What was found
DURING A-CHECK INSP, CRACKS WERE FOUND ON LT AND RT SIDE PANELS IN THE NLG WW AREA OF LT PANEL: THE CRACK WAS LOCATED BETWEEN BS260 AND 280, WL 150, AND THE CRACK LENGTH WAS APPROX 2.0 INCHES (FIG 1). RT PANEL: THE CRACK WAS LOCATED BETWEEN BS300 AND 320, WL 150, AND THE CRACK LENGTH WAS APPROX 8.0 INCHES (FIG 2). (REPAIRS WERE ACCOMPLISHED IAW PROPOSAL REPAIR (HKA-TLS-10-0019-01C), SRM 53-10-04, FIG 116 AND SR 1-1769325648 (FIG 3 AND 4) AND THEY WERE APPROVED BY FAA 8100-9 DATED 29 DEC, 2010 (FIG 5). IAW FAA FORM 8100-9, REPAIRS ARE TIME LIMITED REPAIR, AND NEED PERMANENT REPAIR AT 22,000 TFC IAW PART 3 OF EO 4753A458RB (REF SB 53A2562R2).)