FSC 4920 Aircraft Maintenance and Repair Shop Specialized Equipment: 4920-01-213-2536, 4920-01-213-2539, 4920-01-213-3851
NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
4920-01-213-2536 4920012132536 | 123SAV56608-1 | Test Adapter Assembly | Northrop Grumman Systems Corporation (26512) | ||
4920-01-213-2537 4920012132537 | 128SAV61684-3 | Cable, Special, Assembly | Northrop Grumman Systems Corporation (26512) | ||
4920-01-213-2538 4920012132538 | 128SAV61684-5 | Cable, Special, Assembly | Northrop Grumman Systems Corporation (26512) | ||
4920-01-213-2539 4920012132539 | 128SAV61684-7 | Cable, Special, Assembly | Northrop Grumman Systems Corporation (26512) | ||
4920-01-213-2540 4920012132540 | 128SAV61684-9 | Cable, Special, Assembly | Northrop Grumman Systems Corporation (26512) | ||
4920-01-213-2541 4920012132541 | 128SAV62061-3 | Cable, Special, Assembly | Northrop Grumman Systems Corporation (26512) | ||
4920-01-213-2946 4920012132946 | H06G1538-1003 | Adapter set, Test | McDonnell Douglas Corp. (12464) | ||
4920-01-213-2961 4920012132961 | PWA70180 | Fixture, Engine Maintenance, Aircr | Special Features: Stainless steel and aluminum; C/O a round plate with strap clamps, fittings, adapter and plugs; company item name-fixture Functional Description: Used to flush out the chip/tailings from the oil hole bushing repair. locates and secures the no. 2 bearing support on the rear I.D. and adjacent flange End Item Identification: F-100-PW-100/200/220/220E/229 engines | United Technologies Corporation (77445) | |
4920-01-213-3011 4920012133011 | R-TBD-3324 14E74000-001 | Tube set, Transfer | Boeing Company, The (43999) | ||
4920-01-213-3012 4920012133012 | R-TBD-3300 14E76000-001 14E76000-003 | Adapter Plate, Test Stand | Boeing Company, The (43999) | ||
4920-01-213-3013 4920012133013 | 14E89000-001 R-TBD-3329 | Adapter, Manifold, Test Stand | Boeing Company, The (43999) | ||
4920-01-213-3020 4920012133020 | 3C3217P03 | Fixture, Aircraft Maintenance | General Electric Company (07482) | ||
4920-01-213-3198 4920012133198 | 16U80638-3 | Adapter, Test | Lockheed Martin Corporation (81755) | ||
4920-01-213-3199 4920012133199 | 2D10156G01 | Adapter, Test | Northrop Grumman Systems Corporation (18323) | ||
4920-01-213-3200 4920012133200 | 2D10122G01 | Adapter, Test | Northrop Grumman Systems Corporation (18323) | ||
4920-01-213-3847 4920012133847 | 99-593 | Manifold, Test | Hydro-Aire Inc. (81982) | ||
4920-01-213-3848 4920012133848 | GS21174-1 | Fixture, Aircraft Maintenance | Hamilton Sundstrand Corporation (73030) | ||
4920-01-213-3849 4920012133849 | 9455M19G01 | Adapter set, Aircraft Maintenance | Special Features: 4140 STEEL;130.0 in by 20.0 in O/d; provides interface between cdp seal and hydraulic chuck of high speed grinder during overhaul of high pressure compressor rotor End Item Identification: F101-GE-102 engine B-1B acft age. | General Electric Company (07482) | |
4920-01-213-3850 4920012133850 | PWA70202 | Fixture, Engine Maintenance, Aircr | Special Features: C/O hydraulic chuck that locates the part on prime O.D. and is secured uses strap clamps; made of steel Functional Description: Used to secure rr compressor stator linkage arm bearing during machining of I.D. End Item Identification: F100-PW-100/200 | United Technologies Corporation (77445) | |
4920-01-213-3851 4920012133851 | 21C5839G03 | Fixture, Engine Maintenance, Aircr | Special Features: C/O diamond grinding wheels;backup rings; fixture indexing clamps Functional Description: Maintenance fixture, high pressure turbine;used for selective grinding of high pressure turbine stator SHROUDS;28.0 in DIA;15.0 in H;300 lbs End Item Identification: TF34-GE-100/100A turbofan engine age. | Boniface Tool & DIE Inc. (63259) General Electric Company (99207) |