What was found
L/W O/B AFT FLAP; I/B AFT CORNER DISBONDED<[01] FINAL STATEMENT: REMOVED DAMAGE DELAMINATED UPPER AND LOWER SKINS ON L/W O/B AFT FLAP WEDGE I/B CORNER AS PER B737 SWRM 51-70-10-2R-4. PARAG. (7-A-1). INSTALLED HOT BONDER PERMANENT REPAIR AT L\W O\B AFT FLAP ON I\B CORNER UPPER AND LOWER SURFACE PER B737 SRM 57-53-01-2R-14 AND B737 SRM 51-70-10-2R-0PARAGRAPH (20.B) MATERIAL USED FIM ADHES AF 163-2K-06 PO#2053056 AND TOOL USED TEMPERATURE CONTROL ID:170006 DUE DATE 6/1/24.;[02] VERIFIED STEP 1;[03] CORRECTION: UPDATE MEASUREMENT TABLE