At NSN Unlimited, we maintain a large database of parts 1MA160D01-10215, 60 7563, 60-7563, AMS QQ A 200 11, AMS-QQ-A-200 11 with NSN 9540-01-496-0719 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Transtar Metals Corp, Federal Specifications, Boeing Company The, 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: 9540-01-496-0719 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 014960719 |
| NCB Code: USA (01) |
| Manufacturers: Transtar Metals Corp , Federal Specifications , Boeing Company The , Society Of Automotive Engineers Inc , Sae International |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 1MA160D01-10215 | 9540-01-496-0719 | beam structural | transtar metals corp | Avl | RFQ |
| 1MA160D01-10215 | 9540-01-496-0719 | beam structural | federal specifications | Avl | RFQ |
| 1MA160D01-10215 | 9540-01-496-0719 | beam structural | boeing company the | Avl | RFQ |
| 60 7563 | 9540-01-496-0719 | beam structural | transtar metals corp | Avl | RFQ |
| 60-7563 | 9540-01-496-0719 | beam structural | federal specifications | Avl | RFQ |
| 60-7563 | 9540-01-496-0719 | beam structural | boeing company the | Avl | RFQ |
| AMS QQ A 200 11 | 9540-01-496-0719 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-496-0719 | beam structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-496-0719 | beam structural | transtar metals corp | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-496-0719 | beam structural | federal specifications | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-496-0719 | beam structural | boeing company the | Avl | RFQ |
| QQ-A-200 11 | 9540-01-496-0719 | beam structural | transtar metals corp | Avl | RFQ |
| QQ-A-200 11 | 9540-01-496-0719 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 11 | 9540-01-496-0719 | beam structural | boeing company the | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AJJP | LEG THICKNESS | 0.063 INCHES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY, AMS-QQ-A-200/11, ALLOY 7075 |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.130 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.130 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.900 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.336 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075,TEMPER COND 0 |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| ABKW | OVERALL HEIGHT | 1.500 INCHES NOMINAL |
| FEAT | SPECIAL FEATURES | ANGLE ENDS ARE RADIUS PER DATA PROVIDED |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.398 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.502 INCHES NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| AARN | FABRICATION METHOD | EXTRUDED |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
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