5310-14-352-4417
Sleeve Nut
5310143524417 143524417 01902-02-705 C20214-1-4 85-662-1380
An internally threaded item with a cylindrical and/or square, hexagonal, octagonal, or dodecagonal outer periphery (parallel to the threaded axis) a portion(s) of which may or may not be enlarged, forming a flange(s) and/or shoulder(s). Items not having an enlarged outer portion may be threaded, a part of the full length, or tapped from both ends. Items having an enlarged outer portion (flange(s) or shoulder(s)) may be threaded the full length, threaded a part of the full length, or tapped from both ends. Items tapped from both ends shall have either right-hand threads on both ends or left-hand threads on both ends. For items conforming to any of the above and having a length overall exceeding two times the largest outside diameter or width across flats, use POST, ELECTRICAL-MECHANICAL EQUIPMENT. For items with an outside contour that is the same the full length, having a continuous thread through its entire length, and the length does not exceed two times the diameter or width across the flats use NUT (1), PLAIN (as modified). Excludes NUT (1), PLAIN, CAP. See also TURNBUCKLE BODY. View more Sleeve Nut
July 2023
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143524417 01902-02-705 C20214-1 NumberManufacturerStatus01902-02-705 F6198 - Airbus Operations (Active
Restrictions 5310-14-352-4417
End Users 5310-14-352-4417
- France (ZF)
Approved Sources 5310-14-352-4417
- Part Number
- Manufacturer
- Status
- 01902-02-705
- Manufacturer
- F6198 - Airbus Operations (Active)
- Primary Buy
- Primary Buy
- C20214-1-4
- F6198 - Airbus Operations (Active)
- Secondary Buy
- Secondary Buy
- 85-662-1380
- F5385 - Section De Codification 85 (Cancelled)
- NATO Reference
- NATO Reference