What was found
CRACK FOUND APPROX 1.0" ON FUSELAGE WEB AFT LOWER CORNER RADIUS. STA 909 BL 20L WL 50. AS MARKED. REPAIR ON FUSELAGE WEB L/H AFT LOWER CORNER IAW EO C550-53MIR-002-O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND APPROX 1.0" ON FUSELAGE WEB AFT LOWER CORNER RADIUS. STA 909 BL 20L WL 50. AS MARKED. REPAIR ON FUSELAGE WEB L/H AFT LOWER CORNER IAW EO C550-53MIR-002-O