What was found
INSPECTION IAW AD. CRACK WAS FOUND IN RIGHT ENGINE CANTED BULKHEAD CAP. CRACK WAS LOCATED ON INBOARD SIDE OF CAP JUST INSIDE OF INBOARD WING LIP. CRACK WAS APPROXIAMATELY 1.5 INCHES AND RAN CHORD WISE WITH THE WING, IT WAS LOCATED IN THE AFT OF THE CAP WIDTH. UPON REMOVAL OF CANTED BULKHEAD CAP FOUND FORWARD CANTED BULKHEAD TO BE CRACKED PERPENDICULAR TO CAP CRACK ON INBOARD SIDE IN BEND OF TOP FLANGE. CRACK WAS ABOUT 1 INCH IN LENGTH. AFT AND FORWARD BULKHEADS INBOARD SIDES HAD SEPERATED FROM INBOARD NACELLE WING RIB. FOUND THIS SAME COMBINATION ON THE LT SIDE OF THIS SAME AIRCRAFT.