At NSN Unlimited, we maintain a large database of parts 1MA160D01-10503, 60 18507 7075 O, 60-18507 7075-O, AMS-QQ-A-200 11, QQ-A-200 11 with NSN 9540-01-363-8539 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Federal Specifications, Boeing Company The, Transtar Metals Corp, Society Of Automotive Engineers Inc. 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: 9540-01-363-8539 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 013638539 |
| NCB Code: USA (01) |
| Manufacturers: Federal Specifications , Boeing Company The , Transtar Metals Corp , Society Of Automotive Engineers Inc |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 1MA160D01-10503 | 9540-01-363-8539 | beam structural | federal specifications | Avl | RFQ |
| 1MA160D01-10503 | 9540-01-363-8539 | beam structural | boeing company the | Avl | RFQ |
| 1MA160D01-10503 | 9540-01-363-8539 | beam structural | transtar metals corp | Avl | RFQ |
| 60 18507 7075 O | 9540-01-363-8539 | beam structural | transtar metals corp | Avl | RFQ |
| 60-18507 7075-O | 9540-01-363-8539 | beam structural | federal specifications | Avl | RFQ |
| 60-18507 7075-O | 9540-01-363-8539 | beam structural | boeing company the | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-363-8539 | beam structural | boeing company the | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-363-8539 | beam structural | federal specifications | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-363-8539 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-363-8539 | beam structural | transtar metals corp | Avl | RFQ |
| QQ-A-200 11 | 9540-01-363-8539 | beam structural | transtar metals corp | Avl | RFQ |
| QQ-A-200 11 | 9540-01-363-8539 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 11 | 9540-01-363-8539 | beam structural | boeing company the | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.500 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.100 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.100 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.100 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.800 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.450 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 | 4.250 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.686 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| 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 |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND ANNEALED CONDITION |
| MATT | MATERIAL | ALUMINUM ALLOY, AMS-QQ-A-200/11, ALLOY 7075 |
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