What was found
MAIN CABIN UPPER LOBE FUSELAGE FRAME AT STA.400 BETWEEN S-8R AND S-9R HAS CRACK AT I/B FASTENER HOLE FOR AC OUTLET EXTRUSION SUP PORT BRACKET (REPAIR PER W/C SEQ#1655 FIG 3 STEP 9). REMOVED DAMAGED SECTION OF FRAME AND INSTALLED REPAIR CHANNELS P ER EC/RA#5310-07619,REV.A,PART 1. INITIATED DIP TO "ACCOMPLISH I NSPECTION REQUREMENTS ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERING AFTER 43,00 0 TOTAL FIGHT CYCLES BUT BEFORE 44,000 TOTAL FLIGHT CYCLES FOR I NSPECTION REQUIREMENTS".SEE FLEET CYCLE L/P9666849 FOR ALL WORK ACCOMPLISHED. TOMC APPROVED, PLACE ON DIP TOMC-APPROVAL FROM SC1ELBYC COMMENT INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE. VERIFIED EC/RA 5310-07619 REV.A PART 1 COMPLETED AND DIP ISSUED REVIEWED QC REVIEW QC REVEIWED QC REVIEW