What was found
PIT - SKIN CRACKED .25 INCH, STA 380 STR 8 AND STR 9 RT OVERHEAD ATTACH POINT. INSTALLED .045 INCH ANGLE DOUBLER PER TYPICAL REPAIR 53-10-14. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PIT - SKIN CRACKED .25 INCH, STA 380 STR 8 AND STR 9 RT OVERHEAD ATTACH POINT. INSTALLED .045 INCH ANGLE DOUBLER PER TYPICAL REPAIR 53-10-14. (X)