Miscellaneous Aircraft Accessories and Components: A51C12056-1, A51C13505-27, A51C31501-5
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
A51C12056-1 A51C120561 | 1680-00-239-6589 | Bell Crank, Assy | Northrop Grumman Systems Corporation (26512,61174) | ||
A51C13053-1 A51C130531 | 1680-00-406-1190 | Crank Assy | Northrop Grumman Systems Corporation (26512,61174) | ||
A51C13053-3 A51C130533 | 1680-00-406-1190 | Crank Assy | Northrop Grumman Systems Corporation (61174) | ||
A51C13504-13 A51C1350413 | 1680-00-404-0180 | Axle, Rudder Pedal | General Characteristics Item Description: Steel, MIL-S-8844 cl 1, cadmium plated, 3.083 in. lg, irregularshape, 3/8-24 unjf 3A thd, 0.533 in. lg one end | Northrop Grumman Systems Corporation (26512,61174) | |
A51C13505-21 A51C1350521 | 1680-01-033-0285 | Pedal, Control | Width: 4.340 inches nominal Length: 6.860 inches nominal Mounting Method: Hinge | Northrop Grumman Systems Corporation (26512) | |
A51C13505-23 A51C1350523 | 1680-01-033-0285 | Pedal, Control | Width: 4.340 inches nominal Length: 6.860 inches nominal Mounting Method: Hinge | Acrometal Products Inc. (9F796) Danko Arlington Inc. (26993) Northrop Grumman Systems Corporation (26512,61174) | |
A51C13505-25 A51C1350525 | 1680-01-031-4000 | Pedal, Control | Width: 4.340 inches nominal Length: 6.860 inches nominal Mounting Method: Hinge | Danko Arlington Inc. (26993) Northrop Grumman Systems Corporation (26512,61174) Progress Casting Group, Inc. (50705) | |
A51C13505-27 A51C1350527 | 1680-01-361-5205 | Pedal, Control | III End Item Identification: F-14A Mounting Method: Socket Mounting Position: In line W/mounting center | Northrop Grumman Systems Corporation (26512,61174) | |
A51C13513-1 A51C135131 | 1680-00-406-1184 | Crank Assembly | General Characteristics Item Description: Aluminum alloy, anodized, 4.585 in. O/a lg, 3.806 in. O/a H, 1.510IN. O/a W | Northrop Grumman Systems Corporation (26512,61174) | |
A51C13515-1 A51C135151 | 1680-00-406-1186 | Crank Assembly | General Characteristics Item Description: 4.390 in. O/a lg, 1.822 in. O/a W, 2.310 in. O/a H, materialaluminum, finish anodize | Northrop Grumman Systems Corporation (26512,61174) | |
A51C13517-1 A51C135171 | 1680-00-406-1189 | Crank Assembly | General Characteristics Item Description: Aluminum alloy, MIL-A-22771 7075T73 | Northrop Grumman Systems Corporation (26512,61174) | |
A51C13912-13 A51C1391213 | 1680-00-529-8265 | Handle, Pedal Adjustable | General Characteristics Item Description: 2.625 in. lg, 0.562 in. od | Northrop Grumman Systems Corporation (26512,61174) | |
A51C22057-7 A51C220577 | 1680-01-079-8685 | Bobweight Assembly | III End Item Identification: Aircraft model F-14A | Capy Machine Shop Inc. (0BVP9) Northrop Grumman Systems Corporation (26512,61174) | |
A51C3106-1 A51C31061 | 1680-00-148-8709 | Cylinder Assembly, Reaction | Northrop Grumman Systems Corporation (26512,61174) | ||
A51C31068-11 A51C3106811 | 1680-00-229-0914 | Bell Crank Cluster | Northrop Grumman Systems Corporation (26512,61174) | ||
A51C31069-1 A51C310691 | 1680-00-148-8709 | Cylinder Assembly, Reaction | Northrop Grumman Systems Corporation (26512) | ||
A51C31071-1 A51C310711 | 1680-00-003-6397 | Adjuster, Flight Co | General Characteristics Item Description: 3.000 in. lg, 0.770 in. W | Northrop Grumman Systems Corporation (26512,61174) | |
A51C31084-1 A51C310841 | 1680-01-016-3128 | Crank Assembly, Trim System | III End Item Identification: F-14A aircraft | Northrop Grumman Systems Corporation (26512,61174) | |
A51C31501-3 A51C315013 | 1680-00-004-2901 | Crank Assembly | General Characteristics Item Description: Irregular shaped, 2.343 in. approx O/a W, used on F-14A acft | Northrop Grumman Systems Corporation (26512,61174) | |
A51C31501-5 A51C315015 | 1680-01-009-2403 | Crank Assembly, Output-Longitudin | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: Aluminum alloy, MIL-A-22771, comp 7075, TEMPER-T73 | Northrop Grumman Systems Corporation (26512,61174) |