Used on weapon system : mv-22 aircraft. 1.2530" overall length bushing, threaded , ai 22c-3 solid, external flange one end, internal flange at both ends
Used on weapon system : mv-22 aircraft. 1.2420" overall length navy bushing, sleeve , airc 21c-2 solid, external flange, interior flange (s) not located at either end
Used on weapon system : mv-22 aircraft.. 0.3550" overall length navy bushing, sleeve , airc all dimensions are after epoxy resin coating applied 22c solid, external flange one end
Used on weapon system : mv-22 aircraft.. 0.3550" overall length navy bushing, sleeve, airc end item; all dimensions are after coating of epoxy resin. 22c solid, external flange one end
Used on weapon system : mv-22 aircraft.. 0.9050" overall length navy bushing, sleeve, airc all dimensions are after epoxy resin applied. 22c solid, external flange one end
Used on weapon system : mv-22 aircraft.. 0.7990" overall length navy bushing, sleeve, airc end item. all dimensions are after coating applyed. 22c solid, external flange one end
Used on weapon system : mv-22 aircraft.. 0.7990" overall length navy bushing, sleeve, airc end item: all dimensions are after apoxy resin coating. 22c solid, external flange one end
Used on weapon system : mv-22 aircraft.. 1.1390" overall length navy bushing , sleeve , airc. all dimensions are after epoxy resin coating applyed. 22c solid, external flange one end
Used on weapon system : mv-22 aircraft.. 1.1390" overall length navy bushing, sleeve, airc. all dimensions are after epoxy resin coating applyed. 22c solid, external flange one end
Used on boeing 757 fixed wing aircraft floor beam assy station 720 to 879. 1.7000" overall length chromate surface treated 17c solid, plain, no outside flanges
Used on boeing 757 fixed wing aircraft hydraulic system reservoir installation section. 0.0500" overall length chromate surface treated 17c solid, plain, no outside flanges
Used on boeing 757 fixed wing aircraft elevator mechanical torque box installation. 0.3100" overall length chromate surface treated 17c solid, plain, no outside flanges
Used on boeing 757 fixed wing aircraft emergency door power assist installation. 0.3400" overall length chromate surface treated 17c solid, plain, no outside flanges
Used on boeing 757 fixed wing aircraft nose wheel well forward operating door mechanism. 0.4100" overall length chromate surface treated 17c solid, plain, no outside flanges
Used on boeing 757 fixed wing aircraft elevator power control unit installation. 0.4200" overall length chromate surface treated 17c solid, plain, no outside flanges
Used on boeing 757 fixed wing aircraft aft operating nose wheel well door installation mechanism. 0.4300" overall length chromate surface treated 17c solid, plain, no outside flanges
Used on boeing 757 fixed wing aircraft nose wheel well forward door operating mechanism. 0.4400" overall length chromate surface treated 17c solid, plain, no outside flanges
Used on boeing 757 fixed wing aircraft no 2 passenger door installation. 0.5500" overall length chromate surface treated 17c solid, plain, no outside flanges
Used on boeing 757 fixed wing aircraft elevator mechanism installation. 0.6300" overall length chromate surface treated 17c solid, plain, no outside flanges
Used on boeing 757 fixed wing aircraft elevator aft torque box mechanism. 0.9100" overall length chromate surface treated 17c solid, plain, no outside flanges