At NSN Unlimited, we maintain a large database of parts 1M5218, 1MA160D01-10167, 60-1922, AMS STD 184, AMS-QQ-A-200 11 with NSN 9540-01-038-9749 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Transtar Metals Corp, Society Of Automotive Engineers Inc, Boeing Company The, 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: 9540-01-038-9749 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 010389749 |
| NCB Code: USA (01) |
| Manufacturers: Transtar Metals Corp , Society Of Automotive Engineers Inc , Boeing Company The , Sae International , Federal Specifications |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 1M5218 | 9540-01-038-9749 | beam structural | transtar metals corp | Avl | RFQ |
| 1M5218 | 9540-01-038-9749 | beam structural | society of automotive engineers inc | Avl | RFQ |
| 1M5218 | 9540-01-038-9749 | beam structural | boeing company the | Avl | RFQ |
| 1MA160D01-10167 | 9540-01-038-9749 | beam structural | boeing company the | Avl | RFQ |
| 60-1922 | 9540-01-038-9749 | beam structural | transtar metals corp | Avl | RFQ |
| AMS STD 184 | 9540-01-038-9749 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-038-9749 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-038-9749 | beam structural | transtar metals corp | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-038-9749 | beam structural | boeing company the | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-038-9749 | beam structural | sae international | Avl | RFQ |
| AMS-STD-184 | 9540-01-038-9749 | beam structural | sae international | Avl | RFQ |
| AMS-STD-184 | 9540-01-038-9749 | beam structural | boeing company the | Avl | RFQ |
| AMS-STD-184 | 9540-01-038-9749 | beam structural | transtar metals corp | Avl | RFQ |
| QQ-A-200 11 | 9540-01-038-9749 | beam structural | transtar metals corp | Avl | RFQ |
| QQ-A-200 11 | 9540-01-038-9749 | beam structural | society of automotive engineers inc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-038-9749 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 11 | 9540-01-038-9749 | beam structural | boeing company the | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.250 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.063 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 | 1.750 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 3.500 INCHES NOMINAL |
| 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 | O-ANNEALED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | O TEMPER |
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