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 38355, AMS QQA200 11, QQA200 11, AMS-QQA200-11 under NSN 9540-00-595-8597 of Beam Structural manufactured by Aluminum Co Of America, Society Of Automotive Engineers Inc, Federal Specifications Promulgat, Sae International.
Federal Supply Class of NSN 9540-00-595-8597 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) | 00-595-8597 (005958597) |
| NCB Code | USA (00) |
| Manufacturer | Aluminum Co Of America, Society Of Automotive Engineers Inc, Federal Specifications Promulgat, Sae International |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 38355 | aluminum co of america | beam structural | RFQ |
| AMS QQA200 11 | society of automotive engineers inc | beam structural | RFQ |
| QQA200 11 | federal specifications promulgat | beam structural | RFQ |
| AMS-QQA200-11 | sae international | beam structural | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.875 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.064 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | Z SHAPE |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.064 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXN | WEB FLANGE THICKNESS | 0.064 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 0.750 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 0.938 INCHES NOMINAL |
| BQKQ | OUTER RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE | 0.125 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.310 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | FLANGE LEFT DOWNWARD W/ SQUARE END AND INNER AND OUTER CORNER RADII |
| CNNN | FIRST TIP INNER CORNER RADIUS | 0.125 INCHES NOMINAL |
| CNNP | SECOND TIP INNER CORNER RADIUS | 0.125 INCHES NOMINAL |
| CNNS | FIRST TIP OUTER CORNER RADIUS | 0.125 INCHES NOMINAL |
| CNPS | FIRST TIP THICKNESS | 0.064 INCHES NOMINAL |
| CNPT | SECOND TIP THICKNESS | 0.064 INCHES NOMINAL |
| CNPY | FIRST TIP FLANGE HEIGHT | 0.250 INCHES NOMINAL |
| CNPZ | SECOND TIP FLANGE HEIGHT | 0.189 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| CNQK | SECOND TIP STYLE | FLANGE RIGHT UPWARD WITH SQUARE END, INNER CORNER RADIUS, AND SQUARE OUTER CORNER |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CWKK | RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
| Relevant Components for NSN - 9540-00-595-8597, 9540005958597 | ||||
| 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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