Airframe Structural Components: 160D513200-2, 160D513201-3, 160D514000-1
MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
---|---|---|---|---|---|
160D513200-2 160D5132002 | 1560-01-494-0894 | Panel, Structural, Aircraft | Aircraft Mission Design Series: A10 Special Features: Fiberglass, 3 plies, 120 fabric per s-F 502; hexagonal core, type I Material: Glass fiber | Northrop Grumman Systems Corporation (26512) | |
160D513200-3 160D5132003 | 1560-01-492-7504 | Panel, Structural, Aircraft | Aircraft Mission Design Series: A-10 Special Features: C/O 1 skin, outer and 1 skin, inner; 2 core; items are fiberglass, 3 plies, 120 fabric per SF-502 and hexagonal cores, type I, 1/8 - 3.0(P-M601); dimensions are 13.00 X 10.00 X .60 and 6.50 X 6.00 X .60 Material: Glass fiber | Northrop Grumman Systems Corporation (26512) | |
160D513200-4 160D5132004 | 1560-01-494-0470 | Panel, Structural, Aircraft | Aircraft Mission Design Series: A10 Special Features: Fiberglass, 3 plies, 120 fabric per s-F 502; hexagonal core, type I Material: Glass fiber | Northrop Grumman Systems Corporation (26512) | |
160D513201-13 160D51320113 | 1560-01-568-8978 | Spar, Aircraft | III End Item Identification: A-10A acft Aircraft Mission Design Series: A-10A acft Special Features: Alcd sh; heat treat 0; used on 160D513201-1, -2, -3, -4; next assy 160D513000; dim. are stocksize matl. | Northrop Grumman Systems Corporation (26512) | |
160D513201-23 160D51320123 | 1560-01-554-9304 | Plate, Structural, Aircraft | III End Item Identification: A-10 Aircraft Mission Design Series: A-10A Special Features: Dim. are stock matl.; alcd sh/ used on -3 | Northrop Grumman Systems Corporation (26512) | |
160D513201-24 160D51320124 | 1560-01-554-9338 | Plate, Structural, Aircraft | III End Item Identification: A-10 Aircraft Mission Design Series: A-10A Special Features: Alcd SH-T6; dim. are stocksize matl; used on -4 | Northrop Grumman Systems Corporation (26512) | |
160D513201-25 160D51320125 | 1560-01-555-0487 | Plate, Structural, Aircraft | Aircraft Mission Design Series: A-10A thunderbolt ii Material: Aluminum alloy Aircraft Location: Trim tab elevator | Northrop Grumman Systems Corporation (26512) | |
160D513201-26 160D51320126 | 1560-01-553-7645 | Plate, Structural, Aircraft | Aircraft Mission Design Series: A-10 Special Features: Dim. are stock material Material: Aluminum alloy 7075 | Northrop Grumman Systems Corporation (26512) | |
160D513201-3 160D5132013 | 1560-01-034-9008 | Tab, Trim, Aircraft | Aircraft Mission Design Series: A-10 | Northrop Grumman Systems Corporation (26512) | |
160D513201-4 160D5132014 | 1560-01-027-6804 | Tab, Trim, Aircraft | Aircraft Mission Design Series: A-10 | Northrop Grumman Systems Corporation (26512) | |
160D513401-5 160D5134015 | 1560-01-391-8481 | Fitting, Structural Component, Air | III End Item Identification: A-10 thunderbolt aircraft Aircraft Mission Design Series: A-10A Special Features: Assembly C/O 2 NAS516-1 grease ftg, MS28913-5C bearing, fitting -25, made from -15 forging, -25ALTN for -21 | Capy Machine Shop Inc. (0BVP9) Miller Stuart Inc. (52977) Northrop Grumman Systems Corporation (26512,61174) | |
160D513402-17 160D51340217 | 1560-01-183-0100 | Support, Structural Component, Air | III End Item Identification: Acft model A-10 Special Features: Aluminum alloy per QQ-A-250/12 7075-T351, 1.900 in. lg, 1.600 in. W, 1.700IN. thk III Supplementary Features: Functional description:located fuselage station 464 | Northrop Grumman Systems Corporation (26512) | |
160D513402-21 160D51340221 | 1560-01-009-9299 | Support, Structural Component, Air | III End Item Identification: Model A10 aircraft Special Features: Aluminum alloy | Atec Manufacturing Corp. (63650) Inspirnetics Inc. (2X974) Northrop Grumman Systems Corporation (26512,61174) | |
160D513402-25 160D51340225 | 1560-01-127-4736 | Support, Structural Component, Air | III End Item Identification: Acft model A-10A Special Features: Aluminum alloy per QQ-A-250/12, 7075-T7351 | Northrop Grumman Systems Corporation (26512,61174) Triumph Fabrications-Hot Springs (3H339) | |
160D513402-27 160D51340227 | 1560-01-015-7291 | Support, Structural Component, Air | III End Item Identification: Aircraft model A10 Special Features: Aluminum alloy, QQ-A-250/12, alloy 7075, T7351, stock size, 3.000 in. lg, 2.500 in. W, 2.250 in. thk | B & B Precision Components Inc. (1N108) Inspirnetics Inc. (2X974) Miller Stuart Inc. (52977) Northrop Grumman Systems Corporation (26512,61174) | |
160D513402-31 160D51340231 | 1560-01-074-0465 | Fitting, Structural Component, Air | Aircraft Mission Design Series: A-10 Special Features: C/O:1 fitting (160D513402-25), 2 bushings (S5006-4-084), 1 bushing (S5006-4-130), 1 bushing (S5006-4-126) | Northrop Grumman Systems Corporation (26512) | |
160D513402-7 160D5134027 | 1560-01-004-4736 | Support, Structural Component, Air | III End Item Identification: Model A10 aircraft Special Features: Aluminum alloy, QQ-A-250/12 | B & B Precision Components Inc. (1N108) Capy Machine Shop Inc. (0BVP9) Inspirnetics Inc. (2X974) Miller Stuart Inc. (52977) Northrop Grumman Systems Corporation (26512,61174) | |
160D513403-11 160D51340311 | 1560-01-260-5373 | Support, Structural Component, Air | III End Item Identification: Acft model A-10 Special Features: Aluminum alloy per QQ-A-250/12 7075-T1351, 2.750 in. lg, 2.380 in. W, 1.500 in. thk III Supplementary Features: Functional description:used on fitting assembly-trim tab actuator, elevator | Duncan Models (6U345) Northrop Grumman Systems Corporation (26512,61174) | |
160D513404-9 160D5134049 | 1560-01-391-8485 | Fitting, Structural Component, Air | III End Item Identification: A-10A thunderbolt ii aircraft Aircraft Mission Design Series: A-10A Special Features: Fitting assy-support outer elev hinge & trim tab | Atec Manufacturing Corp. (63650) B & B Precision Components Inc. (1N108) Northrop Grumman Systems Corporation (26512,61174) | |
160D514000-1 160D5140001 | 1560-01-102-3813 | Stabilizer, Horizontal | Aircraft Mission Design Series: A-10A | Northrop Grumman Systems Corporation (26512) |