What was found
AT C-CHECK, CRACK IN FRAME AT STA 203.8, APPROX RBL 18. ACCOMPLISHED HFEC, NO NEW CRACKS, CRACK FROM PREVIOUS STOP DRILL. INSTALLED ANGLE DOUBLER PER SRM 51-40-4, 16 INCHES LONG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, CRACK IN FRAME AT STA 203.8, APPROX RBL 18. ACCOMPLISHED HFEC, NO NEW CRACKS, CRACK FROM PREVIOUS STOP DRILL. INSTALLED ANGLE DOUBLER PER SRM 51-40-4, 16 INCHES LONG.