At NSN Unlimited, we maintain a large database of parts 60 12936, AMS QQ A 200 11, AMS-QQ-A-200, AMS-QQ-A-200 11, AMS-STD-184 with NSN 9540-01-523-9590 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Transtar Metals Corp, Society Of Automotive Engineers Inc. Utilize our interface to browse items by part number, part type, manufacturer, and more. Obtain insights on top MRO and FBO services, Manufacturer profiles, and part catalogs.
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| Alternative NSN: 9540-01-523-9590 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 015239590 |
| NCB Code: USA (01) |
| Manufacturers: Transtar Metals Corp , Society Of Automotive Engineers Inc |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 60 12936 | 9540-01-523-9590 | beam structural | transtar metals corp | Avl | RFQ |
| AMS QQ A 200 11 | 9540-01-523-9590 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 | 9540-01-523-9590 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 | 9540-01-523-9590 | beam structural | transtar metals corp | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-523-9590 | beam structural | transtar metals corp | Avl | RFQ |
| AMS-STD-184 | 9540-01-523-9590 | beam structural | transtar metals corp | Avl | RFQ |
| AMS-STD-184 | 9540-01-523-9590 | beam structural | society of automotive engineers inc | Avl | RFQ |
| LS30661-1 | 9540-01-523-9590 | beam structural | transtar metals corp | Avl | RFQ |
| LS30661-1 | 9540-01-523-9590 | beam structural | society of automotive engineers inc | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AJJP | LEG THICKNESS | 0.088 INCHES MINIMUM AND 0.100 INCHES MAXIMUM |
| MATL | MATERIAL | ALUMINUM ALLOY, AMS-QQ-A-200/11, ALLOY 7075 |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.478 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | C-5 AIRCRAFT |
| BQJG | TOP FLANGE WIDTH | 4.091 INCHES MINIMUM AND 4.159 INCHES MAXIMUM |
| ZZZK | SPECIFICATION/STANDARD DATA | 81348-QQ-A-277 GOVERNMENT SPECIFICATION |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| ABKW | OVERALL HEIGHT | 2.201 INCHES MINIMUM AND 2.249 INCHES MAXIMUM |
| CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | TEE SECTION-EXTRUDED |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.647 INCHES NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.088 INCHES MINIMUM AND 0.100 INCHES MAXIMUM |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.088 INCHES MINIMUM AND 0.100 INCHES MAXIMUM |
| AARN | FABRICATION METHOD | EXTRUDED |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
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