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5340-00-415-0189

Compression Cup

5340004150189 004150189 5190297 205

A nonmetallic cup-shaped item designed to be located within a cylinder, and whose contact edge with the cylinder walls is usually feathered. This item, by means of extrusion, makes close physical contact with the cylinder walls in order to prevent the escape of internal pressure. The item may have a center hole and/or bolt holes. Excludes CUP, HYDRAULIC BRAKE CYLINDER. View more Compression Cup

5340-00-415-0189 CUP,COMPRESSION 5340004150189 004150189

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
January 2023
NATO Update Count
9
NATO Data Quality
5340-00-415-0189 CUP,COMPRESSION 5340004150189 004150189 1/1
NSN 5340-00-415-0189 (Generic Image) 1/1

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5340-00-415-0189 Related Documents Related Documents 5340-00-415-0189 5+ Documents (More...)

DAC: X 1 Jan 1963 5970-00-415-0151 Bushing Insulator 157RNCC: 5 | RNVC: 9 | DAC: X 1 Jan 1963 5340-00-415-0189
058-2897 5996-43-000-1511 5996-12-337-2164 5996-12-376-9762 5820-15-064-2157 5840-12-130-7780 5895-15-205
1560-14-519-0297 1560145190297 145190297 is an item of various configuration that is an integral member of the airframe structure. it is specifically designed for the purpose of maintaining, positioning, joining, and strengthening the aircraft structure. it may include holes for mounting purposes or to form an assembly.
6150-37-519-0297 6150375190297 375190297 is an item consisting of two or more individually insulated conductors (solid, stranded, or tinsel) of a definite length, with or without shielding, held together by lacing cord, metal bands, or similar type binding. the individual conductors are usually identified by color, or by alphabetic or numeric codes or symbols. the item may include fittings which provide for connection to other items. excludes items which are branched, forked, jacketed, sleeved, or contained in a common covering. also excludes cable assembly (as modified); harness, electrical equipment; lead assembly, electrical; and wiring harness, branched.
Upgrade for $1 a day Upgrade your Account Upgrade 3040-01-322-0992Spur Gearshaft3040013220992 013220992 5190297
NumberManufacturerStatus5190297 97993 - General Dynamics Defense Systems (Active) Primary Buy RNCC 3 RNVC 2 DAC E 5190297
53711 - Naval Sea Systems Command (Active) Secondary Buy RNCC 5 RNVC 2 MEDALS DAC A 5190297 50582 -

5340-00-415-0189 Demil Restrictions 5340-00-415-0189

DEMIL: A | DEMILI: | CRITICALITY: X | HMIC: P | PMIC: U | EDC: | ADPEC:

5340-00-415-0189 is a Compression Cup 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.

5340-00-415-0189 End Users End Users 5340-00-415-0189

Spain (YB01)
Effective Date:
1 Apr 1991
Greece (ZU01)
Effective Date:
1 Aug 1995
Turkey (ZW01)
Effective Date:
1 Dec 2005

5340-00-415-0189 Manufacturers Approved Sources 5340-00-415-0189

5340-00-415-0189 Technical Data Datasheet 5340-00-415-0189

Characteristic
Specifications
FIIG
A03100
Material [MATT]
Rubber Overall
Overall Length [ABHP]
0.281 Inches Nominal
Center Hole Diameter [ADYT]
0.266 Inches Nominal
Base Material Thickness [AKKE]
0.141 Inches Nominal
Feather Edge Angle [CXXB]
30.0 Degrees Nominal

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5340-00-415-0189 Freight Data Freight Information 5340-00-415-0189

5340-00-415-0189 has freight characteristics.. 5340-00-415-0189 has a variance between NMFC and UFC when transported by rail and the description should be consulted.