Updated National Stock Numbers

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.

dome light nsn 6220000103982. overall height 2.156 inches

torsion helical spring nsn 5360000103977. inside diameter between 0.815 inches and 0.845 inches

electrolytic fixed capacitor nsn 5910000103882. 1276 wire lead type designator std mil an-3 and an-3 and an-3 and ccc

electrolytic fixed capacitor nsn 5910000103878. body style w/o mtg facilities terminal (s) on one end

electrolytic fixed capacitor nsn 5910000103877. body diameter 1.499 inches

pipe plug nsn 4730000103875. thread direction right-hand external

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

muff backing plate nsn 2990000103815. general characteristics item description steel cadmium plated round 6.25 in. od 0.0598 in. thk 4.0 in. diameter centrally located hole with four ms20501.624 self-locking nuts welded on the flange

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.

manual control lever nsn 1025000103805. special features steel forging fs 1015 through fs 1025 per specification mil-s-13048; 1.0 in. w; 6.75 in. lg; 2 holes in line 0.134 in. dia

3950000117771. drum and brake felt cage code: 20361

2530000117753. steering wheel part numbers: 000444-1007 01750-0705 0508971-00 10093b 1750-705 and 233253

6625000117698. interconnecting box has an overall width of 16.18 inches.

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.

3.25-4.922 in. id.; 0.263-0.27 in. diameter of 8 holes eq sp; 0.188 in. diameter of 2 holes; external spline data: 4.68 in. od; 4.571 in. pitch dia.; 32 teeth; 2nd external spline data: 4.781in. od; 4.75 in. pitch diameter.; 76 teeth; 0.125 in.

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

headless straight pin nsn 5315000103791. first end taper length 0.031 inches

headless straight pin nsn 5315000103689. first end style chamfered

headless straight pin nsn 5315000103688. first end style chamfered

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.

5320000110662. solid rivet has the shear strength 44000 single pounds per square inch.

5120000110641. torque wrench adapter has the material document and classification mil-s-6758 mil spec single material response.