What was found
AREA OF CORROSION ON FORWARD AND AFT END OF PANEL BOTTOM OF FUSELAGE BETWEEN NR 1 AND NR 3 ACM ACCESS DOORS (LEVEL 1). REMOVED CORROSION, ALODINED AND PAINTED AS PER BOEING 747 SRM 51-10-01, PAGES 13, 14, 15, PARAGRAPH 6 AND 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AREA OF CORROSION ON FORWARD AND AFT END OF PANEL BOTTOM OF FUSELAGE BETWEEN NR 1 AND NR 3 ACM ACCESS DOORS (LEVEL 1). REMOVED CORROSION, ALODINED AND PAINTED AS PER BOEING 747 SRM 51-10-01, PAGES 13, 14, 15, PARAGRAPH 6 AND 7.