The Panel,structural,aircraft, cataloged under National Stock Number 1560-01-463-5083, is classified within Federal Supply Class 1560 (Airframe Structural Components) of the Aircraft and Airframe Components group. Government technical data includes 4 specifications, cited from the U.S. Government catalog. 1 additional reference document (drawings, advisory and superseded references) is recorded in the U.S. Government catalog. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 1560-01-463-5083 |
| Item Name | Panel,structural,aircraft |
| FSC / FSG | 1560 / 15 — Airframe Structural Components |
| Status | ACTIVE |
| Material Document and Classification | QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE |
| Aircraft Location | ENGINE NACELLE |
| Material | ALUMINUM ALLOY 2024 |
| Aircraft Mission Design Series | C-17A A |
| Acquisition Status | ACTIVE |
| DEMIL Code | DEMIL A — No Demilitarization Required |
| Hazard | Possible hazard — SDS may be required (DLA HMIC P) |
| Criticality Code | X |
| Reference | Meaning |
|---|---|
| 17P8D9242-1 | 3/2 Design control — primary reference U.S. Government activity |
NSN 1560-01-463-5083 is a Panel,structural,aircraft, classified under FSC 1560, Airframe Structural Components. Status: active.
Key specifications for 1560-01-463-5083: Material Document and Classification: QQ-A-250/4 FED SPEC SINGLE MATERIAL RESPONSE; Special Features: MANUFACTURER SUGGESTED NAME - PANEL ASSEMBLY,OUTER FORWARD TRANSLATING FAN DUCT;NHA 17P8D9211; Aircraft Location: ENGINE NACELLE; Material: ALUMINUM ALLOY 2024. 4 specifications are documented in the U.S. Government catalog.
Possible hazard — SDS may be required (DLA HMIC P). Hazard information on this page is shown exactly as it appears in the DLA record.
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-16.
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.