5325-14-537-0778
Turnlock Fastener Receptacle
5325145370778 145370778 NSA55134-302 212-12 55134-302
A threaded or tempered item used to secure the STUD, TURNLOCK FASTENER or STUD ASSEMBLY, TURNLOCK FASTENER by engaging with the cross pin, cam lead threads, or eared nut of the STUD, TURNLOCK FASTENER and securing it by means of its thread locking or spring action. View more Turnlock Fastener Receptacle
Managed by France
NSN Created on 24 Sep 2003
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 5325-14-537-0778
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Related Documents 5325-14-537-0778 5+ Documents (More...)
Sep 2003 5325-99-619-2793 Turnlock Receptacle 212-12SDRNCC: 3 | RNVC: 2 | DAC: 2 25 Apr 1991 5325-14-537-0778
Assembly 91S2-6WRNCC: 3 | RNVC: 2 | DAC: 4 26 Dec 1978 5325-01-085-3940 Turnlock Fastener Receptacle 212-12
Assembly 91S2-6WRNCC: 3 | RNVC: 2 | DAC: 4 26 Dec 1978 5325-01-085-3940 Turnlock Fastener Receptacle 212-12
4420-00-390-3693 4420003903693 003903693 DISK AND STUD
8040-01-115-8012 8040011158012 011158012 is a substance compounded for binding materials together by surface attachment. it is not used primarily to fill voids or pores or for sealing purposes. excludes canada balsam; cement, watch jewel; film cement, photographic; gasket cement; and gasket shellac compound.
3040-99-024-6784 3040990246784 990246784 is a shaft having two or more different diameters (greater than 0.031 inches (0.79 millimeter)) along its length. it must have one or more of the following conditions: a specified surface finish designation in the range 1 to 125 microinches (0.025 to 3.2 micrometers) arithmetical average (aa), machined peripheral flat(s), circular groove(s), keyway(s), splines, threads, or holes. the ends and/or shoulders may be machined to accommodate bearings, couplings, and the like. it is not designed for use in aligning by fitting into corresponding holes of another item. for items used to support rotating members see axle(1), shouldered. for items not having any of the above conditions see pin, shoulder, headless. excludes shaft(1), straight; and axle(1), straight.
6110-99-747-8846 6110997478846 997478846 is an item consisting of contacts, a magnetic core, and a coil with or without inclosure which is used to repeatedly establish and break a circuit. the item does not provide overload protection and is not used in line to control any other electrical controls. excludes relay, electromagnetic and starter, motor.l circuit. exludes relay, electro-magnetic and starter, motor.
Restrictions 5325-14-537-0778
End Users 5325-14-537-0778
- Oman (VE)
- Slovenia (WL)
- Brazil (YA)
- Spain (YB)
- Singapore (YJ)
- Malaysia (YW)
- France (ZF)
- Greece (ZU)
- Turkey (ZW)
Approved Sources 5325-14-537-0778
- Part Number
- Manufacturer
- Status
- NSA55134-302
- Manufacturer
- F5442 - Airbus Group Sas (Active)
- Source Control
- Source Control
- 212-12
- 71286 - Howmet Global Fastening Systems Inc (Active)
- Primary Buy
- Primary Buy
- 55134-302
- F5442 - Airbus Group Sas (Active)
- Secondary Buy
- Secondary Buy
NATO Stock Numbers Related to 5325-14-537-0778
5325-14-269-6740 5325-14-280-9026 5325-12-303-3865 5325-12-303-3825 5325-14-478-2815 5325-12-303-3862 5325-33-204-6912 5325-14-372-7212 5325-99-305-3640 5325-14-210-3658 5325-19-000-0661 5325-14-390-0034 5325-14-537-0780 5325-21-900-1648 5325-14-441-7188 5325-17-110-8640 5325-14-536-8816 5325-99-796-2381