FSC 3040 Miscellaneous Power Transmission Equipment: 3040-00-010-8293, 3040-00-011-1134, 3040-00-011-1202
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3040-00-010-8293 3040000108293 | 128L10027-1 128L10027 | Connecting link, Rigid | Overall Length: 22.250 inches nominal Body Construction: Tubular Link Style: Tubular shank | TEK Precision Co. LTD. (65780) Capy Machine Shop Inc. (0BVP9) Northrop Grumman Systems Corporation (26512) | |
| 3040-00-010-9335 3040000109335 | 547-5194-002 | Gearshaft, Spur | Rockwell Collins Inc. (13499) | ||
| 3040-00-010-9336 3040000109336 | 547-5195-002 | Cam, Control | Special Features: Stainless STEEL;0, 656 in. DIA;0.343 in. H;0.156 in. ctr hole | Rockwell Collins Inc. (13499) | |
| 3040-00-010-9340 3040000109340 | 547-5230-002 | Shaft, Spur Gear | Rockwell Collins Inc. (13499) | ||
| 3040-00-010-9358 3040000109358 | 543-9994-002 | Plate, Retaining, Shaft | Material: Steel Thickness: 0.123 inches nominal Outside Diameter: 0.649 inches nominal | Rockwell Collins Inc. (13499, 95105) | |
| 3040-00-010-9928 3040000109928 | S6135-20761-1 | Shaft, Straight | Material: Steel Overall Length: 1.800 inches nominal End Similarity: Identical | Sikorsky Aircraft Corporation (78286) | |
| 3040-00-010-9930 3040000109930 | S6135-20763-2 | Gearshaft, Spur | IGW Systems Inc. (93828) Triumph Gear Systems - Macomb Inc. (57152) BMT Aerospace USA Inc. (11371) | ||
| 3040-00-011-0112 3040000110112 | 12M2549-11 | Collar, Shaft | Bore Diameter: 0.8126 inches minimum and 0.8136 inches maximum Style Designator: Round stepped Material: Aluminum bronze | Lockheed Martin Corporation (81755) | |
| 3040-00-011-0113 3040000110113 | 532972-1 530982-1 | Gearshaft, Spur | Honeywell International Inc. (70210) | ||
| 3040-00-011-0154 3040000110154 | 12M2416-7 | Gearshaft, Spur | Lockheed Martin Corporation (81755) | ||
| 3040-00-011-0704 3040000110704 | 175R122P009 175R122P9 | Housing, Mechanical Drive | Special Features: Pto housing assy, includes housing and tubes, T.O. 2J-J85-54/FIG 12/IND 11;OD 1ST end 6.820/6.822;OD 2ND end 6.633/6.635;LGTH 5.470/5.485 in.;does not include cover plates for openinmgs End Item Identification: J85 eng | General Electric Company (99207) General Electric Co. (24446) | |
| 3040-00-011-0717 3040000110717 | 6-50732-503 6-50732-501 6-50732-505 | Connecting link, Rigid | Body Construction: Tubular | Northrop Grumman Technical Services (0JRC1) Northrop Grumman Systems Corporation (76823) | |
| 3040-00-011-0865 3040000110865 | 1087 | Gearshaft, Spur | Overton Chicago Gear Corporation (50582) | ||
| 3040-00-011-1056 3040000111056 | 8492290-1 | Shaft, Straight | Special Features: Passivated;not casehardened;chamfered at 45.0 deg angle Material: Steel Overall Length: 1.212 inches nominal | L-3 Communications Corporation (11447) Lockheed Martin Corp. (49671) | |
| 3040-00-011-1084 3040000111084 | 44A219460 8494560-501 | Gearshaft, Spur | Overall Length: 1.212 inches nominal Shaft Material: Steel Gear Material: Steel | Lockheed Martin Corp. (49671) Herley Chicago (98738) | |
| 3040-00-011-1128 3040000111128 | 3C01127-127 | Connecting link, Rigid | Body Construction: Tubular | Lockheed Martin Corporation (98897) | |
| 3040-00-011-1134 3040000111134 | 3C01127-133 | Connecting link, Rigid | Body Construction: Tubular | Lockheed Martin Corporation (98897) | |
| 3040-00-011-1176 3040000111176 | 3C00049-163 | Connecting link, Rigid | Body Construction: Tubular | Lockheed Martin Corporation (98897) | |
| 3040-00-011-1177 3040000111177 | 3C26118-101 | Cam, Control | Special Features: 5.340 in thk O/a 0.500 in W cam slot on 2.150 in mgt Material: Aluminum alloy 2014 | Lockheed Martin Corporation (98897) | |
| 3040-00-011-1202 3040000111202 | 3F31012-101 | Bell Crank | Special Features: Includes third arm End Item Identification: C-141 aircraft Style Designator: Clevis ends | Lockheed Martin Corporation (98897) Lockheed Martin Services Inc. (1WL60) |