What was found
PIT - DURING Q-1 CHECK INSPECTION, FOUND A 2 INCH CRACK AT VERTICAL STAB ATTACH ANGLE RT SIDE AFT END OF DRAG ANGLE. INSTALLED EXTERNAL DOUBLER PER SRM 53-05 FIG 23 AND 23A. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - DURING Q-1 CHECK INSPECTION, FOUND A 2 INCH CRACK AT VERTICAL STAB ATTACH ANGLE RT SIDE AFT END OF DRAG ANGLE. INSTALLED EXTERNAL DOUBLER PER SRM 53-05 FIG 23 AND 23A. (M)