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NSN 2810-00-810-7294, 2810008107294
Cancelled -> Replaced by 2810008115670

Federal Supply Classification
FSC 2810 - Gasoline Reciprocating Engines, Aircraft Prime Mover; and Components
National Item Identification Number
NIIN 008107294
Codification Country
United States
Item Name Code
INC 15884
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 2810-00-810-7294

National Stock Number (NSN) 2810-00-810-7294, or NIIN 008107294, (valve,poppet,engine) was assigned January 1, 1963 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN replaces 2 stock numbers: 2810005404980, 2810008115670.

There are 4 manufacturer part numbers associated with this NSN. 3 of those part number(s) are considered obsolete. The manufacturer part numbers were originally supplied by 2 suppliers. Today, one supplier is listed as an Active supplier for this NSN. Of the active suppliers, only one supplier is deemed design controlled or valid supply parts.

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

This NSN is assigned to Item Name Code (INC) 15884. [A MUSHROOM OR TULIP-SHAPED ITEM HAVING A CIRCULAR HEAD WITH A CONICAL FACE AND AN EXTENDED STEM USED TO REGULATE THE FLOW OF INCOMING FUEL-AIR MIXTURE OR AIR INTO THE COMBUSTION CHAMBER OR EXHAUST GASES FROM THE COMBUSTION CHAMBER OF A RECIPROCATING INTERNAL COMBUSTION ENGINE.]. 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 2810008107294 contains an unknown precious metal.

This NSN is associated to Schedule B 8409100080: parts for spark-ignition or compression-ignition internal combustion piston engines for use in aircraft except civil. 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

III MATERIAL AND LOCATION
(ANNQ) STEEL HEAD
MATERIAL AND LOCATION
(ANNQ) COBALT ALLOY TIP ERR-100 ERR-100
MATERIAL AND LOCATION
(ANNQ) SODIUM INTERNAL FILLING
III MATERIAL AND LOCATION
(ANNQ) SODIUM INTERNAL FILLING
MATERIAL AND LOCATION
(ANNQ) STEEL HEAD ERR-100 ERR-100
MATERIAL AND LOCATION
(ANNQ) COBALT ALLOY STEM
CARBON RELIEF GROOVE
(ALYZ) NOT INCLUDED
DISTANCE FROM GROOVE TO STEM END
(ALZG) 0.2230 INCHES MINIMUM AND 0.2330 INCHES MAXIMUM
FSC APPLICATION DATA
(ZZZV) ACFT ENG R2800
GROOVE DIAMETER
(AAVZ) 0.5660 INCHES MINIMUM AND 0.5700 INCHES MAXIMUM
GROOVE WIDTH
(ABGF) 0.1865 INCHES MINIMUM AND 0.1885 INCHES MAXIMUM
HEAD HEIGHT
(AASU) 0.4860 INCHES MINIMUM AND 0.5160 INCHES MAXIMUM
HEAD STYLE
(AASK) MUSHROOM
METALLIC HARDNESS RATING AND LOCATION
(ASXJ) 350.0 VICKERS OR FIRTH DIAMOND PYRAMID MINIMUM STEM
METALLIC HARDNESS RATING AND LOCATION
(ASXJ) 69.0 ROCKWELL SUPERFICIAL 30-N NOMINAL TIP
NECK RADIUS
(ALZB) 0.8750 INCHES NOMINAL
OUTSIDE DIAMETER
(ABKV) 2.5680 INCHES MINIMUM AND 2.5980 INCHES MAXIMUM
SEAT ANGLE IN DEG
(AJFY) 45.0
STEM DIAMETER
(ALZE) 0.6765 INCHES MINIMUM AND 0.6775 INCHES MAXIMUM
STEM LENGTH
(ALZD) 5.6070 INCHES MINIMUM AND 5.6370 INCHES MAXIMUM
STEM STYLE
(ALYX) GROOVED
MATERIAL AND LOCATION
(ANNQ) COBALT ALLOY TIP
MATERIAL AND LOCATION
(ANNQ) STEEL HEAD
III MATERIAL AND LOCATION
(ANNQ) COBALT ALLOY TIP
MATERIAL AND LOCATION
(ANNQ) COBALT ALLOY STEM ERR-100 ERR-100
III MATERIAL AND LOCATION
(ANNQ) COBALT ALLOY STEM
UNABLE TO DECODE
(ANNQ) UNABLE TO DECODE

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