At NSN Unlimited, we maintain a large database of parts AMS-QQ-A-200 11, CVC10012-222CA, QQ-A-200 11 with NSN 9540-01-428-5990 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: 9540-01-428-5990 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 014285990 |
| 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 11 | 9540-01-428-5990 | beam structural | triumph aerostructures llc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-428-5990 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-428-5990 | beam structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-428-5990 | beam structural | federal specifications | Avl | RFQ |
| CVC10012-222CA | 9540-01-428-5990 | beam structural | federal specifications | Avl | RFQ |
| CVC10012-222CA | 9540-01-428-5990 | beam structural | society of automotive engineers inc | Avl | RFQ |
| CVC10012-222CA | 9540-01-428-5990 | beam structural | vought aircraft industries inc | Avl | RFQ |
| CVC10012-222CA | 9540-01-428-5990 | beam structural | triumph aerostructures llc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-428-5990 | beam structural | triumph aerostructures llc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-428-5990 | beam structural | society of automotive engineers inc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-428-5990 | beam structural | federal specifications | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AJJP | LEG THICKNESS | 0.608 INCHES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 3.320 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.198 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.198 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | B-2 BOMBER |
| BQJG | TOP FLANGE WIDTH | 6.360 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER 0 |
| CNBD | FIRST TIP INNER RADIUS | 0.031 INCHES NOMINAL |
| CNBJ | FIRST TIP OUTER RADIUS | 0.031 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 94.0 DEGREES NOMINAL |
| ABKW | OVERALL HEIGHT | 3.930 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 3.040 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 1.055 INCHES NOMINAL |
| AARN | FABRICATION METHOD | EXTRUDED |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 1.055 INCHES NOMINAL |
| CRZC | RIGHT TOP INSIDE ANGLE | 86.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
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