What was found
FUSELAGE LH #3 WINDOW FRAME E-F, G-H POST AND E-G UPPER SILL WERE REPAIRED AT GYR. REPAIR IS A PERMANENT SOLUTION WITH INSPECTION REQUIREMENTS. ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF LATEST REVISION OF EC/RA 5610 -01548 ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES. AIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES." NOTE: PART 2, BEFORE THE SUBJECT AIRCRAFT REACHES THE NOTED THRESHOLD. INSPECTION REQUIREMENTS 1. TO BE DETERMINED BY ENGINEERING DIP INITIATED TO ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF LATEST REVISION OF EC/RA 5610 -01548 ON OR BEFORE THE TOMC APPROVED FOR DIP ACCOMPLISH INSPECTION REQUIREMENTS PER TOMC-APPROVAL FROM SC1ELBYC COMMENT PART 2 OF LATEST REVISION OF EC/RA 5610 -01548 ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES." PER ECRA 5610-01548 PART 1-INTERIM REPAIR OF ECRA 5610-01548 WAS ACCOMPLISHED IN GYR UPDATED TO INCLUDE SDR REQUIREMENT AND MAJOR REPAIR. REF EO5310-24023.