What was found
DURING C-CHECK, FOUND VERTICAL STAB TO FUSELAGE EXTERIOR ATTACH ANGLE CRACKED ON LT SIDE APPROX 8 INCH FROM AFT END. INSTALLED DOUBLER REPAIR IAW SRM 53-05 FIG 23.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND VERTICAL STAB TO FUSELAGE EXTERIOR ATTACH ANGLE CRACKED ON LT SIDE APPROX 8 INCH FROM AFT END. INSTALLED DOUBLER REPAIR IAW SRM 53-05 FIG 23.