NSN 1560-01-183-2036 32-15004-56, 01-183-2036, 321500456
Product Details | AIRCRAFT SPAR
1560-01-183-2036 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: 32-15004-56, 1560-01-183-2036, 01-183-2036, 1560011832036, 321500456, 011832036
Aircraft and Airframe Structural Components | Airframe Structural Components
Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
---|---|---|---|
15 | 01-183-2036 | 41028 ( SPAR, AIRCRAFT ) |
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Related Products | NSN 1560-01-183-2036
Technical Data | NSN 1560-01-183-2036
Characteristic | Specifications |
---|---|
MATERIAL | ALUMINUM ALLOY 7075 |
MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE |
AIRCRAFT LOCATION | TRAILING EDGE ASSEMBLY,OUTER WING |
AIRCRAFT MISSION DESIGN SERIES | F-4 |
OVERALL LENGTH | 5.600 INCHES NOMINAL |
OVERALL WIDTH | 4.000 INCHES NOMINAL |
MATERIAL THICKNESS | 0.040 INCHES NOMINAL |
MANUFACTURERS CODE | 76301 |
DESIGN CONTROL REFERENCE | 32-15004-56 |
Restrictions/Controls & Freight Information | NSN 1560-01-183-2036
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 |