What was found
FUSELAGE SKIN CRACKED AT BS 1475, 3 INCHES RT OF VERTICAL STABILIZER/TAIL. CUTOUT DAMAGE, INSTALLED DOUBLER, TRIPLER AND LONGERON SPLICE IAW PRI 522196, REV O AND FINAL ERA 5221914, REV O.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACKED AT BS 1475, 3 INCHES RT OF VERTICAL STABILIZER/TAIL. CUTOUT DAMAGE, INSTALLED DOUBLER, TRIPLER AND LONGERON SPLICE IAW PRI 522196, REV O AND FINAL ERA 5221914, REV O.