What was found
R/H I/B (#6) AFT FLAP FAIRING TAIL CONE IS DELAMINATED R/H I/B (#5) AFT FLAP FAIRING TAIL CONE IS DELAMINATED<[01] REMOVED AND REPLACED PER [AMM 27-51-18-400-802-NG (INBOARD FLAP SUPPORT AFT FAIRING INSTALLATION - PERMANENT)]
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
R/H I/B (#6) AFT FLAP FAIRING TAIL CONE IS DELAMINATED R/H I/B (#5) AFT FLAP FAIRING TAIL CONE IS DELAMINATED<[01] REMOVED AND REPLACED PER [AMM 27-51-18-400-802-NG (INBOARD FLAP SUPPORT AFT FAIRING INSTALLATION - PERMANENT)]