NSN 1560-01-185-6404 53-46501-75, 01-185-6404, 534650175
Product Details | AIRCRAFT SPAR
1560-01-185-6404 A principal spanwise member of the structural framework of a wing, stabilizer, other airfoil, and the like. It is designed to absorb bending loads applied to the airfoil.
Part Alternates: 53-46501-75, 1560-01-185-6404, 01-185-6404, 1560011856404, 534650175, 011856404
Aircraft and Airframe Structural Components | Airframe Structural Components
| Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | 01-185-6404 | 41028 ( SPAR, AIRCRAFT ) |
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Related Products | NSN 1560-01-185-6404
Technical Data | NSN 1560-01-185-6404
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7178 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE |
| AIRCRAFT MISSION DESIGN SERIES | F-4 |
| OVERALL LENGTH | 17.400 INCHES NOMINAL |
| OVERALL WIDTH | 2.700 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.040 INCHES NOMINAL |
| MANUFACTURERS CODE | 76301 |
| DESIGN CONTROL REFERENCE | 53-46501-75 |
Restrictions/Controls & Freight Information | NSN 1560-01-185-6404
| Category | Code | Description |
|---|---|---|
| Hazardous Material Indicator Code | P | There is no information in the HMIS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product |
| Category | Code | Description |
|---|---|---|
| No Freight Information | ||



