What was found
SUSPECTED CRACK ON AFT DRAG ANGLE. INSPECTED AFT DRAG ANGLE IAW REO690-52-11-026 REV B. NO FURTHER DAMAGE NOTICED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SUSPECTED CRACK ON AFT DRAG ANGLE. INSPECTED AFT DRAG ANGLE IAW REO690-52-11-026 REV B. NO FURTHER DAMAGE NOTICED.