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 4712, PA14820, QQ-A-200 5, AMS-QQ-A-200 5, 853G under NSN 9540-00-542-2766 of Beam Structural manufactured by Alcoa Reynolds Metals Company, Transtar Metals Corp, Federal Specifications Promulgat, Society Of Automotive Engineers Inc, Aluminum Co Of America.
Federal Supply Class of NSN 9540-00-542-2766 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) | 00-542-2766 (005422766) |
| NCB Code | USA (00) |
| Manufacturer | Alcoa Reynolds Metals Company, Transtar Metals Corp, Federal Specifications Promulgat, Society Of Automotive Engineers Inc, Aluminum Co Of America, Sae International |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 4712 | alcoa reynolds metals company | beam structural | RFQ |
| PA14820 | transtar metals corp | beam structural | RFQ |
| QQ-A-200 5 | federal specifications promulgat | beam structural | RFQ |
| AMS-QQ-A-200 5 | society of automotive engineers inc | beam structural | RFQ |
| 853G | aluminum co of america | beam structural | RFQ |
| AMS-QQ-A-200 5 | sae international | beam structural | 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 | 0.281 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.281 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.281 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 1.500 INCHES NOMINAL |
| BQJK | LEFT SIDE TOP FLANGE TIP THICKNESS | 0.250 INCHES NOMINAL |
| BQJM | RIGHT SIDE TOP FLANGE TIP THICKNESS | 0.250 INCHES NOMINAL |
| BQKH | LEG TIP THICKNESS | 0.250 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.890 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 |
| CRYX | LEFT TOP INNER FACE TO OUTER FACE ANGLE | 90.0 DEGREES NOMINAL |
| CSTQ | RIGHT TOP INNER FACE TO OUTER FACE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | H-111 STRAIN HARDENED |
| MATT | MATERIAL | ALUMINUM ALLOY 5086 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/5 FED SPEC 1ST MATERIAL RESPONSE |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | H111 TEMPER |
| Relevant Components for NSN - 9540-00-542-2766, 9540005422766 | ||||
| 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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