Aircraft Landing Gear Components: 114L2437-1, 114L2441-1, 114LK103-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 114L2437-1 114L24371 | 1620-00-871-8658 | Sleeve and Poppet a | The Boeing Company (77272,81205) | ||
| 114L2440-1 114L24401 | 1620-00-871-8657 | Cap, End Relief Valv | III End Item Identification: CH-47, rotary wing aircraft | The Boeing Company (77272,81205) | |
| 114L2440-1C 114L24401C | 1620-00-871-8657 | Cap, End Relief Valv | III End Item Identification: CH-47, rotary wing aircraft | The Boeing Company (77272) | |
| 114L2441-1 114L24411 | 1620-00-871-8656 | Cap, End Adjustment | III End Item Identification: CH-47, rotary wing aircraft | The Boeing Company (77272,81205) | |
| 114L2448-1 114L24481 | 1620-00-869-9005 | Sleeve and Spool as | Circor Aerospace Inc. (50601) The Boeing Company (77272,81205) | ||
| 114L2463 | 1620-00-906-3894 | Housing, Potentiometer | General Characteristics Item Description: Aluminum alloy QQ-A-601C T6;L 1.810 in., W 1.840 in., dia 1.600 in. | The Boeing Company (77272) | |
| 114L2463-2 114L24632 | 1620-00-906-3894 | Housing, Potentiometer | General Characteristics Item Description: Aluminum alloy QQ-A-601C T6;L 1.810 in., W 1.840 in., dia 1.600 in. | Forway Industries Inc. (00641) The Boeing Company (77272) | |
| 114L2470 | 1620-00-435-7840 | End cap, Power Steering | General Characteristics Item Description: Aluminum alloy 2014-T6;L 1.090 in.;first end hexagon head width across plats 0.750 in., 3 drilled holes dia 0.047 in.;second end threaded 0.500-20UNF-3A, od 0.312 in., id 0.190 in. | The Boeing Company (77272) | |
| 114L2470-1 114L24701 | 1620-00-435-7840 | End cap, Power Steering | General Characteristics Item Description: Aluminum alloy 2014-T6;L 1.090 in.;first end hexagon head width across plats 0.750 in., 3 drilled holes dia 0.047 in.;second end threaded 0.500-20UNF-3A, od 0.312 in., id 0.190 in. | Manth-Brownell Inc. (07592) The Boeing Company (77272) | |
| 114L2474-1 114L24741 | 1620-00-442-2610 | Filtering Disk, Fluid | Body Diameter: 0.146 inches minimum and 0.156 inches maximum Filtration Rating in Microns: 10.0 nominal Body Thickness: 0.057 inches minimum and 0.067 inches maximum | The Boeing Company (77272) | |
| 114L2498-1 114L24981 | 1620-00-906-3897 | Plate, Mounting, Land | The Boeing Company (77272,81205) | ||
| 114L2510-1 114L25101 | 1620-00-869-2420 | Fitting, Shock Strut | The Boeing Company (77272,81205) | ||
| 114L2514-1 114L25141 | 1620-00-868-9791 | Retainer, Shock Stru | The Boeing Company (77272,81205) | ||
| 114L2515-1 114L25151 | 1620-00-869-2421 | End Fork Lock | Special Features: Static lock aft landing gear Overall Length: 2.375 inches nominal | The Boeing Company (77272,81205) | |
| 114L2516-1 114L25161 | 1620-00-869-2416 | Link, Static Lock | The Boeing Company (77272,81205) | ||
| 114L2520-1 114L25201 | 1620-00-872-6119 | Spacer, Lock out, Aft | The Boeing Company (77272,81205) | ||
| 114L2528-1 114L25281 | 1620-00-906-1266 | Plug, Axle, Landing g | The Boeing Company (77272,81205) | ||
| 114L2529-1 114L25291 | 1620-00-868-9793 | Spacer, Shock Strut | The Boeing Company (77272,81205) | ||
| 114L2532-1 114L25321 | 1620-00-872-7890 | Cap Assembly, End, Af | The Boeing Company (77272,81205) | ||
| 114LK103-1 114LK1031 | 1620-00-980-1857 | Parts kit, Swivel Ho | III End Item Identification: Grumman aircraft, model A10 | The Boeing Company (77272,81205) |