What was found
BS 1354 RBL 116 WL 191 FUSELAGE FRAME INNER CHORD TO PRESSURE WEB ATTACH ANGLE CORRODED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
BS 1354 RBL 116 WL 191 FUSELAGE FRAME INNER CHORD TO PRESSURE WEB ATTACH ANGLE CORRODED.