FSC 2810 Aircraft Prime Mover Gasoline Reciprocating Engines and Components: 2810-00-118-8652, 2810-00-118-8873, 2810-00-118-8968

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NSNMFG SKUItem NameDetailsManufacturer (CAGE)RFQ
2810-00-118-8652
2810001188652
41911Cover, Engine Poppet Valve RockerIII End Item Identification: Acft eng R1830
Special Features: Matl:alum alloy per ams 4212
Overall Length: 5.375 inches nominal
Pratt and Whitney Canada Inc. (00198)
United Technologies Corporation (77445)

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2810-00-118-8662
2810001188662
39711Ring, PistonIII Fsc Application Data: Acft eng R1830
Material: Iron overall
Ring Style: 1 concentric
United Technologies Corporation (77445)
Kaydon Ring & Seal Inc. (75370)
Pratt and Whitney Canada Inc. (00198)

Quote

2810-00-118-8684
2810001188684
94969Ring, PistonIII Fsc Application Data: Acft eng R2800
Material: Iron overall
Ring Style: 1 concentric
Pratt and Whitney Canada Inc. (00198)
United Technologies Corporation (77445)

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2810-00-118-8718
2810001188718
AS66376
66376
RINGCurtiss-Wright Controls Inc. (0AHP5)
Aircraft Supplies (12776)

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2810-00-118-8821
2810001188821
8363CAMIII End Item Identification: Acft eng R1830
Pratt and Whitney Canada Inc. (00198)
United Technologies Corporation (77445)

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2810-00-118-8823
2810001188823
76270CAMIII End Item Identification: Acft eng R2800
United Technologies Corporation (77445)
Pratt and Whitney Canada Inc. (00198)

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2810-00-118-8824
2810001188824
76271CAMUnited Technologies Corporation (77445)
Hamilton Sundstrand Corporation (73030)
Pratt and Whitney Canada Inc. (00198)

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2810-00-118-8825
2810001188825
106759CAMIII End Item Identification: Acft eng R2000
General Characteristics Item Description: Steel AMS6263, hardness rockwell a, 81 min, 84 max, 96 teeth, 20 degreepressure angle, involute form
Pratt and Whitney Canada Inc. (00198)
United Technologies Corporation (77445)

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2810-00-118-8826
2810001188826
106760Cam, Main CrankcaseIII End Item Identification: Acft eng R2000
General Characteristics Item Description: Matl steel per ams 6263; hardness, case, rockwell A81 min and A84 max, core, rockwell C35 min and C45 max; overall od 9.020 in. min and 9.024 in. max; overall length 1.766 in.; gear, 96 teeth, pitch dia 10.8628; four intake and four exhaust lobes
Pratt and Whitney Canada Inc. (00198)
United Technologies Corporation (77445)

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2810-00-118-8851
2810001188851
10897TUBEIII End Item Identification: Acft eng R1340
General Characteristics Item Description: Matl steel per ams 5062; tin flash per ams 2408; overall length 2.750 in.; 0.375 in. of one end at od 0.4815 in. min and 0.4825 in. max; 0.6875 in. of one end at od 0.4995 in. min and 0.5005 in. max; remaining length at od 0.485 in. min and 0.495 in max
Pratt and Whitney Canada Inc. (00198)
United Technologies Corporation (77445)

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2810-00-118-8852
2810001188852
10992RODPratt and Whitney Canada Inc. (00198)

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2810-00-118-8858
2810001188858
13618Adapter, Pushrod CoverIII End Item Identification: Acft eng R1830
General Characteristics Item Description: Matl aluminum alloy per ams 4120 or ams 4152; 0.990 in. min and 1.010 in. max long; first end threaded 1.375-20NS; flange 1.365 in. min and 1.385 in. max od; second end threaded 1.250-20NS; bore 1.052 in. min and 1.072 in. max dia
United Technologies Corporation (77445)
Pratt and Whitney Canada Inc. (00198)

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2810-00-118-8863
2810001188863
23144Ball, Push rod EndIII End Item Identification: Acft eng R1830
General Characteristics Item Description: Matl steel per ams 6272; hardness per rockwell C20 min and C40 max; 1.156 in. long; shoulder 0.688 in. od; shank 0.375 in. min and 0.385 in. max od; end spherical 0.218 in. min and 0.219 in. max radius; bore 0.04 in. dia; counterbored 0.094 in. dia; second counterbore 0.552 in. min and 0.553 in. max dia
United Technologies Corporation (77445)
Pratt and Whitney Canada Inc. (00198)

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2810-00-118-8873
2810001188873
11873PushrodPratt and Whitney Canada Inc. (00198)

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2810-00-118-8874
2810001188874
11874Push rod, ExhaustIII End Item Identification: Acft eng R1340
General Characteristics Item Description: Aluminum per ams 4088; hardness rockwell B60; overall length 13.710 in.; main body od 0.5625, last 0.5 in. of each end od 0.555
Pratt and Whitney Canada Inc. (00198)
United Technologies Corporation (77445)

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2810-00-118-8875
2810001188875
11210CoverPratt and Whitney Canada Inc. (00198)

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2810-00-118-8934
2810001188934
AS18629
18629
GuideIII End Item Identification: Acft eng R1830
Pratt and Whitney Canada Inc. (00198)
United Technologies Corporation (77445)
Aircraft Supplies (12776)

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2810-00-118-8938
2810001188938
AS18630
18630
Guide, Engine Poppet Valve TappetIII End Item Identification: Acft eng R1830
Special Features: Matl alum alloy per AMS4118;4.953 in. lg;body od stepped 1.062 in., 1.125/1.126, 1.125/1.130, 1.131/1.132 in.;flanged stepped 1.25 in. od, 1.125 in. od;threaded 1.375-20N;BORE dia 0.823/0.833 in.
Aircraft Supplies (12776)
Pratt and Whitney Canada Inc. (00198)
United Technologies Corporation (77445)

Quote

2810-00-118-8956
2810001188956
17168Guide, Engine Poppet Valve TappetIII End Item Identification: R1830 acft eng
Special Features: Main body od varies from 1.125 in. min & 1.126 in. max to 1.131 in. min & 1.132 in. max; first end 1.062 in. od X 0.664 in. long; second end externally threaded 1.375-20N X 0.312 in. long; for front lower exhaust valve tappet
Material: Aluminum alloy, ams 4118
United Technologies Corporation (77445)
Pratt and Whitney Canada Inc. (00198)

Quote

2810-00-118-8968
2810001188968
106749Guide, Engine Poppet Valve TappetIII End Item Identification: R2000 acft eng
Special Features: Threading at flange, pitch dia 1.3385-1.3425; body od decreased fm 1.132 in. at flange to 1.125 in., opposite end 1.062 in. od
Material: Aluminum alloy, ams 4118
United Technologies Corporation (77445)
Pratt and Whitney Canada Inc. (00198)

Quote

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