What was found
ATTACH ANGLE CRACKED BETWEEN FUSELAGE SKIN AND LEFT AFT ADF PANEL SUPPORT FR -756 JUST BELOW LONGERON 20 LEFT. REPLACED CRACKED ANGLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ATTACH ANGLE CRACKED BETWEEN FUSELAGE SKIN AND LEFT AFT ADF PANEL SUPPORT FR -756 JUST BELOW LONGERON 20 LEFT. REPLACED CRACKED ANGLE.