The Beam,structural, cataloged under National Stock Number 9540-01-077-0096, is classified within Federal Supply Class 9540 (Structural Shapes, Nonferrous Base Metal) of the Metal Bars, Sheets, and Shapes group. The manufacturer of record is Sikorsky Aircraft Corporation Dba Sikorsky Aircraft Corp. Government technical data includes 18 specifications, cited from the U.S. Government catalog. The record lists 2 manufacturer part numbers for this item, enabling identification through both NSN and commercial part number lookups. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-077-0096 |
| Primary Part Number | 65201-06025-006QQA200-11 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — Structural Shapes, Nonferrous Base Metal |
| Manufacturer | Sikorsky Aircraft Corporation Dba Sikorsky Aircraft Corp |
| Status | ACTIVE |
| Right Side Top Flange Thickness | 0.100 INCHES NOMINAL IN |
| Length | 0.198 FEET NOMINAL FT |
| Left Side Top Flange Distance to Center of Both Flanges | 0.950 INCHES NOMINAL IN |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.188 INCHES NOMINAL IN |
| Material Document and Classification | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.188 INCHES NOMINAL IN |
| Basic Shape Style | T SHAPE |
| Top Flange Width | 1.900 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 7075 |
| Fabrication Method | DIE CAST |
| Leg Thickness | 0.100 INCHES NOMINAL IN |
| First Tip Style | SQUARE END |
| Leg Tip Thickness | 0.040 INCHES NOMINAL IN |
| Left Side Top Flange Thickness | 0.100 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | IDENTICAL |
| Right Side Top Flange Distance to Center of Both Flanges | 0.950 INCHES NOMINAL IN |
| Acquisition Status | ACTIVE |
| DEMIL Code | DEMIL A — No Demilitarization Required |
| Hazard | No hazard code in the DLA record (HMIC N) |
| Criticality Code | X |
| Part Number | Manufacturer |
|---|---|
| 65201-06025-006QQA200-11 PRIMARY | Sikorsky Aircraft Corporation Dba Sikorsky Aircraft Corp (USA) |
| 65201-06025-006 | Sikorsky Aircraft Corporation Dba Sikorsky Aircraft Corp (USA) |
NSN 9540-01-077-0096 is a Beam,structural, manufactured by Sikorsky Aircraft Corporation Dba Sikorsky Aircraft Corp, classified under FSC 9540, Structural Shapes, Nonferrous Base Metal. Status: active.
NSN 9540-01-077-0096 has 2 manufacturer part numbers on file: 65201-06025-006QQA200-11 (Sikorsky Aircraft Corporation Dba Sikorsky Aircraft Corp), 65201-06025-006 (Sikorsky Aircraft Corporation Dba Sikorsky Aircraft Corp).
Key specifications for 65201-06025-006QQA200-11: Overall Height: 2.350 INCHES NOMINAL IN; Right Side Top Flange Thickness: 0.100 INCHES NOMINAL IN; Length: 0.198 FEET NOMINAL FT; Left Side Top Flange Distance to Center of Both Flanges: 0.950 INCHES NOMINAL IN. 18 specifications are documented in the U.S. Government catalog.
No hazard code in the DLA record (HMIC N). 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.