What was found
VERTICAL STAB FRONT SPAR LEFT FWD FUSELAGE FITTING BORE HAS PITTING ; / [01] REMOVED CORROSION AT VERTICAL STAB. FUSELAGE FRONT SPAR LH SIDE LUG BORE ; REAM FITTING HOLE FWD 1.2040'' AND AFT 1.1197'' AS PER B737 SRM -51-10-02-0G-0; [02] CORRECTION FOR STEP 1 <BR><BR>HOLE FWD - 1.1197''<BR>HOLE AFT - 1.2040''; [03] VERIFIED 1-2.; [04] REAM FITTING HOLE FWD 1.2040'' AND AFT 1.1197'' AS PER SRM 51-10-02-0G-0 AND EA 21-153-03538 ; AND NEW BUSHING AS FABRICATED AND INSTALLED AS PER EA 21-153-03538.; [05] VERIFIED STEP 5; [06] TOOLING INFO ONLY : BC 15463 09 MAR 22 CAL DATE