What was found
CANTED FRAME BS 1510 CRACKED AT TAILCONE ALIGNMENT PIN AT 2 O'CLOCK. REPAIRED IAW PRI 546574-14, REV 1 AND COMPLIED WITH ER/A 546574-14, REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CANTED FRAME BS 1510 CRACKED AT TAILCONE ALIGNMENT PIN AT 2 O'CLOCK. REPAIRED IAW PRI 546574-14, REV 1 AND COMPLIED WITH ER/A 546574-14, REV ORIGINAL.