ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers 1MA160B01-10406, 60-13867, QQ-A-200 3, ASTM B221 under NSN 9540-01-363-4315 of Beam Structural manufactured by Boeing Company, Transtar Metals Corp, Federal Specifications Promulgat, American Society For.
Federal Supply Class of NSN 9540-01-363-4315 is FSC 9540 contains part details of Structural Shapes Nonferrous Base Metal. Quote for your desired part numbers.
| Item Name | Beam Structural |
| Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC) | 9540 Structural Shapes Nonferrous Base Metal |
| National Item Identification Number (NIIN) | 01-363-4315 (013634315) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company, Transtar Metals Corp, Federal Specifications Promulgat, American Society For |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 1MA160B01-10406 | boeing company | beam structural | RFQ |
| 60-13867 | transtar metals corp | beam structural | RFQ |
| QQ-A-200 3 | federal specifications promulgat | beam structural | RFQ |
| ASTM B221 | american society for | beam structural | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.750 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT 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 | 2.230 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.390 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 | 4.620 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.880 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 | O-ANNEALED |
| MATT | MATERIAL | ALUMINUM ALLOY, ASTM B221, ALLOY 2024 |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.100 INCHES NOMINAL |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND ANNEALED CONDITION |
| Relevant Components for NSN - 9540-01-363-4315, 9540013634315 | ||||
| 9505-00-004-3522 (9505000043522) | 9505-00-006-5050 (9505000065050) | 9505-00-020-6766 (9505000206766) | 9505-00-023-0121 (9505000230121) | |
| 9505-00-023-4467 (9505000234467) | 9505-00-027-2485 (9505000272485) | 9505-00-027-7789 (9505000277789) | 9505-00-035-7535 (9505000357535) | |
| 9505-00-044-2161 (9505000442161) | 9505-00-051-1088 (9505000511088) | 9505-00-054-7077 (9505000547077) | 9505-00-056-1761 (9505000561761) | |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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