What was found
AT C CK, RT WING - WING TO FUSELAGE FILLET SUPPORT ANGLE CRACKED (2 INCHES) AT XW 908-XCW 69.5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C CK, RT WING - WING TO FUSELAGE FILLET SUPPORT ANGLE CRACKED (2 INCHES) AT XW 908-XCW 69.5.