What was found
THERE IS A .50 CRACK IN THE REAR SPAR VERTICAL PRESSURE WEB AT WL 195.6 AND RBL 41.5. REPAIRED IAW SRM 57-10-10 REP 3 ALT 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THERE IS A .50 CRACK IN THE REAR SPAR VERTICAL PRESSURE WEB AT WL 195.6 AND RBL 41.5. REPAIRED IAW SRM 57-10-10 REP 3 ALT 2.