Aircraft Prime Mover Gasoline Reciprocating Engines and Components: 2810L20-014-3, 2810L23-021, 2810L23-023

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MFG SKUNSNItem NameDetailsManufacturer (CAGE)RFQ
2810L20-014-3
2810L200143
2810-00-119-0202Guide, Valve StemIII Fsc Application Data: Acft eng R985
Material: Copper alloy
Outside Diameter: 0.865 inches minimum and 0.885 inches maximum
U S Army Aviation and Missile (81996)

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2810L20-023
2810L20023
2810-00-118-7746LockplateIII End Item Identification: Acft eng R985
General Characteristics Item Description: Matl steel per ams 5040 or ams 5042; overall length 0.625 in.; 0.25 in. wide; 0.266 in. deep; matl thickness 0.03125 in.
U S Army Aviation and Missile (81996)

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2810L20-027
2810L20027
2810-00-119-0575Tube, SteppedIII End Item Identification: Acft eng R985
General Characteristics Item Description: Matl steel per ams 5050; overall length 1.3125 in.; 0.312 in. od for 0.5625 in.; 0.314 in. od for 0.75 in.; wall 0.025 in. thick
U S Army Aviation and Missile (81996)

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2810L20-043
2810L20043
2810-00-118-8353TUBEIII End Item Identification: Acft eng R985
General Characteristics Item Description: Matl steel per ams 5050; overall length 3.875 in.; od 0.3115 in. min and 0.3120 in max except 0.5625 in. one end with od of 0.3140 in. min and 0.3145 in. max; chamfered ends
U S Army Aviation and Missile (81996)

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2810L20-045
2810L20045
2810-00-165-5796BANDU S Army Aviation and Missile (81996)

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2810L20-049
2810L20049
2810-00-306-7102Liner, CrankcaseIII End Item Identification: Acft eng R1830
General Characteristics Item Description: Matl steel per ams 6272; hardness per rockwell C20 min and C40 max; 1.015625 in. long; body 5.699 in. min and 5.701 in. max od; flange 5.762 od; bore 5.489 dia; 4 holes in side of body 0.187 in. min and 0.189 in. max dia
U S Army Aviation and Missile (81996)

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2810L20-054
2810L20054
2810-00-118-8598TUBEU S Army Aviation and Missile (81996)

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2810L20-054-10
2810L2005410
2810-00-118-8599TUBEU S Army Aviation and Missile (81996)

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2810L20-055-3
2810L200553
2810-00-306-6430Socket, Pushrod BallU S Army Aviation and Missile (81996)

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2810L20-065
2810L20065
2810-00-440-0250LinerU S Army Aviation and Missile (81996)

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2810L20-065-5
2810L200655
2810-00-440-0250LinerU S Army Aviation and Missile (81996)

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2810L20-067-1
2810L200671
2810-00-168-5015Seal Ring, MetalMaterial: Copper alloy overall
Cross-Sectional Shape Style: Plain rectangular, straight face
Material Document AND Classification: Ams 7320B assn std single material response overall
U S Army Aviation and Missile (81996)

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2810L20-067-7
2810L200677
2810-00-554-5681Seal Ring, MetalMaterial: Iron outside periphery
Cross-Sectional Shape Style: Plain rectangular, straight face
Special Features: Bronze, cast leaded, ams 7320B
U S Army Aviation and Missile (81996)

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2810L20-067-9
2810L200679
2810-00-808-9220Seal Ring, MetalMaterial: Copper alloy overall
Cross-Sectional Shape Style: Plain rectangular, straight face
Material Document AND Classification: Ams 7320B assn std single material response overall
U S Army Aviation and Missile (81996)

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2810L23-007
2810L23007
2810-00-670-1692Lock, Valve Spring RetainerCasehardening Indicator: Not casehardened
Overall Height: 0.1245 inches minimum and 0.1255 inches maximum
Metallic Hardness Rating: 60.0 nominal rockwell C
U S Army Aviation and Missile (81996)

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2810L23-013
2810L23013
2810-00-523-3135Ring, Propeller ShafU S Army Aviation and Missile (81996)

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2810L23-020
2810L23020
2810-00-523-3137Sleeve, Propeller ShU S Army Aviation and Missile (81996)

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2810L23-021
2810L23021
2810-00-505-9124Hub, Magneto drIII Fsc Application Data: Eng G0480
U S Army Aviation and Missile (81996)

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2810L23-021-1
2810L230211
2810-00-505-9124Hub, Magneto drIII Fsc Application Data: Eng G0480
U S Army Aviation and Missile (81996)

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2810L23-023
2810L23023
2810-00-807-7820Seat, E, Haust ValveU S Army Aviation and Missile (81996)

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  • We solve sourcing challenges for 2810L20-014-3, 2810L20-043, 2810L20-045, 2810L20-054-10, 2810L20-055-3, 2810L20-065-5, 2810L20-067-9, 2810L23-020, 2810L23-021-1, 2810L23-023 - NSN parts, hard to find, long lead time and obsolete components.