What was found
FLAP TRACK # 2 FWD FAIRING 543AB HAS SOLID DELAMINATION @ EXTERIOR SKIN FASTENERS HOLES MKD DOT<[01] SUMMARY :PERFORMED PULSE-ECHO UT INSP FOR DELAMINATION.<BR>IAW B737 NDT PART 4; 51-00-01 & PART 1; 51-01-02.<BR>TOOL: EPOCH 600; B/C 19498 CAL. DUE: 03-25-2025.<BR>NO ADDITIONAL DAMAGE FOUND OTHER THAN FAULT DETAIL.PERFORMED DRY OUT ON FLAP TRACK # 2 FWD FAIRING 543AB AS PER B737 SRM 51-70-04-2R-9 PARAG 4-B TOOL USED: TEMP CONTROLLER ID160354 AND CALIBRATION DUE 03-07-25.PREPARED DAMAGE AREA FOR REPAIR ON FLAP TRACK # 2 FWD FAIRING 543AB AS PER B737 SRM 51-70-04-2R-9 PARAG 4-C.APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON FLAP TRACK # 2 FWD FAIRING 543AB AS PER B737 SRM 51-70-04-2R-9 PARAG 4-D-M; MATERIAL USED PO#2061896; PO#1738579 AND TOOL USED: TEMP CONTROLLER ID160354; CALIBRATION DUE 03-07-25.PERFORMED ULTRASOUND INSPECTION OF REPAIRED AREA AND MINIMUM OF 6 INCHES ALL AROUND USING CONTACT THROUGH TRANSMISSION ULTRASONIC REF B737 NDT PT 1; 51-01-01; NDT PT4 51-00-02.