What was found
CRACK FOUND AFTER HFEC INSPECTION OF WINDOW L1 PER AVO # 284-19- 10-26-02 (CRACK CONDITION 1). CRACK FOUND AFTER HFEC INSPECTION OF WINDOW L1 HAS BEEN REPAIRED PER EC/RA # 5311-02301. INITIATE A DTA DIP FOR THE L1 WINDOW FRAME REPAIR TO " ACCOMPLISH AN INITIAL INSPECTION PER PART 2, SECTION A ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISH REPETITIVE INSPECTIONS PER PART 2, SECTION A AT INTERVALS NOT TO EXCEED 18,000FLIGHT CYCLES BEFORE THE AIRCRAFT REACHING 50,000 TOTAL AIRCRAFT FLIGHT CYCLES "ACCOMPLISH AN INITIAL INSPECTION PER PART 2, SECTION B ON OR THEREAFTER." INITIATE A DTA DIP FOR L1 WINDOW FRAME REPAIR TO ACCOMPLISH REPETITIVE INSPECTIONS PER PART 2, SECTION B AT INTER VALS NOT TO EXCEED 36,000 FLIGHT CYCLES THEREAFTER." SEE FLEET CYCLE N/R # 9708685 FOR WORK PERFORMED. ?ACCOMPLISH AN INITIAL INSPECTION PER PART 2, SECTIONS A AND B ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISH REPETITIVE INSPECTIONS PER PART 2, SECTION A HFEC AT INTERVALS NOT TO EXCEED 18,000 FLT CYCLES AND PART 2 SEC B LFEC AT INTERVALS NOT TO EXCEED 36,000 FLT CYCLS THEREAFTER.? OK TO INITIATE DTA DIP FOR THE L1 WINDOW FRAME REPAIR TO TOMC-APPROVAL FROM SC1ELBYC COMMENT ADDING ECRA REFERENCE 5311-02301 FOR DIP ADDING ECRA REFERENCE 5311-02302 FOR DIP INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. VERIFIED ALL PAPER WORK IS CORRECT AND ACCOUNTED FOR QC REVIEWED QC REVIEWED