Used on engine aircraft f117, pw-100 (c-17a). 2 bolt hole quantity mismatch .015 max., flash extension .030 max permissible but must no exceed flash thickness oval, one bolt hole circle
Used on aircraft; c-17a support equipment. material, inconel; blank off flange; 05.00, flange spherical receptacle; self aligning joint; center bore 0.500-20unf-3b, per mil-s-7742 round, no bolt holes
Used on aircraft; c-17a support equipment. material, inconel; blank-off flange 05.00; slip flange, self aligning; center bore .500-20unf-3b per mil-s-7742 round, no bolt holes