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 1MA160D05-10322, QQ-A-200/11, 89615-2350, AMS-QQ-A-200 11, PA1382 under NSN 9540-01-189-8617 of Beam Structural manufactured by Boeing Company The, Federal Specifications, Litton Industries Inc, Society Of Automotive Engineers Inc, Transtar Metals Corp.
Federal Supply Class of NSN 9540-01-189-8617 is FSC 9540 contains part details of Structural Shapes Nonferrous Base Metal. Quote for your desired part numbers.
| Item Name | Beam Structural |
| INC Code | 37018 |
| Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC) | 9540 Structural Shapes Nonferrous Base Metal |
| National Item Identification Number (NIIN) | 01-189-8617 (011898617) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The, Federal Specifications, Litton Industries Inc, Society Of Automotive Engineers Inc, Transtar Metals Corp, Alcoa Reynolds Metals Company, Sae International, Sterling Tool Inc |
| Associated Parts Numbers of NSN 9540-01-189-8617 | ||||||
|---|---|---|---|---|---|---|
| Part Number | Manufacturer | Item Name | Cage Code | Type | Status | RFQ |
| 1MA160D05-10322 | boeing company the | beam structural | 76301 | A | A | RFQ |
| QQ-A-200/11 | federal specifications | beam structural | 81348 | A | A | RFQ |
| 89615-2350 | litton industries inc | beam structural | 50200 | A | H | RFQ |
| AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | 81343 | A | R | RFQ |
| PA1382 | transtar metals corp | beam structural | 06012 | F | F | RFQ |
| 16102 | alcoa reynolds metals company | beam structural | 77783 | A | A | RFQ |
| AMS QQ A 200 11 | sae international | beam structural | 0u583 | C | A | RFQ |
| 60-339 | transtar metals corp | beam structural | 29321 | A | A | RFQ |
| 51066 | sterling tool inc | beam structural | 26510 | A | F | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.750 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.125 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.734 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.734 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 | 3.625 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.804 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBD | FIRST TIP INNER RADIUS | 0.031 INCHES NOMINAL |
| CNBJ | FIRST TIP OUTER RADIUS | 0.031 INCHES NOMINAL |
| 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 | T-73511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11,ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T73511 TEMPER |
| Relevant Components for NSN - 9540-01-189-8617, 9540011898617 | ||||
| 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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