What was found
LEFT FWD VERTICAL STAB, AFT DRAG ANGLE IS CRACKED. CUT OUT THE DAMAGE, FABRICATED A REPAIR, AND INSTALLED IAW REO 670-55-31-098, REO 670-55-31-018, REV A, AND SRM 51-25-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT FWD VERTICAL STAB, AFT DRAG ANGLE IS CRACKED. CUT OUT THE DAMAGE, FABRICATED A REPAIR, AND INSTALLED IAW REO 670-55-31-098, REO 670-55-31-018, REV A, AND SRM 51-25-01.