What was found
DELAMINATION ON OTBD AFT FLAP, LT WING. APPLIED BONDING PRIMER ON REPAIR LOWER AREA IAW SRM 57-53-01-2R-16, REPAIR 16, PARAGRAPH 4.H(1), SRM 51-70-10-2R-0, REPAIR GENERAL, PARAGRAPH 15. PERFORMED INTERIM REPAIR ON O/B AFT FLAP AT LT WING IAW SRM 57-53-01-2R-16, REPAIR 16. PERFORMED TAP TEST INSPECTION EVERY 6875 FLIGHT CYCLES OR 30 MONTHS WICHEVER COMES FIRST.