Aircraft Prime Moving Engine System Cooling Components: 8A583-000, 8A800-020, 92011
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 8A583-000 8A583000 | 2935-00-821-8752 | Valve, Thermostatic | General Characteristics Item Description: For support of UH-1N acft | Standard-Thomson Corporation (78493) | |
| 8A800-020 8A800020 | 2935-01-387-9293 | Parts kit, Oil Cooler | Special Features: Esdc unknown | Standard-Thomson Corporation (78493) | |
| 8A860-009 8A860009 | 2935-01-421-3264 | Thermal Package, Val | Standard-Thomson Corporation (78493) | ||
| 8B234-000 8B234000 | 2935-01-055-9435 | Thermal Element Assembly | III End Item Identification: F16A/B aircraft III Fsc Application Data: Engine cooling system component, aircraft General Characteristics Item Description: 4.518 in. l | Standard-Thomson Corporation (78493) | |
| 8B240-000 8B240000 | 2935-01-091-7459 | Valve, Oil Bypass | End Item Identification: Heat exchanger; nsn 2935010852864; fscm 12536; P/N 12/17-000, E/I F16A/B aircraft General Characteristics Item Description: 2.720 porm .020 in. lg; 1.193 in. dia, valve seated 125 deg F porm 5 deg f; valve .180 min open at 110 deg F and below, valve remain seated for all oil pressures below 60 psi at 140 deg F, temp range minus 65 deg F to plus 350 deg F, fluid MIL-L-7808 oil, cap, seat cage, housing, guide, spring cup, end cup alum 6061-T6 ams 4117 or 2024-T4 ams 4120; valve plug, piston, piston ext type 303 stainess steel ams 5640; springs type 302 stainless steel ams 5688; safety wire stainless steel FS302 or FS304 cond a; tet ring PHIS-7M stainless steel; spring ret bronze astm B140; O-ring seals buna-N MIL-R-7362 type 1; sleeve viton; washer polytetrafluoroethylene ams 3651; thermal fill wax, cap, seat cage, housing, guide, spring cup, end cup clear anodize MIL-A-8625 type ii class 1 OR2; valve plug, piston, piston ext passivate MIL-S-5002; ret ring passivated FSC Application Data: Engine cooling system components, aircraft | Standard-Thomson Corporation (78493) | |
| 8B241-000 8B241000 | 2935-01-055-9436 | Cap, Heat Exchanger | III End Item Identification: F16A/B aircraft III Fsc Application Data: Engine colling system component, aircraft General Characteristics Item Description: Aluminum 6061-T6; 1.459 in. l | Grimes Aerospace Company (72914) Standard-Thomson Corporation (78493) | |
| 8B622 | 2935-01-243-7818 | Valve, Fuel | III End Item Identification: Heat exchanger, P/N UA538100-1, nsn 2935-01-112-9354 General Characteristics Item Description: 4.775 in.l.; first end 0.187 in.dia; second end 0.406 in. dia | Standard-Thomson Corporation (78493) | |
| 8B622-000 8B622000 | 2935-01-188-1944 | Thermal Valve | III End Item Identification: U/O heat exchanger cage 78493 P/N 5E800-502; E/I F16C/D acft eng cooling system components, aircraft General Characteristics Item Description: Matl al aly chem treat MIL-C-5541; cres pass; copper aly nickel plated QQ-N-290 cl 2 type vi; 4.777 in. lg | Grimes Aerospace Company (72914) Standard-Thomson Corporation (78493) Stant Mfg Co. Inc. (78225) | |
| 8T7584 | 2935-01-286-9169 | Ring, Wearing | Caterpillar Inc. (11083) | ||
| 9004M31G01 | 2935-00-420-9902 | Manifold, Fluid Cooler | Special Features: Upper manifold section Inlet Connection Type: HOSE Material: Steel, corrosion resisting | General Electric Company (07482) | |
| 9004M32G01 | 2935-00-435-5524 | Manifold, Fluid Cooler | Special Features: Lower manifold section Inlet Connection Type: HOSE Material: Steel, corrosion resisting | General Electric Company (07482) | |
| 9004M38G02 | 2935-00-420-9902 | Manifold, Fluid Cooler | Special Features: Upper manifold section Inlet Connection Type: HOSE Material: Steel, corrosion resisting | General Electric Company (07482) | |
| 9004M40G01 | 2935-00-435-5524 | Manifold, Fluid Cooler | Special Features: Lower manifold section Inlet Connection Type: HOSE Material: Steel, corrosion resisting | General Electric Company (07482) | |
| 9004M40G02 | 2935-00-435-5524 | Manifold, Fluid Cooler | Special Features: Lower manifold section Inlet Connection Type: HOSE Material: Steel, corrosion resisting | General Electric Company (07482) | |
| 9004M42G01 | 2935-00-420-9902 | Manifold, Fluid Cooler | Special Features: Upper manifold section Inlet Connection Type: HOSE Material: Steel, corrosion resisting | General Electric Company (07482) | |
| 9004M42G02 | 2935-01-158-4313 | Manifold, Fluid Cooler | III Fsc Application Data: Engine cooling system components, aircraft Special Features: Manifold, air, upper no. 9004M42 Inlet Connection Type: HOSE | General Electric Company (07482) | |
| 9004M43G01 | 2935-00-435-5524 | Manifold, Fluid Cooler | Special Features: Lower manifold section Inlet Connection Type: HOSE Material: Steel, corrosion resisting | General Electric Company (07482) | |
| 9004M43G02 | 2935-01-158-4314 | Manifold, Fluid Cooler | III Fsc Application Data: Engine cooling system components, aircraft Special Features: Manifold, air, lower no. 9004M43 Inlet Connection Type: HOSE | General Electric Company (07482) | |
| 907385-3 9073853 | 2935-01-406-7947 | Manifold, Fluid Cooler | III End Item Identification: Air augmenter oil cooler duct outbd nac | Lockheed Martin Corporation (98897) | |
| 92011 | 2935-00-455-2232 | Cover, Shipping, Cool | IRL Thermal Systems LTD (U1841) |