Structural Shapes: 687337-9, 7021-124 ITEM 7, 7150183
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 687337-9 6873379 | 9520-01-011-9291 | Channel, Structural | Material: Aluminum alloy, QQ-A-200/9 Fabrication Method: Extruded Heat Treatment: F-as fabricated | Crsi Inc. Delaware (19564) | |
| 69-23639-1 69236391 | 9520-01-249-9987 | Channel, Structural | The Boeing Company (17765,81205) | ||
| 69-70246 6970246 | 9520-01-581-2356 | Angle, Structural | The Boeing Company (81205) | ||
| 69-70246 6970246 | 9520-01-581-2362 | Angle, Structural | The Boeing Company (81205) | ||
| 69-70246-603 6970246603 | 9520-01-581-2362 | Angle, Structural | The Boeing Company (81205) | ||
| 69-70246-604 6970246604 | 9520-01-581-2356 | Angle, Structural | The Boeing Company (81205) | ||
| 69-70246-607 6970246607 | 9520-01-581-0121 | Bracket, Structural Component, Air | END Item Identification: C-135 aircraft Part Name Assigned BY Controlling Agency: Angle assy-T.E.fairing expansion joint | The Boeing Company (81205) | |
| 70084-23105-135 7008423105135 | 9520-01-576-2030 | Channel, Structural | Sikorsky Aircraft Corporation (78286) | ||
| 70201-22101-117 7020122101117 | 9520-01-562-3816 | Angle, Structural | Material: Aluminum alloy, QQ-A-250/11 Special Features: Used on the upper fuselage frame | Sikorsky Aircraft Corporation (78286) | |
| 70207-22200-102 7020722200102 | 9520-01-340-4276 | Angle, Structural | End Item Identification: Seahawk helicopter S70B-2 | Sikorsky Aircraft Corporation (78286) | |
| 70207-22200-127 7020722200127 | 9520-01-340-4276 | Angle, Structural | End Item Identification: Seahawk helicopter S70B-2 | Sikorsky Aircraft Corporation (78286) | |
| 70207-26001-111 7020726001111 | 9520-01-505-9388 | Channel, Structural | Sikorsky Aircraft Corporation (78286) | ||
| 70207-26001-112 7020726001112 | 9520-01-505-9374 | Channel, Structural | Sikorsky Aircraft Corporation (78286) | ||
| 7021-124 ITEM 7 7021124ITEM7 | 9520-01-266-2796 | Beam, Structural | Naval Sea Systems Command (53711) | ||
| 70219-04200-170 7021904200170 | 9520-01-505-9380 | Channel, Structural | Sikorsky Aircraft Corporation (78286) | ||
| 7030996-1 70309961 | 9520-01-494-3428 | Molding, Metal | Material: Steel, corrosion resisting Fabrication Method: Extruded Length: 34.120 inches nominal | Gichner Systems Group Inc. (29381) | |
| 7040260-501 7040260501 | 9520-01-562-3319 | Molding, Metal | End Item Identification: Tactical air control systems 407L | Gichner Systems Group Inc. (29381) | |
| 7092451 | 9520-01-175-7235 | Channel, Structural | Material: Aluminum alloy Fabrication Method: Extruded Length: 1.677 feet nominal | U S Army Tank Automotive Command (19207) | |
| 7092454 | 9520-01-175-7235 | Channel, Structural | Material: Aluminum alloy Fabrication Method: Extruded Length: 1.677 feet nominal | U S Army Tank Automotive Command (19207) | |
| 709-5770322-16 709577032216 | 9520-00-954-5666 | Angle, Structural | Material: Steel, astm A36 Fabrication Method: Extruded Length: 30.000 feet minimum and 40.000 feet maximum | Electric Boat Corporation (96169) | |
| 7150183 | 9520-01-246-0670 | Angle, Structural | Northrop Grumman Shipbuilding Inc. (43689) |