Miscellaneous Aircraft Accessories and Components: A51F9003-149, A51F9004-33, A51G20582-11
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| A51F9003-149 A51F9003149 | 1680-00-364-5592 | Control Assembly, Push-Pull | Core Diameter: 0.125 inches nominal Effective Length: 8.500 inches nominal Core Construction: Wire rope | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F9003-151 A51F9003151 | 1680-00-343-0237 | Control Assembly, Push-Pull | Special Features: Overall length 232.000 Core Material: Steel corrosion resisting Travel Distance: 4.750 inches nominal | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F9003-152 A51F9003152 | 1680-01-008-7999 | Control Assembly, Brake | III End Item Identification: Aircraft model F14A General Characteristics Item Description: Cres, 0.250 IN.-28 thd size both ends | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F9003-153 A51F9003153 | 1680-00-159-7205 | Control Assembly, Push-Pull | Effective Length: 248.750 inches minimum and 249.250 inches maximum Core Material: Steel corrosion resisting Flexible Conduit Outside Diameter: 0.410 inches nominal | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F9003-157 A51F9003157 | 1680-00-159-6884 | Control Assembly, Push-Pull | Effective Length: 170.750 inches minimum and 171.250 inches maximum Core Material: Steel corrosion resisting Flexible Conduit Outside Diameter: 0.410 inches nominal | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F9003-159 A51F9003159 | 1680-00-157-3897 | Control Assembly, Push-Pull | Special Features: Source control drawing number A51F9003 Core Diameter: 0.250 inches nominal Core Processed End Connection Type: Adjustable threaded adapter and nonadjustable connector | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F9003-161 A51F9003161 | 1680-00-357-1112 | Control Assembly, Push-Pull | Special Features: Overall length 111.810 in. Core Diameter: 0.125 inches nominal Core Construction: Wire rope | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F9003-165 A51F9003165 | 1680-01-008-7999 | Control Assembly, Brake | III End Item Identification: Aircraft model F14A General Characteristics Item Description: Cres, 0.250 IN.-28 thd size both ends | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F9003-196 A51F9003196 | 1680-01-343-1644 | Control Assembly, Push-Pull | III End Item Identification: A-6E acft Special Features: Minimum stroke 2.000 in.; overall length: 56.000 in. nominal | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F9004-27 A51F900427 | 1680-01-141-3500 | Control Assembly, Quadrant | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51F9004-29 A51F900429 | 1680-01-136-7827 | Control Assembly, Quadrant | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51F9004-31 A51F900431 | 1680-01-141-3499 | Control Assembly, Quadrant | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51F9004-33 A51F900433 | 1680-01-478-9880 | Control Assembly, Quadrant | Aircraft Mission Design Series: F14 Part Name Assigned By Controlling Agency: Quadrant assembly, throttle control | Northrop Grumman Systems Corporation (26512) | |
| A51FM1307 | 1680-01-504-6447 | Support Block | Northrop Grumman Field Support (9G864) | ||
| A51FM1307 | 1680-01-504-6448 | Support Block | Northrop Grumman Field Support (9G864) | ||
| A51FM1307-11 A51FM130711 | 1680-01-504-6447 | Support Block | Northrop Grumman Field Support (9G864) Northrop Grumman Systems Corporation (61174) | ||
| A51FM1307-13 A51FM130713 | 1680-01-504-6448 | Support Block | Northrop Grumman Field Support (9G864) Northrop Grumman Systems Corporation (61174) | ||
| A51G10542-1 A51G105421 | 1680-00-482-8816 | Link Assembly | General Characteristics Item Description: 2.892 in. O/a lg, 3.206 in. O/a W, 1.138 in. O/a thk, material aluminum | Northrop Grumman Systems Corporation (26512,61174) | |
| A51G10576-2 A51G105762 | 1680-00-498-4115 | Bell Crank | Material: Titanium Bore Diameter: 0.750 inches minimum and 0.751 inches maximum Bore Length: 0.875 inches nominal | Capy Machine Shop Inc. (0BVP9) G A Richards & Co. Inc. (65789) Northrop Grumman Systems Corporation (26512,61174) | |
| A51G10576-3 A51G105763 | 1680-00-123-6736 | Bell Crank | Material: Titanium alloy Bore Diameter: 0.750 inches minimum and 0.751 inches maximum Bore Length: 0.750 inches nominal | Cypress Semiconductor Corporation (65786) Northrop Grumman Systems Corporation (26512,61174) | |
| A51G20582-11 A51G2058211 | 1680-00-397-4301 | Lever, Remote Control | III End Item Identification: Lower inboard door, aircraft Special Features: Offset height: 0.200 in. nominal; surface treatment: cadmium per MIL-C-8837, type 2, class 1 and polyurethane coating over epoxy primer Material: Steel | Northrop Grumman Systems Corporation (26512,61174) |