FSC 3040 Miscellaneous Power Transmission Equipment: 3040-00-009-9005, 3040-00-009-9721, 3040-00-010-0618
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3040-00-009-9005 3040000099005 | 5100143 | Shaft, Straight | Hamilton Sundstrand Corporation (99167) | ||
| 3040-00-009-9026 3040000099026 | 975550-1 | Shaft, Shouldered | Honeywell International Inc. (99193, 59364) | ||
| 3040-00-009-9041 3040000099041 | A51C31565-11 | Shaft, Shouldered | Material: Titanium alloy Overall Length: 5.750 inches nominal End Similarity: Not identical | Northrop Grumman Systems Corporation (26512, 61174) | |
| 3040-00-009-9045 3040000099045 | A51C33518-11 | Shaft, Shouldered | Special Features: 3/8-28 unjf 3A thd size Material: Steel corrosion resisting Overall Length: 13.822 inches nominal | Northrop Grumman Systems Corporation (26512, 61174) | |
| 3040-00-009-9046 3040000099046 | A51K56575-11 | Shaft, Inner Reset link | General Characteristics Item Description: Cres, ams 5643, 5.800 in. O/a lg, 0.812 in. od | Northrop Grumman Systems Corporation (61174, 26512) | |
| 3040-00-009-9047 3040000099047 | 801305-1 | Shaft, Shouldered | Special Features: 1/2-20 unf 3A thd size Material: Steel Overall Length: 4.918 inches nominal | Honeywell International Inc. (70210) | |
| 3040-00-009-9063 3040000099063 | 107C2604-8 | Bell Crank | Special Features: Flight safety critical Material: Aluminum alloy Material Document and Classification: QQ-A-367, comp 7075, T73 fed spec single material response | The Boeing Company (77272) | |
| 3040-00-009-9065 3040000099065 | 107C2606-8 | Bell Crank | Material: Aluminum alloy Bore Diameter: 0.7488 inches minimum and 0.7493 inches maximum Bore Length: 1.630 inches nominal | The Boeing Company (77272) | |
| 3040-00-009-9066 3040000099066 | 107C1109-15 | Bell Crank | Special Features: 90.0 deg bend angle; includes 8 bushings; two 0.500 in. dia drilled holes in fulcrum split hub Material: Aluminum alloy Material Document and Classification: QQ-A-367, comp 7075, T73 fed spec single material response | The Boeing Company (77272) | |
| 3040-00-009-9073 3040000099073 | 975588-1 | Shaft, Straight | Special Features: Arm welded to one end of shaft Material: Steel comp 17-4PH Overall Length: 7.3000 inches nominal | Honeywell International Inc. (99193, 59364) | |
| 3040-00-009-9084 3040000099084 | 107C2605-9 | Bell Crank | Material: Aluminum alloy Bore Diameter: 0.8738 inches minimum and 0.8743 inches maximum Bore Length: 1.735 inches nominal | The Boeing Company (77272) | |
| 3040-00-009-9146 3040000099146 | 123CM12209-511 | Cam, Control | Special Features: Alum alloy QQ-A-225/9;9.437 in. L;2.875 in. W;1.125 in. H End Item Identification: E-2C aircraft | Northrop Grumman Systems Corporation (26512) | |
| 3040-00-009-9347 3040000099347 | 14-40461-3 | Connecting link, Rigid | Special Features: Rockwell C 39.0 to 44.0 Material: Steel Overall Length: 5.417 inches nominal | Northrop Grumman Technical Services (0JRC1) Northrop Grumman Systems Corporation (76823) | |
| 3040-00-009-9721 3040000099721 | TC3-4-1IWSTR0KE 241-0142 00241-0142 | Cylinder Assembly, Actuating, line | Overall Width: 1.000 inches nominal Overall Height: 1.000 inches nominal Body Material: Steel | Mosier Fluid Power of Ohio Inc. (16799) Harsco Corp. (93568) | |
| 3040-00-009-9783 3040000099783 | 539898-1 | Shaft, Input Contro | General Characteristics Item Description: Steel, AMS5610 | Hamilton Sundstrand Corporation (73030) | |
| 3040-00-010-0199 3040000100199 | TIP01153-24MAR71 3050872-5 3050872 | Cylinder Assembly, Actuating, line | Body Material: Steel Design Characteristics: Double acting single cylinder FSC Application Data: Loader, scoop type | New Holland Construction (89926) Cecom LR Center (97403) | |
| 3040-00-010-0205 3040000100205 | 3050877 3050877-4 | Cylinder Assembly, Actuating, line | End Item Identification: 38050519359 Bore Diameter: 5.505 inches minimum Bore Diameter: 5.510 inches maximum | Allis-Chalmers Corp. (92392) New Holland Construction (89926) | |
| 3040-00-010-0302 3040000100302 | 2990000100302 5566876 | Shaft, Shouldered | Material: Steel Overall Length: 12.812 inches nominal End Similarity: Not identical | E.C.A Etablissement Central DES (SCY13) General Motors Corp. (70040, 24617) General Motors LLC (7X677) | |
| 3040-00-010-0352 3040000100352 | 1064114 | Collar, Shaft | Material: Aluminum alloy, QQ-A-225/8, alloy 6061, T6 | U S Army Aviation and Missile (18876) | |
| 3040-00-010-0618 3040000100618 | 1018-36 | Shaft, Straight | Special Features: Drilled hole on second end no. 0.190-32 unf 2B thd and a 0.282 in. radius half dia cut from ctr of hole thru end Material: Aluminum alloy 6061 Overall Length: 12.438 inches nominal | J and H Smith Mfg Co. Inc. (82241) |