What was found
DURING TRANSIT CHECK, IT WAS DETECTED A GOUGE OF THE LEADING EDGE LOWER SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A GOUGE 0.687 LENGTH, 208.75" WIDTH AT 56.25" OF THE RIGHT WING LEADING EDGE LOWER SKIN. THE DAMAGE WAS REMOVED, IAW SRM 57-20-01-1A-1, PARAGRAPH 4B(2), FIGURE 104, DETAIL D, TABLE 104. AN ULTRASONIC THICKNESS MEASUREMENT WAS PERFORMED, IAW 737 NDTM PART 4, 51-00-00, PROCEDURE 2 WITH MAXIMUM DEPTH OF REMOVED MATERIAL OF 0.029, IAW 737-800 SRM 57-20-01-1A-1, ALLOWABLE DAMAGE 1, TABLE 104, BEING WITHIN LIMITS. HIGH FREQUENCY EDDY CURRENT INSPECTION ON REWORKED AREA WAS PERFORMED, IAW 737 NDTM PART 6, 51-00-00, PROCEDURE 23, NO CRACKS WERE FOUND. A FLAP PEEN PROCEDURE ON REWORKED AREA WAS PERFORMED, IAW SRM 57-20-01-1A-1, PARAGRAPH 2H (1) AND SOPM 20-10-03. A CHEMICAL CONVERSION COATING WAS APPLIED, IAW SRM 51-20-01-0G-0, PARAGRAPH 5 A SURFACE FINISHES WERE APPLIED, IAW SRM 57-20-01-1A-1, PARAGRAPH 2H (4), ALL CORRECT.