What was found
LEFT WING TO FUSELAGE, LOWER ATTACH ANGLE IS CRACKED AT FRAME 46. NEW ANGLE INSTALLED IAW ETN-EM-53-142.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING TO FUSELAGE, LOWER ATTACH ANGLE IS CRACKED AT FRAME 46. NEW ANGLE INSTALLED IAW ETN-EM-53-142.