What was found
TAIL INTERIOR, CANTED FRAME WEB HAS 4" LONG CRACK, CBS 1485, APPROXIMATELY 8 O`CLOCK POSITION. REPAIRED IAW PRI 550919-14, REV 0 AND ERA 550919-14, REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL INTERIOR, CANTED FRAME WEB HAS 4" LONG CRACK, CBS 1485, APPROXIMATELY 8 O`CLOCK POSITION. REPAIRED IAW PRI 550919-14, REV 0 AND ERA 550919-14, REV ORIGINAL.