What was found
INSPECTION TYPE:C E/E COMPT STA400 FRAME INNER CHORD FOUND CRACKED AT S44L, CRACK LENGTH 5/8". E/E COMPT BS 400 FRAME INNER CHORD AT ABOVE STR 44L AREA REPAIRED AS PER SRM 51-40-04 FIG 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C E/E COMPT STA400 FRAME INNER CHORD FOUND CRACKED AT S44L, CRACK LENGTH 5/8". E/E COMPT BS 400 FRAME INNER CHORD AT ABOVE STR 44L AREA REPAIRED AS PER SRM 51-40-04 FIG 3.