At NSN Unlimited, we maintain a large database of parts 30081, 34951, 60-8530, 6341, AMS QQ A 200 3 with NSN 9540-00-287-9338 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Aluminum Co Of America, Alcoa Reynolds Metals Company, Transtar Metals Corp, Society Of Automotive Engineers Inc, Sae International. 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: 9540-00-287-9338 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 002879338 |
| NCB Code: USA (00) |
| Manufacturers: Aluminum Co Of America , Alcoa Reynolds Metals Company , Transtar Metals Corp , Society Of Automotive Engineers Inc , Sae International , The Boeing Company , Federal Specifications , Hiller Aircraft Corporation |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 30081 | 9540-00-287-9338 | beam structural | aluminum co of america | Avl | RFQ |
| 34951 | 9540-00-287-9338 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| 60-8530 | 9540-00-287-9338 | beam structural | transtar metals corp | Avl | RFQ |
| 6341 | 9540-00-287-9338 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| AMS QQ A 200 3 | 9540-00-287-9338 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 3 | 9540-00-287-9338 | beam structural | sae international | Avl | RFQ |
| BAC1505-46618 | 9540-00-287-9338 | beam structural | the boeing company | Avl | RFQ |
| BAC1505-46618 | 9540-00-287-9338 | beam structural | aluminum co of america | Avl | RFQ |
| BAC1505-46618 | 9540-00-287-9338 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| BAC1505-46618 | 9540-00-287-9338 | beam structural | federal specifications | Avl | RFQ |
| FS50116-2930 | 9540-00-287-9338 | beam structural | federal specifications | Avl | RFQ |
| FS50116-2930 | 9540-00-287-9338 | beam structural | hiller aircraft corporation | Avl | RFQ |
| FS50116-2930 | 9540-00-287-9338 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| FS50116-2930 | 9540-00-287-9338 | beam structural | aluminum co of america | Avl | RFQ |
| LS3716 | 9540-00-287-9338 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| LS3716 | 9540-00-287-9338 | beam structural | federal specifications | Avl | RFQ |
| LS3716 | 9540-00-287-9338 | beam structural | aluminum co of america | Avl | RFQ |
| PA6722 | 9540-00-287-9338 | beam structural | transtar metals corp | Avl | RFQ |
| QQ A 200 3 | 9540-00-287-9338 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 3 | 9540-00-287-9338 | beam structural | aluminum co of america | Avl | RFQ |
| QQ-A-200 3 | 9540-00-287-9338 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 3.000 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.350 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.350 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.200 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.450 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.450 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.200 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.200 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.900 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 1.880 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T3511 TEMPER |
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