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5340-00-181-1380
Helical Compression Spring Seat
5340001811380 001811380 2483282
A circular item, usually having a flat or grooved flange, boss(es), and/or counterbore designed to accommodate the end of the spring. It is used to position the spring, but does not encase the spring or restrain lateral motion. It may be used in conjunction with a RETAINER, HELICAL COMPRESSION SPRING. Excludes WASHER (1), (as modified); SEAT, BALL SOCKET and HOLDER, SPRING. See also ROTOR, ENGINE POPPET VALVE. View more Helical Compression Spring Seat
January 2023
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Related Documents 5340-00-181-1380 5+ Documents (More...)
Helical Compression Spring Seat 001811380 Documents 5340-00-181-1380 2+ Documents (More... ) https
-248-3282 Branched Wiring Harness 5995002483282,484982 www.nsnlookup.com /fsg-53/fsc-5340/us 5340-00-181-1380
Helical Compression Spring Seat 001811380 3282 5945012483282 012483282 RELAY,ELECTROMAGNETIC https
Restrictions 5340-00-181-1380
5340-00-181-1380 is a Helical Compression Spring Seat that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. The precious metals content of this item is unknown.
End Users 5340-00-181-1380
- Spain (YB01)
- Effective Date:
- 1 Apr 1991
- New Zealand (ZE01)
- Effective Date:
- 1 Apr 1991
- Greece (ZU01)
- Effective Date:
- 1 Mar 2008
Approved Sources 5340-00-181-1380
- Part Number
- Manufacturer
- Status
- 2483282
- Manufacturer
- 32970 - Aircraft Parts Corporation (Replaced)
- Original Design
- Original Design
- 2483282
- R1120 - Satair A/S (Active)
- Secondary Buy
- Secondary Buy
- 2483282
- 94931 - Bendix Corp The Bendix International (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
- 2483282
- 95270 - Skurka Aerospace Inc (Active)
- Advisory Reference
- Advisory Reference
Datasheet 5340-00-181-1380
- Characteristic
- Specifications
- FIIG
- Specifications
- T319-E
- Distance From End To First Step [BZDH]
- 0.1000 Inches Minimum And 0.1200 Inches Maximum
- End Diameter [BBRB]
- 0.4200 Inches Minimum And 0.4400 Inches Maximum
- Bore Diameter [ABXV]
- 0.1900 Inches Minimum And 0.1950 Inches Maximum
- Design Type [APGF]
- Solid
- First Step Diameter [ABPR]
- 0.5400 Inches Minimum And 0.5500 Inches Maximum
- Material [MATT]
- Steel
- Overall Height [ABKW]
- 0.1320 Inches Minimum And 0.1520 Inches Maximum
- Special Features [FEAT]
- Not Casehardened
- Style Designator [STYL]
- Seat
- Surface Treatment [SFTT]
- Cadmium And Chromate
NATO Stock Numbers Related to 5340-00-181-1380
Freight Information 5340-00-181-1380
5340-00-181-1380 has freight characteristics.. 5340-00-181-1380 has a variance between NMFC and UFC when transported by rail and the description should be consulted.