What was found
RIGHT I/B FLAP RIB STA XW. 130.000, CRACKED. STOP DRILLED CRACK PER SRM 57-2-5 FIG 2. FABRICATED REINFORCING ANGLE PER SRM 57-2-5 FIG 2. INSTALLED REINFORCING ANGLE PER SRM 57-2-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT I/B FLAP RIB STA XW. 130.000, CRACKED. STOP DRILLED CRACK PER SRM 57-2-5 FIG 2. FABRICATED REINFORCING ANGLE PER SRM 57-2-5 FIG 2. INSTALLED REINFORCING ANGLE PER SRM 57-2-5.