What was found
FOUND CRACK ON RIGHT WING I/B AFT FLAP LOWER SURFACE 5.000 UP FROM T/E; AND 17.000 O/B FROM I/B EDGE PUNCTURE MEASURES 0.625 IN DIAMETER AND IS LOCATED IN A NON CRITICAL AREA. EXCEEDS SRM LIMITS FOR THIS TYPE OF DAMAGE REF SRM 57-53-01-1A-2 4. (4). PICTURES ATTACHED / [01] MEASUREMENTS ADDED;[02] PUNCTURE MEASURES 0.625? IN DIAMETER AND IS LOCATED IN A NON CRITICAL AREA. EXCEEDS SRM LIMITS FOR THIS TYPE OF DAMAGE REF SRM 57-53-01-1A-2 4. (4).<BR> <BR>COMPLIED WITH EA 22-157-03625. SPEED TAPE APPLIED. ACCOMPLISH A DETAILED VISUAL INSPECTION (DVI) OF THE DAMAGED AREA EVERY 8 CALENDAR DAYS. WITHIN 30 CALENDAR DAYS; ACCOMPLISH PERMANENT REPAIR PER THE APPLICABLE SRM SECTION OR REMOVE AND REPLACE THE DISCREPANT R/H INBOARD T.E. AFT FLAP.<BR><BR>REF TSR: 2022009186