The NSN 9540-01-189-8617 part numbers QQ-A-200 11, PA1382, AMS QQ A 200 11, 16102, 60-339 manufactured by Federal Specifications Promulgat, Transtar Metals Corp, Sae International, Alcoa Reynolds Metals Company, Litton Industries Inc 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 9540-01-189-8617 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 9540-01-189-8617 parts of Beam Structural, and one of our account managers will respond to it within fifteen minutes or less.
| Alternative NSN: 9540-01-189-8617 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 011898617 |
| NCB Code: USA (01) |
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| QQ-A-200 11 | federal specifications promulgat | beam structural | Avl | RFQ |
| PA1382 | transtar metals corp | beam structural | Avl | RFQ |
| AMS QQ A 200 11 | sae international | beam structural | Avl | RFQ |
| 16102 | alcoa reynolds metals company | beam structural | Avl | RFQ |
| 60-339 | transtar metals corp | beam structural | Avl | RFQ |
| 89615-2350 | litton industries inc | beam structural | Avl | RFQ |
| 1MA160D05-10322 | boeing company | beam structural | Avl | RFQ |
| AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.734 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 3.625 INCHES NOMINAL |
| CNBD | FIRST TIP INNER RADIUS | 0.031 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| HEAT | HEAT TREATMENT | T-73511 SOLUTION HEAT TREATED |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T73511 TEMPER |
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.750 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.125 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.734 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.804 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBJ | FIRST TIP OUTER RADIUS | 0.031 INCHES NOMINAL |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
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