FSC 3040 Miscellaneous Power Transmission Equipment: 3040-00-022-0008, 3040-00-022-1625, 3040-00-023-1642
NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
3040-00-022-0008 3040000220008 | 439685 572367 | Bell Crank | Special Features: Fulcrum shaft 0.490 in. dia, 1.240 in. lg; fulcrum 462801 M/F forging 410674-F Material: Steel corrosion resisting End Item Identification: TF33 aircraft engine | BMT Aerospace USA Inc. (11371) United Technologies Corporation (77445) Electro-Methods Inc. (33617) | |
3040-00-022-0022 3040000220022 | 0N020317 | Bell Crank | Material: Steel corrosion resisting Bore Diameter: 0.128 inches nominal Surface Treatment: Passivate | National Security Agency (98230) | |
3040-00-022-0024 3040000220024 | 110299 | Shaft, Pointer, au, Il | General Dynamics Canada LTD (05257) | ||
3040-00-022-1625 3040000221625 | 10239 | Shaft, Straight | Material: Steel Overall Length: 6.062 inches nominal First End Diameter: 1.5000 inches nominal | Stanadyne Corporation (84760) | |
3040-00-022-2559 3040000222559 | 4505260 | Shaft, Straight | Special Features: Drilled for oil passage | Agco Corp. (6N299) | |
3040-00-022-2629 3040000222629 | 10075 | Shaft, cam Roller | Reference Number Differentiating Characteristics: As differentiated by no special cleaning required | Cryogenic Equipment Inc. (16760) | |
3040-00-022-3038 3040000223038 | 104643 | Gearshaft, Spur | Astronautics Corporation of America (10138) | ||
3040-00-022-5329 3040000225329 | 609042 | Shaft, Shouldered | Material: Steel comp 4620 Overall Length: 1.988 inches nominal End Similarity: Not identical | Eaton Aerospace LLC (62983) | |
3040-00-022-6937 3040000226937 | 10124698 | Gearshaft, Spur | U S Army Aviation and Missile (18876) | ||
3040-00-022-7111 3040000227111 | S429F9713 S429F SG-3598 SG-3598 PIECE 11 S429F0713 | Plate, Retaining, Shaft | Special Features: Jp;es equally spaced on 4.875 in. dia bolt circle; mtg holes counterbored on one side opposite face, 0.875 in. dia by 0.312 in. deep Material: Copper alloy Thickness: 0.562 inches nominal | Siemens Demag Delaval Turbomachinery (16712) IMO Industries Inc. (59180) | |
3040-00-022-7158 3040000227158 | PY43-1 2220605 | Shaft Assembly, Flexible | Screw Thread Series Designator: Un both ends End Connection Type: Threaded internal both ends Casing Material: Rubber, chloroprene | Navair and Navsea Managed (10001) S.S. White Technologies Inc. (0KZS2) Pennwalt Corp. (97945) | |
3040-00-022-7838 3040000227838 | 2480777 | Shaft, Output Bearing | End Item Identification: Common jet engine General Characteristics Item Description: Heat treat 34-40 rc per MIL-H-6875 | Parker Hannifin Corporation (92003) Goodrich Corporation (99551) | |
3040-00-022-8524 3040000228524 | 871519 | Collar, Shaft | Bore Diameter: 0.1875 inches nominal Style Designator: Plain round Material: Aluminum alloy, QQ-A-225/6, alloy 2024, T4 | Lockheed Martin Corporation (56232) | |
3040-00-022-9033 3040000229033 | 115902-2 | Cam, Control | Raytheon Company (37695) | ||
3040-00-022-9049 3040000229049 | 435797 | Gearshaft, Drive, Oil | United Technologies Corporation (77445) | ||
3040-00-022-9601 3040000229601 | 594327 | Connecting link, Rigid | United Technologies Corporation (77445) | ||
3040-00-022-9706 3040000229706 | 658675-2 658675-0002 | Shaft, Shouldered | Special Features: 1ST end chamfer 0.03 by 45 deg, 2ND end 0.01 by 45.0 Material: Steel Overall Length: 2.9063 inches nominal | Northrop Grumman Guidance And (06481) | |
3040-00-022-9709 3040000229709 | 658675-1 658675-0001 | Shaft, Shouldered | Special Features: 1ST end chamfer 0.03 by 45 deg, 2ND end 0.01 by 45.0 Material: Steel Overall Length: 3.469 inches nominal | Northrop Grumman Guidance And (06481) | |
3040-00-022-9938 3040000229938 | 42102D14 | Gearshaft, Spur | Triumph Gear Systems Inc. (82402) | ||
3040-00-023-1642 3040000231642 | 464041PC2T04 8-4041-2 464041PCS2T04 | Shoe, Thrust Bearing | Siemens Demag Delaval Turbomachinery (16712) Kingsbury Inc. (75333) |