What was found
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AND .5 INCH CRACK SKIN AT BS 380 BETWEEN BL 0 AND STRINGER 28L. INSTALLED DOUBLER, REPAIRED PER TR 53-30-04. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AND .5 INCH CRACK SKIN AT BS 380 BETWEEN BL 0 AND STRINGER 28L. INSTALLED DOUBLER, REPAIRED PER TR 53-30-04. (M)