Miscellaneous Aircraft Accessories and Components: A51F10065-5, A51F10107-3, A51F23608-25
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| A51F10065-5 A51F100655 | 1680-01-104-9385 | Shield Assembly | III End Item Identification: Aircraft model F-14 | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F10065-7 A51F100657 | 1680-01-104-9386 | Shield Assembly | III End Item Identification: Aircraft model F-14 | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F10065-9 A51F100659 | 1680-01-236-5131 | Shield Assembly | General Characteristics Item Description: Includes lever; stiffener; vinyl cloth; tape; nylon thread | Airborne Industries Inc. (66860) D F P Manufacturing Corp. (9J659) Northrop Grumman Systems Corporation (26512,61174) | |
| A51F10091-27 A51F1009127 | 1680-01-447-6173 | Glareshield, Aircraft | III End Item Identification: F-14A aircraft Material: Plastic polycarbonate Aircraft Mission Design Series: F-14A | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F10091-41 A51F1009141 | 1680-01-447-6173 | Glareshield, Aircraft | III End Item Identification: F-14A aircraft Material: Plastic polycarbonate Aircraft Mission Design Series: F-14A | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F10107-3 A51F101073 | 1680-01-009-2333 | Panel, Computer | III Fsc Application Data: Equipment installation, cockpit, aircraft | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F10614-3 A51F106143 | 1680-00-434-0231 | Lever, Remote Control | Material: Aluminum alloy Material Document and Classification: QQ-A-225/9, alloy 7075, T7351 fed spec single material response Surface Treatment: Anodize | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F11082-3 A51F110823 | 1680-01-361-9971 | Panel, Indicator | III End Item Identification: F-14 tomcat fighter airplane Indicator Type: Light | East/West Industries Inc. (30941) Northrop Grumman Systems Corporation (26512,61174) | |
| A51F11508-1 A51F115081 | 1680-00-334-8803 | Crank Assembly | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: Aluminum alloy, QQ-A-225/9, comp 7075, temper T7351 | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F11509-3 A51F115093 | 1680-00-434-0228 | Bell Crank | Material: Aluminum alloy Bore Diameter: 0.873 inches minimum and 0.874 inches maximum Bore Length: 0.790 inches nominal | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F11512-11 A51F1151211 | 1680-00-334-8802 | Fitting, Flap Control | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: Aluminum alloy, QQ-A-225/9, comp 7075, temper T7351, 7.606IN. O/a lg, 3.339 in.O/a W | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F12060-11 A51F1206011 | 1680-00-321-1269 | Control, Landing Gear | III End Item Identification: Aircraft model F-14A | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F12104-3 A51F121043 | 1680-00-505-1311 | Cover Assembly, Canopy Control Pi | III End Item Identification: Aircraft model F14A General Characteristics Item Description: Aluminum alloy, QQ-A-250/12, composition 7075, TEMPER-T6, 0.063 in. nom thk | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F12212-1 A51F122121 | 1680-00-323-0744 | Knob Assembly, Control | III End Item Identification: Acft model F-14A General Characteristics Item Description: 1.500 in. od | Abelconn LLC (66886) Northrop Grumman Systems Corporation (26512,61174) | |
| A51F12525-11 A51F1252511 | 1680-00-406-4591 | Lever, Remote Control | III End Item Identification: Pump, cockpit, aircraft Material: Aluminum alloy Bore Diameter: 0.876 inches minimum and 0.881 inches maximum | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F12603-13 A51F1260313 | 1680-01-239-5289 | Yoke, Arresting Hook | General Characteristics Item Description: Aluminum alloy, A357-T61, overall; primer, epoxy polyamide overall, coating, linear polyurethane, dark gray on shank; 0.127 in. min and 0.133 in. max dia 2 holes; 0.217 in. min and 0.223 in. max hole dia 2 places; 0.385 in. min and 0.392 in. max hole dia, one place; 0.249 in. min and 0.255 in. max hole dia 2 places; right hand side | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F12606-1 A51F126061 | 1680-00-406-1167 | Handle Assembly | General Characteristics Item Description: 2.812 in. O/a lg, 0.625 in. O/a dia, material aluminum | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F13007-49 A51F1300749 | 1680-01-249-1067 | Panel, Shelf | General Characteristics Item Description: Consists of eleven panel spacers P/N GS500E08D47-5; four panel spacers P/N GS500E3D47-5; two skins P/N A51F13007-11; one core P/N A51F13007-15; compound; adhesive; primer | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F20206-11 A51F2020611 | 1680-01-008-4058 | Cover, Computer Air Data Single P | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: Plastic /abs/, GM4003-3-3-2, fscm 26512, 0.047 in. nom thk | Northrop Grumman Systems Corporation (26512,61174) | |
| A51F23608-25 A51F2360825 | 1680-01-284-0190 | Lever, Engine Shut off | III End Item Identification: Aircraft model F-14A | Northrop Grumman Systems Corporation (26512,61174) |