At NSN Unlimited, we maintain a large database of parts 60 10675, 60-10675, AMS QQ A 200 11, AMS-QQ-A-200 11, ASTM B221 with NSN 9540-01-428-2776 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Transtar Metals Corp, Vought Aircraft Industries Inc, Triumph Aerostructures Llc, American Society For Testing And, Federal Specifications. 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: 9540-01-428-2776 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 014282776 |
| NCB Code: USA (01) |
| Manufacturers: Transtar Metals Corp , Vought Aircraft Industries Inc , Triumph Aerostructures Llc , American Society For Testing And , Federal Specifications , Sae International , Society Of Automotive Engineers Inc |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 60 10675 | 9540-01-428-2776 | beam structural | transtar metals corp | Avl | RFQ |
| 60-10675 | 9540-01-428-2776 | beam structural | vought aircraft industries inc | Avl | RFQ |
| 60-10675 | 9540-01-428-2776 | beam structural | triumph aerostructures llc | Avl | RFQ |
| 60-10675 | 9540-01-428-2776 | beam structural | american society for testing and | Avl | RFQ |
| 60-10675 | 9540-01-428-2776 | beam structural | federal specifications | Avl | RFQ |
| AMS QQ A 200 11 | 9540-01-428-2776 | beam structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-428-2776 | beam structural | triumph aerostructures llc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-428-2776 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-428-2776 | beam structural | federal specifications | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-428-2776 | beam structural | american society for testing and | Avl | RFQ |
| ASTM B221 | 9540-01-428-2776 | beam structural | federal specifications | Avl | RFQ |
| ASTM B221 | 9540-01-428-2776 | beam structural | american society for testing and | Avl | RFQ |
| ASTM B221 | 9540-01-428-2776 | beam structural | triumph aerostructures llc | Avl | RFQ |
| CVC10012-36CH | 9540-01-428-2776 | beam structural | triumph aerostructures llc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-428-2776 | beam structural | triumph aerostructures llc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-428-2776 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 11 | 9540-01-428-2776 | beam structural | american society for testing and | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AJJP | LEG THICKNESS | 0.140 INCHES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.190 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | B-2 BOMBER |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.190 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 4.000 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 1.594 POUNDS PER SQUARE FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER T73511 |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 100.0 DEGREES NOMINAL |
| ABKW | OVERALL HEIGHT | 5.500 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.000 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.000 INCHES NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.140 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.140 INCHES NOMINAL |
| AARN | FABRICATION METHOD | EXTRUDED |
| CRZC | RIGHT TOP INSIDE ANGLE | 80.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-73511 SOLUTION HEAT TREATED |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
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