What was found
DOOR 532JB FUEL ACCESS HOLE O/B LEFT WING LOWER AREA WITH CORROSION ON FLANGE OUTER SURFACE.<[01] REMOVED CORROSION FROM 532JB FUEL ACCESS HOLE O/B LEFT WING LOWER AREA ON FLANGE OUTER SURFACE PER SRM 57-20-01-2R-1.;[02] VERIFIED STEP 1;[03] REWORKED AREA TO 63 MICROINCHES SMOOTH; AND MEASURED REMAINING MATERIAL: .203'; FOUND TO BE WITHIN LIMITS PER SRM 57-20-01-2R-1 FIG 203 DETAIL A TOOLS USED B/C 175310 CAL DUE 26-MAY-24 AND B/C 171855 NO DUE DATE.;[04] CORRECTION STEP 3: REWORKED AREA TO 63 MICROINCHES SMOOTH; AND MEASURED REMAINING MATERIAL: .197'; FOUND TO BE WITHIN LIMITS PER SRM 57-20-01-2R-1 FIG 203 DETAIL A TOOLS USED B/C 175310 CAL DUE 26-MAY-24 AND B/C 171855 NO DUE DATE.;[05] VERIFIED STEP 4;[06] FLAP PEEN THE AREA AND APPLIED CHEMICAL CONVERSION COATING TO AREA AS PER SRM 57-20-01-2R-1.;[07] REMOVED LIGHT CORROSION AT DOOR 532JB FUEL ACCESS HOLE O/B FLANGE OUTER SURFACE AND REWORKED AREA TO 63 MICROINCHES MIN. REMAINING MATERIAL FOUND WITHIN LIMITS; AREA WAS FLAP PEENED AND CHEMICAL CONVERSION COATING APPLIED AS PER SRM 57-20-01-2R-1.;[08] VERIFIED LIGHT CORROSION REMOVAL AT DOOR 532JB FUEL ACCESS HOLE O/B FLANGE OUTER SURFACE AND REWORKED AREA TO 63 MICROINCHES MIN. REMAINING MATERIAL FOUND WITHIN LIMITS; AREA WAS FLAP PEENED AND CHEMICAL CONVERSION COATING APPLIED.