The Fairing,aircraft, cataloged under National Stock Number 1560-01-397-0451, is classified within Federal Supply Class 1560 (Airframe Structural Components) of the Aircraft and Airframe Components group. The manufacturer of record is Aero Components, Llc. Government technical data includes 7 specifications, cited from the U.S. Government catalog. The record lists 1 manufacturer part number for this item, enabling identification through both NSN and commercial part number lookups. 2 additional reference documents (drawings, advisory and superseded references) are recorded in the U.S. Government catalog. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 1560-01-397-0451 |
| Primary Part Number | 123P40725-17 |
| Item Name | Fairing,aircraft |
| FSC / FSG | 1560 / 15 — Airframe Structural Components |
| Manufacturer | Aero Components, Llc |
| Status | ACTIVE |
| Aircraft Station Number | FS517 |
| Material Document and Classification | QQ-A-250/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Material Thickness | 0.040 INCHES NOMINAL IN |
| Aircraft Location | FUSELAGE |
| Material | ALUMINUM ALLOY 6061 |
| Side for Which Designed | BOTH SIDES |
| Aircraft Mission Design Series | C-2A A |
| Acquisition Status | ACTIVE |
| DEMIL Code | DEMIL Q — CCL Item — Commerce Control List |
| Hazard | Possible hazard — SDS may be required (DLA HMIC P) |
| Criticality Code | X |
| Part Number | Manufacturer |
|---|---|
| 123P40725-17 PRIMARY | Aero Components, Llc (USA) |
| Reference | Meaning |
|---|---|
| 123P40725-17 | 5/9 Secondary reference Northrop Grumman Systems Corporation |
| 123P40725-17 | C/1 Advisory reference — outside the item-of-supply concept Northrop Grumman Systems Corporation |
NSN 1560-01-397-0451 is a Fairing,aircraft, manufactured by Aero Components, Llc, classified under FSC 1560, Airframe Structural Components. Status: active.
NSN 1560-01-397-0451 has 1 manufacturer part number on file: 123P40725-17 (Aero Components, Llc).
Key specifications for 123P40725-17: Aircraft Station Number: FS517; Material Document and Classification: QQ-A-250/11 FED SPEC SINGLE MATERIAL RESPONSE; Material Thickness: 0.040 INCHES NOMINAL IN; Aircraft Location: FUSELAGE. 7 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.
NSN 1560-01-397-0451 has DEMIL Code Q. Demilitarization may be required before disposal or transfer to non-military entities.
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.