Aircraft Landing Gear Components: 123SCL5000-1, 1243421-3, 12567-4
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 123SCL5000-1 123SCL50001 | 1620-00-479-8749 | Shock Strut Assy, La | Northrop Grumman Systems Corporation (26512) | ||
| 123SCL5000-2 123SCL50002 | 1620-00-494-8606 | Strut Assembly, Righ | General Characteristics Item Description: Matl-corrosion resisting steels, aluminum alloy components, magnesium shall not be used for structural application, use titaniumand titanium base alloys, structural fittings shall be made fromaluminum, steel or titanium | Northrop Grumman Systems Corporation (26512) | |
| 123SCL5001-1 123SCL50011 | 1620-00-003-0392 | Drag Brace, Landing Gear | Special Features: All parts of unit shall be made of cres matl or suitably protected against corrosion, internally and externally;c/O shock strut plus attaching parts Reference Number Differentiating Characteristics: As modified by mfr source controlling dwg no. 123SCL5001-1FSCM 26512 | Northrop Grumman Systems Corporation (26512) | |
| 123SCL5001-2 123SCL50012 | 1620-00-003-0393 | Drag Brace, Landing Gear | Special Features: All parts of unit shall be made of cres matl or shall be suitably protected against corrosion, internally and externally.C/O shock strut plus attaching parts Reference Number Differentiating Characteristics: As modified by mfr source controlling dwg no. 123SCL5001-2FSCM 26512 | Northrop Grumman Systems Corporation (26512) | |
| 123SCL5003-1 123SCL50031 | 1620-00-003-0391 | Drag Brace, Landing Gear | Special Features: All parts of unit shall be made of cres matl or suitably protected against corrosion, internally and externally.C/O a strut assy plus attaching parts Reference Number Differentiating Characteristics: As modified by mfr source controlling dwg no. 123SCL5003-1FSCM 26512 | Northrop Grumman Systems Corporation (26512) | |
| 123SCL5003-3 123SCL50033 | 1620-01-408-6637 | Drag Brace, Landing Gear | Northrop Grumman Systems Corporation (26512) | ||
| 123SCL6000-1 123SCL60001 | 1620-01-213-2228 | Landing Gear, Retractable | Northrop Grumman Systems Corporation (26512) | ||
| 123SCL6000-2 123SCL60002 | 1620-01-213-2229 | Landing Gear, Retractable | Northrop Grumman Systems Corporation (26512) | ||
| 123SCL6002-1 123SCL60021 | 1620-01-221-2698 | Landing Gear, Retractable | Northrop Grumman Systems Corporation (26512) | ||
| 123SCL6003-1 123SCL60031 | 1620-01-221-2708 | Drag Brace, Landing Gear | III End Item Identification: Aircraft model C-2A III Part Name Assigned By Controlling Agency: Drag brace alighting gear - nose wheel Aircraft for Which Designed: C2A | Northrop Grumman Systems Corporation (26512) | |
| 1241L009 | 1620-00-045-5780 | Bleeder Assembly, Shock Absorber | General Characteristics Item Description: 0.500 in. hex. head, cres, 0.870 in. approx lg, 180 deg angle of seat | Circor Aerospace Inc. (50601) Goodrich Corp. (17576) Smith and Smith Aircraft Co. (28298) | |
| 1243421-3 12434213 | 1620-00-992-0517 | Roller, Trunnion | Cessna Aircraft Company (71379) | ||
| 1243626 | 1620-00-992-0463 | Support, Ring Pack | Cessna Aircraft Company (71379) | ||
| 1243626-1 12436261 | 1620-00-992-0463 | Support, Ring Pack | Cessna Aircraft Company (71379) | ||
| 1244955-101 1244955101 | 1620-00-279-3727 | Collar, Launch bar, Nose Landing g | III End Item Identification: Aircraft model S-3A Criticality Code Justification: AGAV | Lockheed Martin Services Inc. (1WL60) | |
| 125053 | 1620-00-868-3497 | Retainer, Filter cyl | Parker-Hannifin Corporation (93835) | ||
| 125057 | 1620-00-868-3498 | Bracket and Yoke Assembly | III End Item Identification: C-141 aircraft | Parker-Hannifin Corporation (93835) | |
| 125071 | 1620-00-872-2357 | Retainer, Spring | Parker-Hannifin Corporation (93835) | ||
| 125075 | 1620-00-868-3499 | Retainer, Valve | Parker-Hannifin Corporation (93835) | ||
| 12567-4 125674 | 1620-00-771-7122 | Spring, Tail | Piper Aircraft Inc. (77294) |