Aircraft and Missile Prime Movers Engine Fuel System Components: 16S442-7, 16VP005-3, 1700466
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 16S442-7 16S4427 | 2915-01-050-0761 | Sleeve, nut, Ejector, Fuel Pylon | III End Item Identification: F16 acft General Characteristics Item Description: Dia. 2.218 in. III Fsc Application Data: Aircraft fuel system | Lockheed Martin Corporation (81755) | |
| 16VP004-300 16VP004300 | 2915-01-060-6851 | Cartridge Assembly, Fuel Transfer | III End Item Identification: F16A & b aircraft wing tank General Characteristics Item Description: Use with 1646T100-5 turbine driven fuel transfer pump III Fsc Application Data: Acft fuel system | Lockheed Martin Corporation (81755) | |
| 16VP004-4 16VP0044 | 2915-01-463-5076 | Pump, Fuel, jet Engine | Overall Length: 4.280 inches nominal Overall Height: 3.090 inches nominal Overall Width: 3.270 inches nominal | Lockheed Martin Corporation (81755) | |
| 16VP004-400 16VP004400 | 2915-01-235-5188 | Cartridge Assembly, Fuel Transfer | Functional Description: Used W/turbine-driven transfer pump, P/N 2484, spec control 16VP004-4 General Characteristics Item Description: 3.10 in. max H, 2.00 in. max od FSC Application Data: F16A/B acft fuel system | Lockheed Martin Corporation (81755) | |
| 16VP005-3 16VP0053 | 2915-01-053-7764 | Filter, Fluid | III End Item Identification: F-16 aircraft III Fsc Application Data: Fuel system, gas turbine engine, aircraft III Part Name Assigned By Controlling Agency: Quick disconnect/strainer, fuel line | Lockheed Martin Corporation (81755) | |
| 16VP005-4 16VP0054 | 2915-01-083-0431 | Filter, Fluid | III End Item Identification: F-16 aircraft III Fsc Application Data: Fuel system, gas turbine engine, aircraft III Part Name Assigned By Controlling Agency: Quick disconnect/strainer, fuel | Lockheed Martin Corporation (81755) | |
| 16VP005-5 16VP0055 | 2915-01-179-3834 | Filter, Fluid | Filtration Rating in Microns: 40.0 nominal End Item Identification: F-16 aircraft Design Type: Reusable | Lockheed Martin Corporation (81755) | |
| 16VP006 | 2915-01-041-4481 | Proportioner, Fuel Pump | End Item Identification: F-16A/B model engine FSC Application Data: Fuel system acft engine | Lockheed Martin Corporation (81755) | |
| 16VP006-1 16VP0061 | 2915-01-041-4481 | Proportioner, Fuel Pump | End Item Identification: F-16A/B model engine FSC Application Data: Fuel system acft engine | Lockheed Martin Corporation (81755) | |
| 16VP006-2 16VP0062 | 2915-01-041-4481 | Proportioner, Fuel Pump | End Item Identification: F-16A/B model engine FSC Application Data: Fuel system acft engine | Lockheed Martin Corporation (81755) | |
| 16VP006-3 16VP0063 | 2915-01-041-4481 | Proportioner, Fuel Pump | End Item Identification: F-16A/B model engine FSC Application Data: Fuel system acft engine | Lockheed Martin Corporation (81755) | |
| 16VP012-1 16VP0121 | 2915-00-941-9631 | Valve, Fuel Shutoff | III End Item Identification: Aircraft engine fuel control valve assy, P/N A6834 General Characteristics Item Description: Stainless steel and aluminum alloy, passivated and anodized finish, electrically operated, 28 volts, direct current, O/a dim. approx 9.217 in. lg by 2.656 in. H by 5.000 in. W, concentric-eared flange W/6 holes | Lockheed Martin Corporation (81755) | |
| 16VP013-1 16VP0131 | 2915-01-454-6663 | Pump, Fuel, Metering and Distribut | End Item Identification: F-16 acft, F-100 eng Part Name Assigned BY Controlling Agency: Pump, dual inlet, fuel Material: Aluminum alloy | Lockheed Martin Corporation (81755) | |
| 16VP014-1 16VP0141 | 2915-01-454-4612 | Pump, Fuel, Metering and Distribut | III End Item Identification: F16 Criticality Code Justification: AGAV III Purchase Description Identification: 26433-9C125-3 | Lockheed Martin Corporation (81755) | |
| 16VP035-1 16VP0351 | 2915-01-057-5545 | Valve, Fuel Divider | End Item Identification: Acft F16A and b model General Characteristics Item Description: 3.82 in.lg, 2.42 in.W, 3.10 in. H FSC Application Data: Acft fuel system | Lockheed Martin Corporation (81755) | |
| 16VP035-2 16VP0352 | 2915-01-057-5545 | Valve, Fuel Divider | End Item Identification: Acft F16A and b model General Characteristics Item Description: 3.82 in.lg, 2.42 in.W, 3.10 in. H FSC Application Data: Acft fuel system | Lockheed Martin Corporation (81755) | |
| 16VP035-2 16VP0352 | 2915-01-075-9723 | Valve, Fuel Flow Divider | End Item Identification: F-16A&B usaf General Characteristics Item Description: 3.820 in. lg, 2.420 in. W, 3.100 in. H. inlet FLOW-20-225 ppm. operating FLUID-JP-4 or JP-5. ambient temperature M65 deg F to 165 deg F. max inlet-outlet pressure, drop 15 psid at 160 ppm in FSC Application Data: Acft eng fuel system components | Lockheed Martin Corporation (81755) | |
| 16VP050-1 16VP0501 | 2915-01-186-2454 | Module, Fail-Safe, Valve | III End Item Identification: Fuel system, F-16 aircraft General Characteristics Item Description: Elec load 4.0 amp max 28VDC (inductive); module design per MIL-STD-454G III Functional Description: To assure that only open elec signal is applied to main fuel shutoff valve when, thru malfunction, both an open and close signal are applied at input connector | Lockheed Martin Corporation (81755) | |
| 1700-2533 17002533 | 2915-01-582-1692 | Duel Coil Solenoid | Special Features: From operating engine fun/stop levers, throttles, chokes, valves and clutches to protecting expensive diesel engines from overspeed, low lube pressure and high temperature | Woodward Governor Company (31361) | |
| 1700465 | 2915-01-507-7741 | Pump Assembly, Submerged, Aircraft | Hamilton Sundstrand Corporation (99167) | ||
| 1700466 | 2915-01-507-7744 | Pump Assembly, Submerged, Aircraft | Hamilton Sundstrand Corporation (99167) |