Airframe Structural Components: 160D521128-3, 160D521131-4, 160D610103
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 160D521128-3 160D5211283 | 1560-01-029-7314 | Coupling Assembly, Elevator | III End Item Identification: Acft model A-10A | Aero Components Inc. (59213) Capy Machine Shop Inc. (0BVP9) Miller Stuart Inc. (52977) Northrop Grumman Systems Corporation (26512,61174) | |
| 160D521131-1 160D5211311 | 1560-01-011-8820 | Support, Structural Component, Air | Aircraft Mission Design Series: A10 Side FOR Which Designed: Left side | Northrop Grumman Systems Corporation (26512) | |
| 160D521131-2 160D5211312 | 1560-01-015-0806 | Support, Structural Component, Air | Aircraft Mission Design Series: A-10 Side FOR Which Designed: Right side | Northrop Grumman Systems Corporation (26512) | |
| 160D521131-3 160D5211313 | 1560-01-011-8820 | Support, Structural Component, Air | Aircraft Mission Design Series: A10 Side FOR Which Designed: Left side | Northrop Grumman Systems Corporation (26512) | |
| 160D521131-4 160D5211314 | 1560-01-015-0806 | Support, Structural Component, Air | Aircraft Mission Design Series: A-10 Side FOR Which Designed: Right side | Northrop Grumman Systems Corporation (26512) | |
| 160D52117-13 160D5211713 | 1560-01-021-0393 | Bell Crank | Bore Diameter: 0.625 inches minimum and 0.630 inches maximum Bore Length: 2.080 inches nominal Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 3.625 inches nominal 1ST end | Northrop Grumman Systems Corporation (26512) | |
| 160D523105-1 160D5231051 | 1560-01-108-1325 | Crank Assembly, Horizontal | III End Item Identification: Aircraft model A-10 General Characteristics Item Description: Consists of 1 160D523110-1 crank assembly, 1 160D920104-19 cable assembly, 1 HS15-8 collar, 1 AS62-8-9 pin and AN960C416L washer | Air Craftors Engineering Inc. (7N480) Capy Machine Shop Inc. (0BVP9) Northrop Grumman Systems Corporation (26512,61174) | |
| 160D523110-1 160D5231101 | 1560-01-004-4610 | Crank Assembly, cable, Yaw Control | III End Item Identification: Model A10 aircraft | Capy Machine Shop Inc. (0BVP9) Design/OL Inc. (0R2T5) Miller Stuart Inc. (52977) Northrop Grumman Systems Corporation (26512,61174) | |
| 160D523110-3 160D5231103 | 1560-01-004-4610 | Crank Assembly, cable, Yaw Control | III End Item Identification: Model A10 aircraft | Northrop Grumman Systems Corporation (26512) | |
| 160D523131-3 160D5231313 | 1560-01-077-8105 | Support, Structural Component, Air | Aircraft Mission Design Series: A-10A Special Features: C/O 1 support, 1 pad, misc hardwr Aircraft Location: Yan control | Thompson Aerospace Inc. (11809) | |
| 160D523131-4 160D5231314 | 1560-01-079-4106 | Support, Structural Component, Air | Aircraft Mission Design Series: A-10A Special Features: C/O 1 support, 1 pad, misc hardw | Northrop Grumman Systems Corporation (26512) | |
| 160D523210-2 160D5232102 | 1560-01-114-7181 | Support Assembly, Rudder | III End Item Identification: Aircraft A-10 General Characteristics Item Description: Located at rudder actuator BL113 | Northrop Grumman Systems Corporation (26512,61174) | |
| 160D610001-101 160D610001101 | 1560-01-492-6056 | Wing Assembly, Aircraft | Aircraft Mission Design Series: A-10A Special Features: C/O spars, ribs, skin, supports, panels, sections, fastening devices, misc. hardware; fairings Material: Aluminum alloy | Northrop Grumman Systems Corporation (26512) | |
| 160D610001-19 160D61000119 | 1560-01-533-2793 | Wing Assembly, Aircraft | Northrop Grumman Systems Corporation (26512) | ||
| 160D610001-23 160D61000123 | 1560-01-484-1782 | Wing Section, Center | Aircraft Mission Design Series: A-10 airc. Special Features: C/O support assy; fairing instl.;splice fairing instl.; foam instl.; eqpt & harn.instl.; te instl.; le instl.;rib instl.; rear spar instl.; ctr. spar instl.;front spar instl.; lwr. skinaft.; lwr skin fwd; wing splice instl.; flap track instl.; pylon ftg. instl.; misc. hardware; same as 160J611011-5, except all new parts used; manufacturer suggested name is wing, assy Material: Aluminum alloy | Northrop Grumman Systems Corporation (26512) | |
| 160D610001-93 160D61000193 | 1560-01-532-5617 | Wing Assembly, Aircraft | Part Name Assigned BY Controlling Agency: WING Aircraft Location: Wing assembly Aircraft Mission Design Series: A-10A thunderbolt ii | Northrop Grumman Systems Corporation (26512) | |
| 160D610001-95 160D61000195 | 1560-01-492-6057 | Wing Assembly, Aircraft | Aircraft Mission Design Series: A-10A Special Features: U/O center or sides; C/O sections, panels, spars, ribs, skin, supports, fairings, fastening devices, misc. har dware Material: Aluminum alloy | Northrop Grumman Systems Corporation (26512) | |
| 160D610001-97 160D61000197 | 1560-01-492-6054 | Wing Assembly, Aircraft | Aircraft Mission Design Series: A-10A Special Features: Maybe used center or right/left sides;c/O spars, panels, ribs, skins, supports, fairings, fastening devises, misc. hardware Material: Aluminum alloy | Northrop Grumman Systems Corporation (26512) | |
| 160D610001-99 160D61000199 | 1560-01-492-6055 | Wing Assembly, Aircraft | Aircraft Mission Design Series: A-10A Special Features: C/O sections, spars, ribs, skin, supports, panels, components, fastening devices, misc. hardware Material: Aluminum alloy | Northrop Grumman Systems Corporation (26512) | |
| 160D610103 | 1560-01-505-2116 | Support, Structural Component, Air | Aircraft Mission Design Series: A-10 Special Features: Dims are stock material; -37 opp -38; U/O F-16 Material: Aluminum alloy 7075 | Northrop Grumman Systems Corporation (26512) |