What was found
R/H WINGLET L/E CORRODED SEVERAL AREAS / [01] REMOVED CORROSION ON R/W WINGLET L/E; MATERIAL REMAINING 0.035'; FOUND OUT OF LIMITS; AREA EXCEEDS MAXIMUM DIAMETER OF 0.25' AND ALL WITHIN 1' OF FASTENER HOLES REF. AVIATION PARTNERS BOEING 737-NG WINGLET SRM 57-30-01;[02] LOCATED AND DRILLED NEW L/E AT R/H WINGLET IN REF SRM 51-40-02-0G-0;[03] ENTER IN ERROR REFERENCE NUMBER:<BR>LOCATED AND DRILLED NEW L/E AT R/H WINGLET IN REF SRM 51-40-05-0G-0;[04] VERIFIED STEPS 1 AND 3<BR>OK TO TREAT AND PRIME HOLES.;[05] TREATED AND PRIME HOLES AT NEW SKIN PANEL ASSY REF USED SRM 51-20-01-0G-0;[06] VERIFIED STEP 5;[07] OK TO INSTALL NEW RT WINGLET L/E SKIN PANEL.;[08] STEP 7 ENTERED IN ERROR <BR>INSTALLATION WILL BE ACCOMPLISHED ON CARD TTG8Q002MZ22