At NSN Unlimited, we maintain a large database of parts AMS-QQ-A-200 15, CVC10010-170CJ, QQ-A-200 15 with NSN 9540-01-429-4910 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Triumph Aerostructures Llc, Society Of Automotive Engineers Inc, Sae International, Federal Specifications, 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: 9540-01-429-4910 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 014294910 |
| NCB Code: USA (01) |
| Manufacturers: Triumph Aerostructures Llc , Society Of Automotive Engineers Inc , Sae International , Federal Specifications , Vought Aircraft Industries Inc |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| AMS-QQ-A-200 15 | 9540-01-429-4910 | beam structural | triumph aerostructures llc | Avl | RFQ |
| AMS-QQ-A-200 15 | 9540-01-429-4910 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 15 | 9540-01-429-4910 | beam structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 15 | 9540-01-429-4910 | beam structural | federal specifications | Avl | RFQ |
| CVC10010-170CJ | 9540-01-429-4910 | beam structural | federal specifications | Avl | RFQ |
| CVC10010-170CJ | 9540-01-429-4910 | beam structural | triumph aerostructures llc | Avl | RFQ |
| CVC10010-170CJ | 9540-01-429-4910 | beam structural | society of automotive engineers inc | Avl | RFQ |
| CVC10010-170CJ | 9540-01-429-4910 | beam structural | vought aircraft industries inc | Avl | RFQ |
| QQ-A-200 15 | 9540-01-429-4910 | beam structural | triumph aerostructures llc | Avl | RFQ |
| QQ-A-200 15 | 9540-01-429-4910 | beam structural | society of automotive engineers inc | Avl | RFQ |
| QQ-A-200 15 | 9540-01-429-4910 | beam structural | federal specifications | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AJJP | LEG THICKNESS | 0.150 INCHES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/15, ALLOY 7075 |
| 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 | B-2 BOMBER |
| BQJG | TOP FLANGE WIDTH | 4.000 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBD | FIRST TIP INNER RADIUS | 0.032 INCHES NOMINAL |
| CNBJ | FIRST TIP OUTER RADIUS | 0.032 INCHES NOMINAL |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER T76511 |
| 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 | 2.750 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.000 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET 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 | 0.150 INCHES NOMINAL |
| AARN | FABRICATION METHOD | EXTRUDED |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.150 INCHES NOMINAL |
| HEAT | HEAT TREATMENT | T-76511 SOLUTION HEAT TREATED |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
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