Aircraft and Missile Prime Movers Engine Fuel System Components: 6-256-5, 626184-7, 626542A1M
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 6-256-5 62565 | 2915-00-736-4899 | Cage Assy, Float act | Parker Hannifin Corporation (92003) | ||
| 6-256-501 6256501 | 2915-00-736-4898 | Parts kit, Valve, Overall | General Characteristics Item Description: Consist of 13 items | Parker Hannifin Corporation (92003) | |
| 6-256-502 6256502 | 2915-00-971-9151 | Parts kit, Valve, Cure Date | III End Item Identification: Aircraft engine fuel system, P/N 6-256-61 General Characteristics Item Description: Includes 13 parts, closure P/N SP8, deflector P/N 6-256-47, packing, preformed P/ns MS29513-12, -15, -16 and 27, pilot and floats P/ns 6-256-103-1 and -2, screws P/ns LP507-832R4M, R6M and R12M and LP500-8-8M and spring P/N 6-256-40 | Parker Hannifin Corporation (92003) Parker-Hannifin Corporation (3H889,59211) | |
| 6-256-506 6256506 | 2915-00-980-2697 | Parts kit, Valve, Cur | Parker Hannifin Corporation (92003) | ||
| 6-256-61 625661 | 2915-00-618-5925 | Valve, Float, Aircraft Fuel Tank | General Characteristics Item Description: Material data, aluminum alloy body, nonmetallic composition float, aluminum alloy seat seating surface, aluminum alloy disk seating surface; anodized finish on aluminum alloy parts; float data, 3 floats, 15 deg approx effective travel of floats; W/solenoids, 2 solenoids, dc; port data, inlet ports identical, thd female, 1/4 in, od tube, thread data, 7/16-20 thd size, nf, class 3 fit, rh; mtg data, horizontal position, top mtd, 4 mtg holes; fuel data, rated for specific grades of aircraft fuel, spec data, mil, MIL-F-5624; over-all dim., 7.15 in. lg, 3.30 in. W, 3.565 in. H | Parker Hannifin Corporation (92003) Parker-Hannifin Corporation (3H889,59211) | |
| 6-256-64 625664 | 2915-00-736-4896 | Fitting, Electric Lead Port | General Characteristics Item Description: Aluminum alloy, QQ-A-591B, anoidize finish, 0.758 in. O/a lg, first end connection per MS33656-6, 0.250 in. id, flange type on second end, 2.600 in. min, 2.620 in. max flange od, hub on second end, 0.620 in. min, 0.625 in. max hub od, hub protrude 0.074 min, 0.84 in from end of flange | Parker Hannifin Corporation (92003) | |
| 625900 | 2915-00-936-6411 | Cover, Vapor Separator, Fuel Pump | III End Item Identification: Aircraft engine injection system, model EQ6042C, P/N 628203 General Characteristics Item Description: Fits between ejector P/N 625901 and screw P/N AN500A8-12 and on gasket P/N 625548 | Teledyne Industries Inc. (28839) | |
| 625901 | 2915-00-936-6412 | Ejector, Vapor Separator, Fuel Inj | III End Item Identification: Aircraft engine fuel injection system, model EQ6042C, P/N 628203 General Characteristics Item Description: Fits between cover P/N 625900 and 90 deg elbow, vapor return P/N 628437 | Teledyne Industries Inc. (28839) | |
| 625919 | 2915-00-936-6404 | Strainer Element, Sediment | END Item Identification: Fuel control, engine, acft Filtering Media Design: MESH | Teledyne Industries Inc. (28839) | |
| 625921 | 2915-00-936-6403 | Screen, Dust, Fuel Injection Nozzl | III End Item Identification: Aircraft engine fuel injection system, model EQ6042C, P/N 632147-10 General Characteristics Item Description: Fits into shield P/N 625919 and connects to jet P/N 627333-10 | Teledyne Industries Inc. (28839) | |
| 626011 | 2915-01-251-4453 | Pump, Fuel, jet Engine | III End Item Identification: TF30 aircraft engine Reference Number Differentiating Characteristics: As differentiated by source control dwg no. 2186906 III Functional Description: Axial piston pump, supplies high pressure hydraulic power rqrd to actuate eng systems using fuel as hydraulic fluid | United Technologies Corporation (77445) | |
| 626048-1-1 62604811 | 2915-00-341-4330 | Distributor, Fuel | Honeywell International Inc. (06848) | ||
| 626048-1-3 62604813 | 2915-00-341-4331 | Distributor, Fuel | Honeywell International Inc. (06848) | ||
| 626048-1-5 62604815 | 2915-00-341-4332 | Distributor, Fuel | Honeywell International Inc. (06848) | ||
| 626184-4 6261844 | 2915-00-888-4143 | Fuel Control, Main, Turbine Engine | III End Item Identification: Aircraft jet engine model J69-T-25 General Characteristics Item Description: Multi item assembly used in control of jet fuels | Honeywell International Inc. (06848) | |
| 626184-5 6261845 | 2915-00-888-4143 | Fuel Control, Main, Turbine Engine | III End Item Identification: Aircraft jet engine model J69-T-25 General Characteristics Item Description: Multi item assembly used in control of jet fuels | Honeywell International Inc. (06848) | |
| 626184-7 6261847 | 2915-00-888-4143 | Fuel Control, Main, Turbine Engine | III End Item Identification: Aircraft jet engine model J69-T-25 General Characteristics Item Description: Multi item assembly used in control of jet fuels | Honeywell International Inc. (06848) | |
| 626534 | 2915-00-078-0999 | Manifold Assembly, Afterburner Sp | United Technologies Corporation (77445) | ||
| 626542A1 | 2915-00-193-7608 | Valve, Fuel Pressurizing and Drai | III End Item Identification: Aircraft engine model IO-470L General Characteristics Item Description: Steel | Teledyne Industries Inc. (28839) | |
| 626542A1M | 2915-00-193-7608 | Valve, Fuel Pressurizing and Drai | III End Item Identification: Aircraft engine model IO-470L General Characteristics Item Description: Steel | Teledyne Industries Inc. (28839) |