What was found
MAJOR REPAIR DURING MAINTENANCE BASE INSPECTION THE FUSELAGE SKIN WAS FOUND CRACKED FORWARD AND AFT OF RIVET ON FRAME 75 AND STRINGER 2 LEFT CUT OUT DAMAGE. FABRICATED A .8" X .78" FILLER, A 9.5" X 7.4" DOUBLER AND A .9" X 2.7" SHIM USING AL2024T3 0.063". PREPPED, CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR IAW AEA EO EM-53MR-1347. AIRCRAFT RETURNED TO SERVICE.