What was found
INSPECTION FOUND A 1.25 CRACK IN LT WING BOOST PUMP CUTOUT IN REAR SPAR AFT WEB ON PERIPHERY AND AFT FACE OF CUTOUT. THE CRACK WAS STOP DRILLED. DOUBLER, FILLER, AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 53 AND 51-31-01.