Aircraft and Missile Prime Movers Engine Fuel System Components: 51-0048-2, 5106T85P12, 5106T85P13
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 51-0048-2 5100482 | 2915-00-446-7903 | Screen and Valve Assembly | General Characteristics Item Description: Steel body, pleated dutch weave stainless steel screen, ball valve, spring operated, 1.150 in. lg first end 0.605 in. dia, second end 0.735 in. dia, nominal particle retention 0.0012 III Fsc Application Data: Fuel filter, engine, aircraft | Grimes Aerospace Company (72914) | |
| 51-0050-1 5100501 | 2915-00-627-4830 | Spring, Helical | Grimes Aerospace Company (72914) | ||
| 51-0052-2 5100522 | 2915-00-627-4831 | Housing, Filter, Fuel | Grimes Aerospace Company (72914) | ||
| 51-0052-3 5100523 | 2915-00-706-8467 | Housing, Fuel Filter | Grimes Aerospace Company (72914) | ||
| 51-0055-1 5100551 | 2915-00-627-4832 | Poppet, Filter, Fuel | Grimes Aerospace Company (72914) | ||
| 51005-6 510056 | 2915-00-505-0033 | Piston and Sleeve a | Hydro-Aire Inc. (81982) | ||
| 51007 | 2915-00-938-4201 | Block, Splice, Fuel Control | III End Item Identification: J79-GE-17 aircraft engine fuel control, P/N 311D893P09 | Sealtron Inc. (97814) | |
| 510-07055 51007055 | 2915-01-292-4940 | Switch, Liquid Level | Anchor Scientific Inc. (63541) Marshall-ORR LTD (U4272) | ||
| 510-14056-502 51014056502 | 2915-01-345-6768 | Switch, Liquid Level | III End Item Identification: Aircraft model A-6B Overall Length: 20.390 inches nominal Operating Temp Rating: 65.0 deg fahrenheit minimum and 160.0 deg fahrenheit maximum | The Boeing Company (82918) | |
| 510-14060-1 510140601 | 2915-01-338-0380 | Valve, Fuel Pressurizing and Drai | The Boeing Company (82918) | ||
| 510-14128-503 51014128503 | 2915-01-347-4204 | Sleeve, Cooling, Fuel Injection No | General Characteristics Item Description: Aluminum alloy, QQ-A-225/8, alloy 6061-T4; plastic polyurethane, MIL-C-83286, color 17925, FED-STD-595; 4.022 in. square with chamfered corners; 4 mtg holes 0.339 in. min and 0.343 in. max dia on bolt circle of 4.017 in. min and 4.027 in. max; 4 additional mtg holes for inserts MS21209F5-10P; center hole 2.500 in. dia | The Boeing Company (82918) | |
| 5102T11G01 | 2915-01-491-3092 | Tube Assembly, Aircraft Engine | III End Item Identification: Ge F414-400 aircraft engine Special Features: Ndi inspected and pressure tested III Part Name Assigned By Controlling Agency: Tube, oil, scavenge-front frame | General Electric Company (99207) | |
| 5102T36P01 | 2915-01-491-3269 | Tube Assembly, Aircraft Engine | III End Item Identification: Ge F414-400 engine Special Features: No. 2 bearing seal drain tube Criticality Code Justification: AGAV | General Electric Company (99207) | |
| 5106 | 2915-00-172-2657 | Regulator, Air Pressure | III End Item Identification: Aircraft engine model TF30 | Triumph Group Operations Inc., The (26101) | |
| 5106T85P07 | 2915-01-443-4318 | Pump, Fuel, jet Engine | III End Item Identification: Preprovisioning support navicp is poe | General Electric Company (99207) | |
| 5106T85P09 | 2915-01-443-4318 | Pump, Fuel, jet Engine | III End Item Identification: Preprovisioning support navicp is poe | General Electric Company (99207) | |
| 5106T85P10 | 2915-01-470-5398 | Pump, Fuel, jet Engine | III End Item Identification: Ge F414-400 engine | General Electric Company (99207) | |
| 5106T85P11 | 2915-01-470-7229 | Pump, Fuel, jet Engine | III End Item Identification: Ge 414-400 engine | General Electric Company (99207) | |
| 5106T85P12 | 2915-01-470-5397 | Pump, Fuel, jet Engine | III End Item Identification: Ge F414-400 engine | General Electric Company (99207) | |
| 5106T85P13 | 2915-01-511-3023 | Pump, Fuel, jet Engine | General Electric Company (99207) |