2530-14-230-2073

Ball Stud Adjusting Plug

2530142302073 142302073 327135

A headless, externally threaded item usually slotted in one end to facilitate turning and to accommodate a locking device. The opposite end may be flat, concave or drilled to mate with a tension spring, bearing, ball or ball seat. It is designed to adjust tension and secure in position the ball stud of a steering tie rod end, drag link end and/or other connectors of this type. View more Ball Stud Adjusting Plug

2530-14-230-2073 PLUG,ADJUSTING,BALL STUD 2530142302073 142302073

Managed by France
NSN Created on 1 Jan 1967
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2530-14-230-2073 PLUG,ADJUSTING,BALL STUD 2530142302073 142302073 1/1
NSN 2530-14-230-2073 (Generic Image) 1/1

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2530-14-230-2073 Related Documents Related Documents 2530-14-230-2073 5+ Documents (More...)

www.nsnlookup.com /nato/nato-stock-numbers/inc Ball Stud Adjusting Plug (INC 18541) Jan 1964 2530-14-230-2073
1991 2530-14-209-0360 Ball Stud Adjusting Plug 0604699500RNCC: 3 | RNVC: 2 | DAC: 6 1 Jan 1964 2530-14-230-2073
1560-01-076-8932 1560010768932 010768932 is a preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. it is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. it may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. it may be mounted by means of fasteners, bonding or welding. excludes panel, interior lining, aircraft; cover access; cover, access, aircraft; floor (1), aircraft; core material, cellular, structural.
1560-01-076-8933 1560010768933 010768933 is a preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. it is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. it may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. it may be mounted by means of fasteners, bonding or welding. excludes panel, interior lining, aircraft; cover access; cover, access, aircraft; floor (1), aircraft; core material, cellular, structural.

2530-14-230-2073 Demil Restrictions 2530-14-230-2073

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2530-14-230-2073 is a Ball Stud Adjusting Plug

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