Aircraft and Missile Prime Movers Engine Fuel System Components: 7446735, 7451-1, 746346
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 7446735 | 2915-00-907-5260 | Pump, Submerged, Aircraft | General Characteristics Item Description: Designed for partially submerged operation, positive displacement, air turbine driven 7 lbs per min rating, 8000 rpm, 10000 phr at, 20 psi discharge pressure, internal square flange pump discharge port 5 holes, 11 slots, evenly spaced around 8 in. dia mtg flange, 10000 in. lg parallel to shaft axis, 9.500 in. lg perpendicular to shaft axis, 8 in. W perpendicular to shaft axis, O/a dim. | Boeing Company, The (88277) | |
| 7451-1 74511 | 2915-00-289-3944 | Valve, Fuel Drain | III End Item Identification: 29159850204 General Characteristics Item Description: Aluminum alloy, anodize finish, 2.270 in. O/a lg 1.781 in. O/a dia, 1 tube 0.250 in. O/a dia, consists of 16 each, components | Parker Hannifin Corporation (92003) | |
| 7451-2 74512 | 2915-00-876-0923 | Valve Assy, Fuel | Parker Hannifin Corporation (92003) | ||
| 745352 | 2915-00-126-0160 | Fuel Control, Main, Turbine Engine | United Technologies Corporation (77445) | ||
| 745366 | 2915-01-316-7784 | Support, Bearing | III End Item Identification: Engine model F-404 | Hamilton Sundstrand Corporation (99167) | |
| 74-550056-203 74550056203 | 2915-01-231-7736 | Valve, Float, Aircraft Fuel Tank | Boeing Company, The (76301) | ||
| 74556 | 2915-01-360-2969 | Injector Assembly, Fuel | Textron Lycoming Inc. (80254) | ||
| 74-580110-111 74580110111 | 2915-01-156-0876 | Valve, Interconnect | End Item Identification: Acft model F-18 General Characteristics Item Description: Housing aluminum alloy per MIL-A-21180; 5.938 in. O/a lg; 5.073 in. O/a h; 2.651 in. O/a w; fluid gasoline per MIL-G-5572; 0.0 to 12.0 psig; M65.0 to P160.0 deg F temp rating | Boeing Company, The (76301) | |
| 74-580110-119 74580110119 | 2915-01-156-0876 | Valve, Interconnect | End Item Identification: Acft model F-18 General Characteristics Item Description: Housing aluminum alloy per MIL-A-21180; 5.938 in. O/a lg; 5.073 in. O/a h; 2.651 in. O/a w; fluid gasoline per MIL-G-5572; 0.0 to 12.0 psig; M65.0 to P160.0 deg F temp rating | Boeing Company, The (76301) | |
| 74-580142-109 74580142109 | 2915-01-454-6718 | Valve, Fuel Pressurizing and Drai | III End Item Identification: Preprovisioning support navicp is poe | Boeing Company, The (76301) | |
| 74-580191-111 74580191111 | 2915-01-454-6734 | Valve, Fuel Pressurizing and Drai | Boeing Company, The (76301) | ||
| 74-580191-111 74580191111 | 2915-01-509-9509 | Valve, Fuel Pressurizing and Drai | III End Item Identification: Fighter aircraft-first (F18 E/f). Criticality Code Justification: AGAV | Northrop Grumman Systems Corporation (76823) | |
| 74-580191-111 74580191111 | 2915-01-542-9496 | Valve, Fuel System | III End Item Identification: Aircraft model code for F/A-18E/F Special Features: Thermal management. item name: valve, fuel pressure | Northrop Grumman Systems Corporation (76823) | |
| 74-580191-112 74580191112 | 2915-01-509-9503 | Valve, Fuel Pressurizing and Drai | III End Item Identification: Fighter aircraft-first (F18 E/f). Criticality Code Justification: AGAV | Boeing Company, The (76301) | |
| 74-580191-113 74580191113 | 2915-01-542-7593 | Valve, Fuel Pressurizing and Drai | III End Item Identification: F-18 E/F fighter aircraft III Part Name Assigned By Controlling Agency: Inavy valve, fuel pressure Criticality Code Justification: AGAV | Boeing Company, The (76301) | |
| 74-580198-203 74580198203 | 2915-01-454-5059 | Actuator, Electro-Mechanical, Rota | III End Item Identification: F18 E/F aircraft Criticality Code Justification: AGAV | Boeing Company, The (76301) | |
| 74581 | 2915-00-896-9811 | Shaft and Plate Assembly | III End Item Identification: Engine acft J85 fuel pump 9233A4 | Goodrich Corporation (11599) | |
| 745908 | 2915-01-011-8731 | Connector, Fuel Pump | III End Item Identification: Acft engine TF33 fuel pump General Characteristics Item Description: 90 deg angle tube connection one end 1.187-12 NS3A thd 0.475 in. lg, 2.380 in. sq flange other end W/4 mtg holes 0.344 in. dia equispaced 1.756 in.C to C. | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 745911 | 2915-01-012-2872 | Elbow, Fuel Control | III End Item Identification: Acft engine TF33 fuel control General Characteristics Item Description: Aluminum alloy, 45 deg angle tube connection 1.500-12 NS3A thd 0.508 in. lg one end, triangular shaped mtg flange W/3 holes 0.345 in. dia irregularly spaced other end for fuel outlet | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 745912 | 2915-01-012-3207 | Connector, Fuel Pump | III End Item Identification: Acft engine TF33PW100 fuel pump General Characteristics Item Description: Aluminum alloy, ams 4215, two plain tube connections one end W/ 1.500-12 NS3A thd 0.508 in. lg, triangular shaped flange other end W/ 3 mtg holes equispaced on 2.023 in. dia circle for fuel inlet | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (52661,77445) | |
| 74633 | 2915-00-886-9671 | Lever, Stop | III End Item Identification: T-53 series engines | Goodrich Corporation (11599) | |
| 746346 | 2915-01-011-8828 | Fuel Control, Main, Turbine Engine | United Technologies Corporation (77445) |