NSN 1560-01-146-9416 32110245, 32-11024-5, 01-146-9416
Product Details | AIRCRAFT STRUCTURAL COMPONENT WEB
1560-01-146-9416 An item designed as a principal member of various primary structures within an aircraft. It provides strength, rigidity and the like while maintaining the proper dimensional distances as required. It may include holes for mounting and/or joining to other items to form an assembly.
Part Alternates: 32110245, 32-11024-5, 1560-01-146-9416, 01-146-9416, 1560011469416, 011469416
Aircraft and Airframe Structural Components | Airframe Structural Components
| Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | 01-146-9416 | 41019 ( WEB, STRUCTURAL COMPONENT, AIRCRAFT ) |
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Technical Data | NSN 1560-01-146-9416
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| AIRCRAFT LOCATION | RIB ASSY, CTR SECT WING CLOSURE |
| AIRCRAFT MISSION DESIGN SERIES | F-4 |
| OVERALL LENGTH | 15.700 INCHES NOMINAL |
| OVERALL WIDTH | 11.980 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.010 INCHES NOMINAL |
| SPECIAL FEATURES | TEMPER T6 |
| MANUFACTURERS CODE | 76301 |
| DESIGN CONTROL REFERENCE | 32-11024-5 |
Restrictions/Controls & Freight Information | NSN 1560-01-146-9416
| 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 | ||



