As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BS 1510 FRAME IS CRACKED AT 4:30 POS AT TAIL CONE ALINGMENT PIN--CRACKED EMPENNAGE (HFEC-M-). NR 128: REPAIRED IAW ERA 511420-14, REV ORIGINAL BY FRAME SECTION REPLACEMENT. WORK ACCOMPLISHED ON PRI 511420-14 REV O COINCIDES WITH FINAL ER/A 511420-14, REV ORIGINAL.