What was found
DURING "L" CHECK FOUND CORROSION ON FUSELAGE SKIN AT BS 889 S27L. REPAIRED PER EA 55-215350 SECT I SECTION II REQUIRES DTA ANALYSIS AND APPROVAL FROM BOEING NO LATER THAN MAY 9, 2010.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING "L" CHECK FOUND CORROSION ON FUSELAGE SKIN AT BS 889 S27L. REPAIRED PER EA 55-215350 SECT I SECTION II REQUIRES DTA ANALYSIS AND APPROVAL FROM BOEING NO LATER THAN MAY 9, 2010.