What was found
TAIL INTERIOR - CANTED FRAME RT WEB IB EDGE HAS 1.2500" LONG CRACK AT HORIZONTAL "T" ANGLE, BS 1485, NEAR RUDDER TRIM CABLE DRUM. REPAIRED CANTED FRAME REF SRM 53-03D, FIG 49.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL INTERIOR - CANTED FRAME RT WEB IB EDGE HAS 1.2500" LONG CRACK AT HORIZONTAL "T" ANGLE, BS 1485, NEAR RUDDER TRIM CABLE DRUM. REPAIRED CANTED FRAME REF SRM 53-03D, FIG 49.