At NSN Unlimited, we maintain a large database of parts AMS-QQ-A-200 11, CVC10010 114CA, CVC10010-114CA, QQ-A-200 11 with NSN 9540-01-429-3726 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Sae International, Federal Specifications, Triumph Aerostructures Llc, Society Of Automotive Engineers Inc, Vought Aircraft Industries 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: 9540-01-429-3726 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 014293726 |
| NCB Code: USA (01) |
| Manufacturers: Sae International , Federal Specifications , Triumph Aerostructures Llc , Society Of Automotive Engineers Inc , Vought Aircraft Industries Inc |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| AMS-QQ-A-200 11 | 9540-01-429-3726 | beam structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-429-3726 | beam structural | federal specifications | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-429-3726 | beam structural | triumph aerostructures llc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-429-3726 | beam structural | society of automotive engineers inc | Avl | RFQ |
| CVC10010 114CA | 9540-01-429-3726 | beam structural | triumph aerostructures llc | Avl | RFQ |
| CVC10010-114CA | 9540-01-429-3726 | beam structural | vought aircraft industries inc | Avl | RFQ |
| CVC10010-114CA | 9540-01-429-3726 | beam structural | society of automotive engineers inc | Avl | RFQ |
| CVC10010-114CA | 9540-01-429-3726 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 11 | 9540-01-429-3726 | beam structural | triumph aerostructures llc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-429-3726 | beam structural | society of automotive engineers inc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-429-3726 | beam structural | federal specifications | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AJJP | LEG THICKNESS | 0.107 INCHES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.760 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.170 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.170 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | B-2 BOMBER |
| BQJG | TOP FLANGE WIDTH | 5.520 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBD | FIRST TIP INNER RADIUS | 0.020 INCHES NOMINAL |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER 0 |
| CNBJ | FIRST TIP OUTER RADIUS | 0.020 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| ABKW | OVERALL HEIGHT | 1.730 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.760 INCHES NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.107 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.107 INCHES NOMINAL |
| AARN | FABRICATION METHOD | EXTRUDED |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
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