Aircraft Prime Mover Gasoline Reciprocating Engines and Components: 228010, 22897, 23064370
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 228010 | 2810-00-048-7634 | Guide, Engine Poppet Valve Tappet | III End Item Identification: R2800 acft eng Special Features: Exhaust valve tappet front cylinders 16 & 18 Material: Aluminum alloy, ams 4118 | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) | |
| 228010P015 | 2810-00-310-9187 | Guide, Engine Poppet Valve Tappet | III End Item Identification: R2800 acft eng Special Features: Thd end 1.375 in. dia; fm thd end 1.295 in. dia, flange 1.25 in. dia, groove 1.08 in. dia; body decreases in dia, 1.1465 in. dia at 0.781 in. fm flange, 1.1425 in. dia at 2.078 in. fm flange, 1.1405 in. dia at 3.219 in. fm flange; second end 1.062 in. dia, 0.156 in. lg chamfered end; thd end slanted 6.0 deg Material: Aluminum alloy, ams 4118 | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) | |
| 228010P15 | 2810-00-310-9187 | Guide, Engine Poppet Valve Tappet | III End Item Identification: R2800 acft eng Special Features: Thd end 1.375 in. dia; fm thd end 1.295 in. dia, flange 1.25 in. dia, groove 1.08 in. dia; body decreases in dia, 1.1465 in. dia at 0.781 in. fm flange, 1.1425 in. dia at 2.078 in. fm flange, 1.1405 in. dia at 3.219 in. fm flange; second end 1.062 in. dia, 0.156 in. lg chamfered end; thd end slanted 6.0 deg Material: Aluminum alloy, ams 4118 | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) | |
| 228010R1 | 2810-00-335-4816 | Guide, Valve Stem | Special Features: Aa end threaded at 1.375-20 ns and pitch dia 1.3405 Material: Aluminum alloy, ams 4118 Outside Diameter: 1.075 inches minimum and 1.085 inches maximum | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) | |
| 228011 | 2810-00-048-7635 | Guide, Engine Poppet Valve Tappet | III End Item Identification: Acft eng, reciprocating Special Features: Matl alum alloy per AMS4118;MAIN body od 1.125/1.126 in. to 1.131/1.132 in.;first end 1.052/1.072 in. by 0.666 in. lg;second end externally thded 1.375-20 ns, lgth 0.96/0.98 in.;for rear exhaust valve tappet Overall Length: 4.736 inches nominal | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) | |
| 228011P15 | 2810-00-310-9188 | Guide, Engine Poppet Valve Tappet | III End Item Identification: R2800 acft eng Special Features: Main body od varies fm 1.140 in. min & 1.141 in. max to 1.146 in. min & 1.147 in. max; first end 1.052 in. min & 1.072 in. max od by 0.666 in. lg; second end externally threaded 1.375-20NS by 0.96 in. min & 0.98 in. max lg; for rear exhaust valve tappet Material: Aluminum alloy, ams 4118 | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) | |
| 228011R1 | 2810-00-335-4817 | Guide, Engine Poppet Valve Tappet | Special Features: Main body od varies fm 1.135 in. min & 1.136 in. max to 1.141 in. min &1.142 in. max; first end 1.052 in. min & 1.072 in. max od by 0.666 in. lg; second end externally thd 0.96 in. min & 0.98 in. max lg; for rear exhaust valve tappet Material: Aluminum alloy, ams 4118 Overall Length: 4.736 inches nominal | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) | |
| 22895 | 2810-00-118-7748 | Valve, Oil Return | III End Item Identification: Acft eng R985 General Characteristics Item Description: Matl steel per ams 5022; 2.5 in. long; first end threaded 0.25-28NF-3; body 0.248 od; flange 1.34375 in. od | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) | |
| 22897 | 2810-00-118-7167 | SEAT | Pratt and Whitney Canada Inc. (00198) | ||
| 229297 | 2810-00-808-4352 | Valve, Poppet, Engine | III Fsc Application Data: Engine, aircraft, reciprocating Outside Diameter: 2.5830 inches nominal Head Style: 2 mushroom | Pratt and Whitney Canada Inc. (00198) United Technologies Corporation (77445) | |
| 23033761 | 2810-01-326-2434 | Baffle, Airflow, Aircraft Reciproc | III Fsc Application Data: T56A427 engine | Rolls-Royce Corporation (63005) | |
| 23035451 | 2810-01-326-2435 | Baffle, Airflow, Aircraft Reciproc | III Fsc Application Data: T56A427 engine | Rolls-Royce Corporation (63005) | |
| 23036361 | 2810-01-334-8494 | Push rod, Engine Poppet Valve | Rolls Royce Naval Marine Inc. (38ZC7) Rolls-Royce Corporation (63005) | ||
| 2304 | 2810-00-098-2484 | Cover, Starter Drive | Teledyne Industries Inc. (28839) Teledyne Technologies Inc. (03104) | ||
| 23052738 | 2810-01-446-6543 | Screen Assembly | III End Item Identification: C130-J hercules acft | Rolls-Royce Corporation (63005) | |
| 23052738 | 2810-01-473-6631 | Screen Assy, Oil Sca | Rolls Royce Corp. (1E0F1) | ||
| 23052738 | 2810-01-475-7926 | Screen Assy | III End Item Identification: C130J fixed wing aircraft | Allison Transmission Inc. (73342) | |
| 23058479 | 2810-01-509-7054 | Guard, Gasoline Engine, Aircraft | Rolls-Royce Corporation (63005) | ||
| 23058481 | 2810-01-509-7056 | Guard, Gasoline Engine, Aircraft | Rolls-Royce Corporation (63005) | ||
| 23060896 | 2810-01-573-4160 | Ring, Piston | Rolls-Royce Corporation (63005) | ||
| 23061010 | 2810-01-502-0696 | Liner, Bearing | III End Item Identification: Models AE2100A, C and AE2100D2, D3, J aircraft engines Special Features: Liner, bearing hsg-aft carrier | Rolls-Royce Corporation (63005) | |
| 23064370 | 2810-01-463-8880 | Screen Assy, Oil Sca | Rolls Royce Corp. (1E0F1) |