The NSN 9540-01-093-9731 part numbers CVC10010-99CA, PA6222, AMS-QQ-A-200 11, 60-16632, 26846 manufactured by Triumph Actuation Systems, Transtar Metals Corp, Triumph Aerostructures Llc, Society Of Automotive Engineers Inc, Sae International is available in our inventory. As an ASAP Semiconductor owned and operated website, ASAP Aviation Unlimited has access to over three billion parts, paired with easy-to-use search engines that enable our customers to browse through our NSN 9540-01-093-9731 inventory quickly and efficiently. Our focus on quality control has earned us our FAA AC 0056B accreditation and AS9120B, ISO 9001:2015 certification, and we are the only independent distributor with a No China Sourcing pledge. If you are ready to get started, you can send an Instant RFQ form from this page for NSN 9540-01-093-9731 parts of Beam Structural, and one of our account managers will respond to it within fifteen minutes or less.
| Alternative NSN: 9540-01-093-9731 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 010939731 |
| NCB Code: USA (01) |
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| CVC10010-99CA | triumph actuation systems | beam structural | Avl | RFQ |
| PA6222 | transtar metals corp | beam structural | Avl | RFQ |
| CVC10010-99CA | triumph aerostructures llc | beam structural | Avl | RFQ |
| AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | Avl | RFQ |
| 60-16632 | transtar metals corp | beam structural | Avl | RFQ |
| AMS-QQ-A-200 11 | sae international | beam structural | Avl | RFQ |
| 26846 | aluminum co of america | beam structural | Avl | RFQ |
| QQ A 200 11 | federal specifications promulgat | beam structural | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABKW | OVERALL HEIGHT | 2.650 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.248 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.400 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.870 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 110.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| AARN | FABRICATION METHOD | EXTRUDED |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.248 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.060 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.370 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CRZC | RIGHT TOP INSIDE ANGLE | 70.0 DEGREES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | O TEMPER |
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