What was found
CRACK INDICATION FOUND DURING X-RAY INSPECTION AT STA 6-100, LONGERON 1R AFT SECTION EDGE, CRACK LENGTH APPROX 0.5 INCH. REPAIRED AS PER SRM 53-10-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK INDICATION FOUND DURING X-RAY INSPECTION AT STA 6-100, LONGERON 1R AFT SECTION EDGE, CRACK LENGTH APPROX 0.5 INCH. REPAIRED AS PER SRM 53-10-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.