What was found
R/H H/S I/B L/E ASSY UPPER RIB END CRACKED AT XFS 66.250 . STOP DRILLED CRACK AND FABRICATED REPAIR PARTS IAW SM 55-2-0. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR PARTS IAW SRM 55-2-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
R/H H/S I/B L/E ASSY UPPER RIB END CRACKED AT XFS 66.250 . STOP DRILLED CRACK AND FABRICATED REPAIR PARTS IAW SM 55-2-0. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED REPAIR PARTS IAW SRM 55-2-0.