What was found
PIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK AT RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE STA 1087. INSTALLED DOUGLAS PER SRM 53-05 FIG 23B. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-4 CHECK, FOUND 1.5 INCH CRACK AT RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE STA 1087. INSTALLED DOUGLAS PER SRM 53-05 FIG 23B. (M)