Aircraft Prime Moving Engine System Cooling Components : 2650266, 2A264, 35001-2
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2650266 | 2935-00-307-2780 | Cap, Filler Opening | Outside Diameter: 4.250 inches minimum and 4.500 inches maximum System for Which Designed: Pressurized Retaining Device Type: Chain | Parker Hannifin Corporation (92003) | |
| 2651-94 265194 | 2935-00-309-1497 | Cap, Filler Opening | Rockwell Collins Electromechanical (86831) | ||
| 2651-94A 265194A | 2935-00-309-1497 | Cap, Filler Opening | Rockwell Collins Electromechanical (86831) | ||
| 269D4518-165 269D4518165 | 2935-01-677-0194 | Tube Assembly, Aircraft Engine | End Item Identification: MQ-8B firescout Aircraft Mission Design Series: MQ8B | Northrop Grumman Corporation (78022) Northrop Grumman Systems Corporation (78JW8) | |
| 269D4528-1 269D45281 | 2935-01-677-3886 | Cap, Filler Opening | End Item Identification: MQ-8B air vehicle Part Name Assigned BY Controlling Agency: Cap, filler opening | Northrop Grumman Corporation (78022) Northrop Grumman Systems Corporation (78JW8) Sikorsky Aircraft Corporation (78286) | |
| 2890046-101 2890046101 | 2935-01-669-4272 | Cap, Filler Opening | End Item Identification: KC-46 air craft Reference Number Differentiating Characteristics: Item is faa certified | ||
| 2935PL0643914 | 2935-00-486-0971 | Gasket, Valve | General Characteristics Item Description: 7.590 in. min, 7.650 in. max lg; 1.970 in. min, 2.030 in. max dia 3 holes; 0.330 in. min, 0.350 in. max dia 8 holes | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2935PL0734930 | 2935-01-440-9157 | Cooler, Lubricating Oil, Engine | End Item Identification: E/I C-130 acft;t.O. 7J1-99-3 | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2935PL0866596 | 2935-01-085-2864 | Cooler, Lubricating Oil, Engine | End Item Identification: T.O.F16-28F-49-20;U/O F100PW100 Special Features: Heat exchanger, fuel | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2935PL0866618 | 2935-01-324-9087 | Cooler, Lubricating Oil, Engine | End Item Identification: F100PW0229 Reference Number Differentiating Characteristics: As differentiated by material | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2935PL0893312 | 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 | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2935PL1602721 | 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 | Inspektorat Wsparcia SIL Zbrojnych (9009H) | |
| 2A264 | 2935-01-269-4729 | Cap, Filler Opening | Thread Class: 3A Outside Diameter: 2.620 inches nominal Overall Height: 4.430 inches nominal | Eaton Aerospace LLC (97484) | |
| 3090311 | 2935-00-640-7476 | Cap, Filler Opening | Gripping Accommodation Type: Handle Outside Diameter: 3.500 inches nominal Overall Height: 2.728 inches minimum and 2.998 inches maximum | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) | |
| 309311 | 2935-00-640-7476 | Cap, Filler Opening | Gripping Accommodation Type: Handle Outside Diameter: 3.500 inches nominal Overall Height: 2.728 inches minimum and 2.998 inches maximum | Turbo Power & Marine System Inc. (11449) United Technologies Corporation (77445) Wisco Products Incorporated (10203) | |
| 3108495-1 31084951 | 2935-01-676-0194 | Cap, Filler Opening | Honeywell International Inc. (99193) | ||
| 315T3128-29 315T312829 | 2935-01-688-7215 | Tube Assembly, Aircraft Engine | The Boeing Company (81205) | ||
| 315T3128-32 315T312832 | 2935-01-688-7172 | Tube Assembly, Aircraft Engine | The Boeing Company (81205) | ||
| 340-311-402-0 3403114020 | 2935-01-690-4577 | Manifold, Fluid Cooler | CFM International Inc. (58828) | ||
| 35001-2 350012 | 2935-00-988-9299 | Cap, Filler Opening | Gripping Accommodation Type: Handle System for Which Designed: Pressurized Cam Quantity: 3 | Parker-Hannifin Corporation (99321) |