Our Updated Products - Page 8 of 100

3120000110891. sleeve bearing has an overall length of between 0.5640 inches and 0.5680 inches.

5330000110883. packing retainer has a hole diameter of between 0.389 inches and 0.397 inches.

3010000110876. output clutch has the end item identification h-46 aircraft.

5340000110885. helical compression spring seat cage codes: 77272 and 81205

4710000110875. spacer tube has a diameter of 0.880 inches.

1560000110874. stop disc has the end item identification h-46 helicopter.

1560000110873. clutch piston has the end item identification h-46 aircraft.

5365000110867. plate spacer has an overall length of 3.355 inches and 3.360 inches.

3010000110870. sliding clutch cage code: 50582

1560000110863. bearing plate cage code: 50582

3040000110865. spur gearshaft cage code: 50582

1650000110853. retaining ring insert cage code: 81982

1650000110861. rod guide cage code: 81982

4710000110848. metal tube assembly is classified into thread class 3a for the first end and thread class 3b for the second end.

1650000110849. hydraulic fluid cap cage code: 81982

4730000110846. pipe flange has a thickness of 0.030 inches.

4730000110847. valve orifice cage codes: 81873 18876 81873 and 18876

1650000110844. pump seal ring has the end item identification sea stallion h-53 helicopter.

1650000110843. seal drive ring cage codes: 90166 43491 and 62983

4320000110837. rotary pump wear plate cages codes: 62983 43491 and 90166

1650000110830. line actuating cylinder assembly has an overall height of 3.250 inches and an overall width of 5.750 inches.

1650000110829. line actuating cylinder assembly is made of aluminum alloy.

5310000110818. hexagon plain nut is classified as thread class 2b.

5310000110816. hexagon plain nut is classified into thread class 2b.

5310000110814. hexagon plain nut is classified as thread class 2b.

5310000110813. hexagon plain nut is classified as thread class 2b.

5310000110812. hexagon plain nut has a hexagon nut style and a nut height of between 0.212 inches and 0.226 inches.

5320000110803. solid rivet has a fastener length of 1.750 inches.

5320000110798. solid rivet has a straight style shank and a shank diameter of 0.156 inches.

5320000110797. solid rivet has a fastener length of 1.000 inches.

5320000110796. solid rivet has a straight style shank and a shank diameter of 0.156 inches.

5320000110791. solid rivet has a button head style and a head height of between 0.110 inches and 0.124 inches.

6650000110765. spectrometer jaw has the end item identification 6650-00-937-4401.

6650000110764. electrode guide has the end item identification 6650-00-937-4401.

5315000110743. headless straight pin has a first end tapered angle of 25.0 degrees.

5315000110733. headless straight pin has an overall length of between 0.800 inches and 0.824 inches.

5315000110741. headless straight pin part numbers: 110741 19j325pc51 19j328-64 3272841 49j325pc51 49j328-64 5b9504 72837s and g25jd8.

5315000110731. woodruff key has a hardness rating of 10.0 rockwell c.

5310000110730. lock washer has a hole diameter of between 0.382 inches and 0.398 inches.

3040000110717. rigid connecting link part numbers: 6-50732-501 6-50732-503 and 6-50732-505.

2995000110716. ove valve parts kit cage code: 09445.

2995000110715. metering plug assy cage code 77445

5340000110696. rod end connector has a thread length of 0.500 inches.

5340000110695. angle bracket has the material document and classification 5510 national spec single material response.

2840000110693. aircraft ga turbine rotor spacer has the end item identification aircraft eng t56.

2840000110692. aircraft gas turbi turbine shaft has the end item identification acft eng t56.

2840000110678. aircraft gas tur compressor disk has a hardness rating of between 32.0 rockwell c and 38.0 rockwell c.

2840000110677. aircraft gas tur compressor disk has a hardness rating if between 32.0 rockwell c and 38.0 rockwell c.

1560000110674. rudder trim tab is apart of the aircraft mission design series kc-135.

4730000110667. pipe plug has a recessed square drive end style.