11:30 O`CLOCK POSITION. REPAIRED IAW PRI 538315-14, REV "0" AND ER/A 538315-14, REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL INTERIOR, AFT CANTED FRAME AT BS 1510 HAS .5 INCH LONG CRACK AT CONE ALIGN PIN, 11:30 O`CLOCK POSITION. REPAIRED IAW PRI 538315-14, REV "0" AND ER/A 538315-14, REV ORIGINAL.