FSC 1680 Miscellaneous Aircraft Accessories and Components: 1680-01-366-4205, 1680-01-366-4206, 1680-01-367-0240
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 1680-01-366-4205 1680013664205 | 414G5213-1 | Cable Assembly, Control | The Boeing Company (77272) | ||
| 1680-01-366-4206 1680013664206 | 414G5212-1 | Cable Assembly, Control | The Boeing Company (77272) | ||
| 1680-01-366-4302 1680013664302 | 46-0966-11 | Actuator, Electro-Mechanical, Rota | III End Item Identification: Used on lynx helicopter landing and taxi light Special Features: Rotating mechanism subassy | Grimes Aerospace Company (72914) | |
| 1680-01-366-4342 1680013664342 | 80-0300-1G 80-300-1G | Panel, Control, Electrical-Electro | III End Item Identification: Used on lynx helicopter Special Features: Warning unit and master control panel | Grimes Aerospace Company (72914) | |
| 1680-01-366-4343 1680013664343 | 80-0300-5H | Panel, Control, Electrical-Electro | III End Item Identification: Used on lynx helicopter Special Features: Warning unit and master caution panel | Grimes Aerospace Company (72914) | |
| 1680-01-366-4982 1680013664982 | MBEU147444 366E100-5 | Survival kit, Aircraft Seat | End Item Identification: Aircraft model F-18/TF-18 Component Document Origin: Government Document Type: Federal specification | East/West Industries Inc. (30941) Naval Air Systems Command (30003) | |
| 1680-01-366-5280 1680013665280 | 990-00-228 | Cable Assembly, Control | Bergen Cable Technology LLC (70958) | ||
| 1680-01-366-5739 1680013665739 | DAA3233A026-013 | Panel, Control, Electrical-Electro | III End Item Identification: Pacer special Accessory Components and Quantity: Consists of mounting plate assys, cover assy, lightplate, knobs, connectors, potentiometers, and miscellaneoushardware | Northrop Grumman Systems Corporation (1W025, 76823) | |
| 1680-01-366-6282 1680013666282 | 8445-52-1 | Tube, Return | III End Item Identification: Aircraft, hercules C-130 General Characteristics Item Description: Used on drive screw assy | CEF Industries Inc. (00268) | |
| 1680-01-366-6671 1680013666671 | 8445-6 | Gearbox Assembly, Aircraft | III End Item Identification: C-130H aircraft Special Features: Output gear assembly | CEF Industries Inc. (00268) | |
| 1680-01-366-6672 1680013666672 | DAA3255A117-029 | Uplock Assembly, Door, Aircraft | III End Item Identification: Pacer special Aircraft Location: Right middle slave-nlg wheel door | Northrop Grumman Systems Corporation (1W025) | |
| 1680-01-366-6743 1680013666743 | DAA3233A006-027 DAA3233A006-033 | Panel, Control, Electrical-Electro | III End Item Identification: Pacer special III Fsc Application Data: Complete environmental control system Accessory Components and Quantity: Light plate, potentiometers, switches, knobs | Northrop Grumman Systems Corporation (1W025) | |
| 1680-01-366-6744 1680013666744 | DAA3233A006-031 | Panel, Control, Electrical-Electro | III End Item Identification: Pacer special Accessory Components and Quantity: Consists of mounting plate assy, cover assy, lightplate, potentiometer, switches, knobs, connectors, terminal studs and miscellaneous hardware | Northrop Grumman Systems Corporation (1W025) | |
| 1680-01-366-6745 1680013666745 | DAA3233A013-023 | Panel, Control, Electrical-Electro | III End Item Identification: Pacer special Accessory Components and Quantity: 3 mounting plate assemblies, 1 angle bracket, 7 switches, 1 cover assy, connectors, resistors and miscellaneous hardware | Northrop Grumman Systems Corporation (1W025) | |
| 1680-01-366-6746 1680013666746 | DAA3233A013-025 | Panel, Control, Electrical-Electro | III End Item Identification: Pacer special Accessory Components and Quantity: 3 mount plate assemblies, 1 angle bracket, 7 switches, 1 cover assy, connectors, resistors and miscellaneous hardware | Northrop Grumman Systems Corporation (1W025) | |
| 1680-01-366-6765 1680013666765 | DAA3255A123-011 | Bell Crank | III End Item Identification: Pacer special Special Features: Bb arm end hole dia opposite 0.6250 hole is 0.4370 in. Center to Center Distance between Fulcrum and arm End Hole/Slot/Ball: 3.410 inches nominal 1ST end | Northrop Grumman Systems Corporation (1W025) | |
| 1680-01-366-7305 1680013667305 | DAA3255D222-001 | Bell Crank | III End Item Identification: B-2 aircraft Material: Steel | Northrop Grumman Systems Corporation (1W025) | |
| 1680-01-366-8009 1680013668009 | 09-43088-2-1 | Grip Assembly, Controller, Aircraf | III End Item Identification: F14 acft | Dover Diversified DE Inc. (78062) Rockwell Collins Electromechanical (86831) | |
| 1680-01-366-8010 1680013668010 | 09-43088-2-3 | Grip Assembly, Controller, Aircraf | III End Item Identification: F14 acft | Dover Diversified DE Inc. (78062) Rockwell Collins Electromechanical (86831) | |
| 1680-01-367-0240 1680013670240 | DAA3255A123-012 | Bell Crank | III End Item Identification: Pacer special Special Features: Bb arm end hole dia opposite 0.6250 hole is 0.4370 in. Center to Center Distance between Fulcrum and arm End Hole/Slot/Ball: 3.410 inches nominal 1ST end | Northrop Grumman Systems Corporation (1W025) |