NSN 1560-01-188-0214 3215502281, 32-15502-281, 01-188-0214
Product Details | AIRCRAFT STRUCTURAL PLATE
1560-01-188-0214 A flat or preformed item of metallic or nonmetallic material. It may vary in shape and its surface may be smooth and/or serrated. Its thickness is small in comparison to both its length and width. It is designed to be mounted upon a surface or between two surfaces. Its primary function is to strengthen, join, or separate aircraft structural parts. Excludes PLATE, MENDING; SHIM; and SPACER, PLATE.
Part Alternates: 3215502281, 32-15502-281, 1560-01-188-0214, 01-188-0214, 1560011880214, 011880214
Aircraft and Airframe Structural Components | Airframe Structural Components
| Supply Group (FSG) | NSN Assign. | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 15 | 01-188-0214 | 31495 ( PLATE, STRUCTURAL, AIRCRAFT ) |
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Technical Data | NSN 1560-01-188-0214
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/5 T3 FED SPEC SINGLE MATERIAL RESPONSE |
| AIRCRAFT LOCATION | WING ASSEMBLY,OUTER STRUCTURE |
| AIRCRAFT MISSION DESIGN SERIES | F-4 |
| OVERALL LENGTH | 9.760 INCHES NOMINAL |
| OVERALL WIDTH | 1.700 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.063 INCHES NOMINAL |
| SPECIAL FEATURES | OPPOSITE -282; STRAP |
| MANUFACTURERS CODE | 76301 |
| DESIGN CONTROL REFERENCE | 32-15502-281 |
Restrictions/Controls & Freight Information | NSN 1560-01-188-0214
| 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 | ||