At NSN Unlimited, we maintain a large database of parts 1MA160D05-10323, 60-21205, AMS-QQ-A-200 11, QQ-A-200 11 with NSN 9540-01-364-1574 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Transtar Metals Corp, Boeing Company The, Society Of Automotive Engineers Inc, Sae International, Federal Specifications. 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: 9540-01-364-1574 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 013641574 |
| NCB Code: USA (01) |
| Manufacturers: Transtar Metals Corp , Boeing Company The , Society Of Automotive Engineers Inc , Sae International , Federal Specifications |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 1MA160D05-10323 | 9540-01-364-1574 | beam structural | transtar metals corp | Avl | RFQ |
| 1MA160D05-10323 | 9540-01-364-1574 | beam structural | boeing company the | Avl | RFQ |
| 1MA160D05-10323 | 9540-01-364-1574 | beam structural | society of automotive engineers inc | Avl | RFQ |
| 60-21205 | 9540-01-364-1574 | beam structural | society of automotive engineers inc | Avl | RFQ |
| 60-21205 | 9540-01-364-1574 | beam structural | transtar metals corp | Avl | RFQ |
| 60-21205 | 9540-01-364-1574 | beam structural | boeing company the | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-364-1574 | beam structural | boeing company the | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-364-1574 | beam structural | transtar metals corp | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-364-1574 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-364-1574 | beam structural | sae international | Avl | RFQ |
| QQ-A-200 11 | 9540-01-364-1574 | beam structural | transtar metals corp | Avl | RFQ |
| QQ-A-200 11 | 9540-01-364-1574 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 11 | 9540-01-364-1574 | beam structural | society of automotive engineers inc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-364-1574 | beam structural | boeing company the | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.125 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.750 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.875 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.187 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.187 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 3.625 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.926 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| 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 |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| HEAT | HEAT TREATMENT | T-73511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY, AMS-QQ-A-200/11, ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T73511 TEMPER |
| ABKW | OVERALL HEIGHT | 2.562 INCHES NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
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