FSC 2810 Aircraft Prime Mover Gasoline Reciprocating Engines and Components: 2810-00-118-8652, 2810-00-118-8873, 2810-00-118-8968
NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
2810-00-118-8652 2810001188652 | 41911 | Cover, Engine Poppet Valve Rocker | III 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) | |
2810-00-118-8662 2810001188662 | 39711 | Ring, Piston | III 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) | |
2810-00-118-8684 2810001188684 | 94969 | Ring, Piston | III Fsc Application Data: Acft eng R2800 Material: Iron overall Ring Style: 1 concentric | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) | |
2810-00-118-8718 2810001188718 | AS66376 66376 | RING | Curtiss-Wright Controls Inc. (0AHP5) Aircraft Supplies (12776) | ||
2810-00-118-8821 2810001188821 | 8363 | CAM | III End Item Identification: Acft eng R1830 | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) | |
2810-00-118-8823 2810001188823 | 76270 | CAM | III End Item Identification: Acft eng R2800 | United Technologies Corporation (77445) Pratt and Whitney Canada Inc. (00198) | |
2810-00-118-8824 2810001188824 | 76271 | CAM | United Technologies Corporation (77445) Hamilton Sundstrand Corporation (73030) Pratt and Whitney Canada Inc. (00198) | ||
2810-00-118-8825 2810001188825 | 106759 | CAM | III 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) | |
2810-00-118-8826 2810001188826 | 106760 | Cam, Main Crankcase | III 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) | |
2810-00-118-8851 2810001188851 | 10897 | TUBE | III 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) | |
2810-00-118-8852 2810001188852 | 10992 | ROD | Pratt and Whitney Canada Inc. (00198) | ||
2810-00-118-8858 2810001188858 | 13618 | Adapter, Pushrod Cover | III 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) | |
2810-00-118-8863 2810001188863 | 23144 | Ball, Push rod End | III 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) | |
2810-00-118-8873 2810001188873 | 11873 | Pushrod | Pratt and Whitney Canada Inc. (00198) | ||
2810-00-118-8874 2810001188874 | 11874 | Push rod, Exhaust | III 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) | |
2810-00-118-8875 2810001188875 | 11210 | Cover | Pratt and Whitney Canada Inc. (00198) | ||
2810-00-118-8934 2810001188934 | AS18629 18629 | Guide | III End Item Identification: Acft eng R1830 | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) Aircraft Supplies (12776) | |
2810-00-118-8938 2810001188938 | AS18630 18630 | Guide, Engine Poppet Valve Tappet | III 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) | |
2810-00-118-8956 2810001188956 | 17168 | Guide, Engine Poppet Valve Tappet | III 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) | |
2810-00-118-8968 2810001188968 | 106749 | Guide, Engine Poppet Valve Tappet | III 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) |