What was found
A 3.75 INCH CRACK IN LOWER SKIN OF LT HORIZONTAL STABILIZER NR 2 BALANCE BOARD ACCESS PANEL. INSTALLED DOUBLER PER SRM 55-20-3 FIG 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 3.75 INCH CRACK IN LOWER SKIN OF LT HORIZONTAL STABILIZER NR 2 BALANCE BOARD ACCESS PANEL. INSTALLED DOUBLER PER SRM 55-20-3 FIG 5.