What was found
VERTICAL STAB FRONT SPAR RIGHT FWD FUSELAGE FITTING BORE HAS PITTING ; / [01] REMOVED CORROSION AT VERTICAL STAB. FUSELAGE FRONT SPAR RH SIDE LUG BORE ; REAM HOLE FITTING FWD 1.1195'' AS PER B737 SRM 51-10-02-0G-0.; [02] VERIFIED 1.; [03] NEW BUSHING WAS FABRICATED AND INSTALLED AS PER EA 21-153-03537. BUSHING WAS FABRICATED BY PREMIER AEROSPACE PO- 1748138.; [04] ''PERFORMED EA 21-153-03537. REF. FAULT TTG8Q009DJAZ.'; [05] VERIFIED STEPS 3 AND 4.