What was found
AFT L/H UPPER FUSELAGE AT STA 1088 LEFT VERTICAL PRIMARY ATTACH FITTING ON AIRCRAFT SIDE FORWARD DRAG ANGLE FITTING CORRODED IN BORE. / R&R DRAG ANGLE IAW DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT L/H UPPER FUSELAGE AT STA 1088 LEFT VERTICAL PRIMARY ATTACH FITTING ON AIRCRAFT SIDE FORWARD DRAG ANGLE FITTING CORRODED IN BORE. / R&R DRAG ANGLE IAW DWG.