What was found
REPAIRED AREA OF CORROSION TO FUSELAGE SKIN UNDERWING TO BODY PANEL BS 655, STRINGERS 28-26 WITH EXTERNAL REPAIR DOUBLER PER J2 ENGINEERING ORDER J2EO17-MAS-S040717, REV. 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
REPAIRED AREA OF CORROSION TO FUSELAGE SKIN UNDERWING TO BODY PANEL BS 655, STRINGERS 28-26 WITH EXTERNAL REPAIR DOUBLER PER J2 ENGINEERING ORDER J2EO17-MAS-S040717, REV. 5.