What was found
INSPECTION FOUND SEVERAL .75 INCH CRACKS IN LT VERTICAL STABILIZER ATTACH ANGLE ABOVE CANTED STA 1463. THE CRACKED AREAS WERE CUT OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 23.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND SEVERAL .75 INCH CRACKS IN LT VERTICAL STABILIZER ATTACH ANGLE ABOVE CANTED STA 1463. THE CRACKED AREAS WERE CUT OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 23.