What was found
TAIL INTERIOR, AFT CANTED FRAME BS 1510 HAS .5" CRACK AT TAIL CONE ALIGNMENT PIN, 8 O`CLOCK. REPAIRED IAW ERA497316-14MA, REV ORIGINAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL INTERIOR, AFT CANTED FRAME BS 1510 HAS .5" CRACK AT TAIL CONE ALIGNMENT PIN, 8 O`CLOCK. REPAIRED IAW ERA497316-14MA, REV ORIGINAL.