What was found
PIT - DURING Q-4 CHECK INSPECTION, FOUND 2 INCH CRACK IN DRAG ANGLE RADIUS RT VERTICAL STABILIZER. DRAG ANGLE STA 1089. INSTALLED REPAIR ANGLE PER SRM 53-05, FIGURE 23. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-4 CHECK INSPECTION, FOUND 2 INCH CRACK IN DRAG ANGLE RADIUS RT VERTICAL STABILIZER. DRAG ANGLE STA 1089. INSTALLED REPAIR ANGLE PER SRM 53-05, FIGURE 23. (X)