What was found
RT FUSELAGE HAS CHAFING DAMAGE AT AFT WING TO FUSELAGE POINT UNDER FLAP STUB FAIRING. BLENDED RT FUSELAGE AFT WING TO FUSELAGE DOES NOT EXCEED ALLOWABLE LIMITS IAW 601R-53-45-1215.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT FUSELAGE HAS CHAFING DAMAGE AT AFT WING TO FUSELAGE POINT UNDER FLAP STUB FAIRING. BLENDED RT FUSELAGE AFT WING TO FUSELAGE DOES NOT EXCEED ALLOWABLE LIMITS IAW 601R-53-45-1215.