The Plate,structural,aircraft, cataloged under National Stock Number 1560-01-732-9594, is classified within Federal Supply Class 1560 (No Item Name Available) of the Aircraft and Airframe Components group. The primary manufacturer of record is The Boeing Company. Government technical data includes 2 verified specifications, sourced from the Federal Logistics Information System. This item has 1 commercial cross-reference from 1 manufacturer, enabling identification through both NSN and commercial part number lookups. 8 verified substitutes exist in the government interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 1560-01-732-9594 |
| Primary Part Number | 352SK233-201 |
| Item Name | Plate,structural,aircraft |
| FSC / FSG | 1560 / 15 — No Item Name Available |
| Manufacturer | The Boeing Company |
| Status | ACTIVE |
| Material Thickness | 0.063 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| 352SK233-201 PRIMARY | The Boeing Company (USA) |
NSN 1560-01-732-9594 is a Plate,structural,aircraft, manufactured by The Boeing Company, classified under FSC 1560 (No Item Name Available). Status: active.
NSN 1560-01-732-9594 has 1 cross-referenced part number: 352SK233-201 (The Boeing Company).
There are 8 known substitutes for 1560-01-732-9594: 1560-00-000-0047, 1560-00-001-1849, 1560-00-001-1850 and 5 more. Verify interchangeability with system specifications before substitution.
Key specifications for 352SK233-201: Part Name Assigned by Controlling Agency: UPPER DOUBLER; Special Features: MATERIAL IS ALUMINUM ALLOY SHEET, 20.5 INCHES BY 10.25 INCHES BY 0.063 INCHES THICK. IN; Material Thickness: 0.063 INCHES NOMINAL IN; Material: ALUMINUM ALLOY. 4 total characteristics are documented in the Federal Logistics Information System.