Miscellaneous Aircraft Accessories and Components: 160D120310-5, 160D121200-3, 160D123100
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 160D120310-5 160D1203105 | 1680-01-010-2818 | Bell Crank | Material: Aluminum alloy Fsc Application Data: Cable, control, fuselage aircraft | Northrop Grumman Systems Corporation (26512) | |
| 160D120310-7 160D1203107 | 1680-01-010-2818 | Bell Crank | Material: Aluminum alloy Fsc Application Data: Cable, control, fuselage aircraft | Capy Machine Shop Inc. (0BVP9) Design/OL Inc. (0R2T5) Miller Stuart Inc. (52977) Northrop Grumman Systems Corporation (26512,61174) Unisys Corp. (6U975) | |
| 160D1204-3 160D12043 | 1680-00-361-4445 | Handle Assembly | III End Item Identification: Acft, model C-5A | B E Aerospace Inc. (86735) | |
| 160D121200 | 1680-01-494-0261 | Linkage Assembly | III End Item Identification: Nha - linkage assy-pitch control;e/I A-10 | Northrop Grumman Systems Corporation (26512) | |
| 160D121200 | 1680-01-494-0265 | Linkage Assembly | III End Item Identification: Nha - linkage assy-pitch control;e/I - A-10 | Northrop Grumman Systems Corporation (26512) | |
| 160D121200-1 160D1212001 | 1680-01-494-0265 | Linkage Assembly | III End Item Identification: Nha - linkage assy-pitch control;e/I - A-10 | Northrop Grumman Systems Corporation (26512,61174) | |
| 160D121200-3 160D1212003 | 1680-01-494-0261 | Linkage Assembly | III End Item Identification: Nha - linkage assy-pitch control;e/I A-10 | Northrop Grumman Systems Corporation (26512,61174) | |
| 160D121210-1 160D1212101 | 1680-01-010-2819 | Bell Crank | Material: Aluminum alloy Fsc Application Data: Control, pitch, fuselage aircraft | Northrop Grumman Systems Corporation (26512,61174) | |
| 160D121225-1 160D1212251 | 1680-01-010-2825 | Bell Crank | Material: Aluminum alloy Bore Diameter: 0.873 inches minimum and 0.874 inches maximum Bore Length: 0.813 inches minimum and 0.823 inches maximum | Northrop Grumman Systems Corporation (26512) | |
| 160D121225-3 160D1212253 | 1680-01-010-2825 | Bell Crank | Material: Aluminum alloy Bore Diameter: 0.873 inches minimum and 0.874 inches maximum Bore Length: 0.813 inches minimum and 0.823 inches maximum | Northrop Grumman Systems Corporation (26512) | |
| 160D121230-1 160D1212301 | 1680-01-004-0715 | Bell Crank | Material: Aluminum alloy Fsc Application Data: Roll control, fuselage aircraft | Capy Machine Shop Inc. (0BVP9) Design/OL Inc. (0R2T5) Miller Stuart Inc. (52977) Northrop Grumman Systems Corporation (26512,61174) | |
| 160D121235-1 160D1212351 | 1680-01-013-8799 | Bell Crank | Material: Aluminum alloy Fsc Application Data: Pitch control, fuselage aircraft | Capy Machine Shop Inc. (0BVP9) Design/OL Inc. (0R2T5) Northrop Grumman Systems Corporation (26512,61174) | |
| 160D121250-1 160D1212501 | 1680-01-004-1591 | Bell Crank | Material: Aluminum alloy Bore Diameter: 0.875 inches nominal Bore Length: 2.218 inches nominal | Aerometals Inc. (32664) Bruder Industry (32776) Capy Machine Shop Inc. (0BVP9) CPI Aerostructures Inc. (9U679) Design/OL Inc. (0R2T5) Miller Stuart Inc. (52977) Northrop Grumman Systems Corporation (26512,61174) Northwest Machining & Mfg. Inc. (9J448) Tens Machine Company Inc. (8P689) Thomas Instrument & Machine Co. Inc. (5H860) | |
| 160D121250-3 160D1212503 | 1680-01-004-1591 | Bell Crank | Material: Aluminum alloy Bore Diameter: 0.875 inches nominal Bore Length: 2.218 inches nominal | Northrop Grumman Systems Corporation (26512) | |
| 160D121260-1 160D1212601 | 1680-01-171-2072 | Crank Assembly, Pitch Control | III End Item Identification: A-10A aircraft General Characteristics Item Description: Consists of MIL-S-81733 sealant, as REQUIRED;1 160D920112-11 PLUG;1 S5000-3-105 BUSHING;1 S5005-4-180 BUSHING;2 MS21042L3 NUTS;2 AN975-3 WASHERS;2 AN386-2-15A PINS;1 160D121265-11 CRANK;1 160D121262-11 crank III Fsc Application Data: Aircraft accessory equipment | Aerometals Inc. (32664) Capy Machine Shop Inc. (0BVP9) Design/OL Inc. (0R2T5) Miller Stuart Inc. (52977) Northrop Grumman Systems Corporation (26512,61174) | |
| 160D122130-1 160D1221301 | 1680-01-256-4315 | Crank Assembly, Roll | III End Item Identification: A10 aircraft | Capy Machine Shop Inc. (0BVP9) Design/OL Inc. (0R2T5) Miller Stuart Inc. (52977) Northrop Grumman Systems Corporation (26512,61174) | |
| 160D122130-3 160D1221303 | 1680-01-011-8782 | Crank Assembly, Roll Control | III End Item Identification: Aircraft model A10 General Characteristics Item Description: Aluminum alloy, QQ-A-200/11, alloy 7075, T73511, stock size, 7.600 in. lg, 6.800 in. W, 3.500 in. thk | Northrop Grumman Systems Corporation (26512) | |
| 160D123056-1 160D1230561 | 1680-01-094-2344 | Torque Shaft | III End Item Identification: A-10A aircraft | Capy Machine Shop Inc. (0BVP9) Northrop Grumman Systems Corporation (26512,61174) | |
| 160D123063-11 160D12306311 | 1680-01-009-3356 | Lever, Remote Control | III End Item Identification: Acft accessories and components Special Features: 125 aa microinch surface treatment Material: Steel | Northrop Grumman Systems Corporation (26512) | |
| 160D123070-1 160D1230701 | 1680-01-004-0480 | Control Assembly Rudder | III End Item Identification: Model A10 aircraft | Northrop Grumman Systems Corporation (26512) | |
| 160D123100 | 1680-01-494-0204 | Bell Crank | III End Item Identification: Nha - control assembly-differential brake and rudder pedal; E/I - A-10 | Northrop Grumman Systems Corporation (26512) | |
| 160D123100 | 1680-01-494-0239 | Bell Crank | III End Item Identification: Nha - control assembly-differential brake and rudder pedal; E/I - A-10 | Northrop Grumman Systems Corporation (26512) |