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NSN 2935-00-350-6193, 2935003506193
RING,WEARING

Federal Supply Classification
FSC 2935 - Engine System Cooling Components, Aircraft Prime Moving
National Item Identification Number
NIIN 003506193
Codification Country
United States
Item Name Code
INC 22534
Criticality
(X) This item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.
Hazardous Material Indicator Code
(N) There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials.
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DLMS® Summary

National Stock Number 2935-00-350-6193

National Stock Number (NSN) 2935-00-350-6193, or NIIN 003506193, (ring,wearing) was assigned March 25, 1970 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There are no manufacturer part numbers associated to this NSN.

This part number has not been procured by the US Government in over 5 years.

This NSN is somewhat common among different platforms, belonging to 3 different weapons systems.

Based on a planned procurement review by the Primary Inventory Control Activity (PICA) on Aug 02, 2005, this NSN's acquisition method was noted as: Not established. Not established.

This NSN is assigned to Item Name Code (INC) 22534. [A CYLINDRICAL ITEM WITH OR WITHOUT FLANGE(S), DESIGNED TO BE INSERTED IN A PUMP CASING OR SECURED TO THE IMPELLER OF A CENTRIFUGAL PUMP. IT IS USED FOR THE PURPOSE OF PROVIDING A CLOSE RUNNING CLEARANCE BETWEEN THE IMPELLER AND CASING IN ORDER TO PREVENT OR OVERCOME LEAKAGE DUE TO EROSION. IT MAY ALSO BE USED AS A DIFFUSER RING IN THE SUCTION AND DISCHARGE THROATS OF VALVES.]. This item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials. NSN 2935003506193 does not contain precious metals.

This NSN is associated to Schedule B 8411917050: parts of turbojet and turbopropeller aircraft engines, other than for use in civil aircraft. The Schedule B End Use is listed as engines and turbines for military aircraft. NAICS classification category 336412: aircraft engine and engine parts manufacturing.

This information was last updated on .


Technical Characteristics

BODY INSIDE DIAMETER
(ADAS) 6.497 INCHES MINIMUM AND 6.498 INCHES MAXIMUM
BODY OUTSIDE DIAMETER
(ADAR) 7.499 INCHES MINIMUM AND 7.501 INCHES MAXIMUM
BODY STYLE
(AAQL) PLAIN
CHAMFER ANGLE
(CSYT) 45.0 DEGREES NOMINAL INSIDE RIGHT CORNER
CHAMFER ANGLE
(CSYT) 45.0 DEGREES NOMINAL OUTSIDE RIGHT CORNER
CHAMFER LENGTH
(AAZP) 0.063 INCHES NOMINAL OUTSIDE RIGHT CORNER
CHAMFER LENGTH
(AAZP) 0.125 INCHES NOMINAL INSIDE RIGHT CORNER
CORNER SHAPE
(BZLX) CHAMFERED INSIDE RIGHT CORNER
CORNER SHAPE
(BZLX) CHAMFERED OUTSIDE RIGHT CORNER
CORNER SHAPE
(BZLX) SQUARE INSIDE LEFT CORNER
CORNER SHAPE
(BZLX) SQUARE OUTSIDE LEFT CORNER
FSC APPLICATION DATA
(ZZZV) CATAPULT,ACFT
OVERALL LENGTH
(ABHP) 3.469 INCHES NOMINAL
MATERIAL
(MATT) STEEL COMP 440C
SPECIAL FEATURES
(FEAT) SILVER PLATED FINISHON OD OF BODY
SURFACE FINISH
(CSYM) 125.0 MICROINCHES INSIDE
SURFACE FINISH
(CSYM) 63.0 MICROINCHES OUTSIDE
III MATERIAL
(MATT) STEEL COMP 440C

Manufacturer Part Numbers


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