| Item Name | Beam Structural |
| INC Code | 37018 |
| Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC) | 9540 Structural Shapes Nonferrous Metal |
| National Item Identification Number (NIIN) | 01-071-2142 (010712142) |
| NCB Code | USA (01) |
| Manufacturer | Alcoa Reynolds Metals Company, Aluminum Co Of America, Federal Specifications, International Light Metals Corp, Lockheed Martin Corporation, Military Standards Corp, Pimalco Inc, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp |
| Associated Parts Numbers of NSN 9540-01-071-2142 | ||||||
|---|---|---|---|---|---|---|
| Part Number | Manufacturer | Item Name | Cage Code | Type | Status | RFQ |
| 5614 | alcoa reynolds metals company | beam structural | 77783 | A | A | RFQ |
| 32548 | aluminum co of america | beam structural | 01634 | A | Y | RFQ |
| QQ-A-200/3 | federal specifications | beam structural | 81348 | A | A | RFQ |
| 14733 | international light metals corp | beam structural | 27610 | A | F | RFQ |
| K40A109O | lockheed martin corporation | beam structural | 81755 | A | A | RFQ |
| MS14375E161 | military standards corp | beam structural | 96906 | NSN | Avl | RFQ |
| 11008-A | pimalco inc | beam structural | 55088 | A | A | RFQ |
| AMS-QQ-A-200 3 | sae international | beam structural | 0u583 | C | A | RFQ |
| AMS QQ A 200 3 | society of automotive engineers inc | beam structural | 81343 | A | R | RFQ |
| 60-11639 | transtar metals corp | beam structural | 29321 | A | A | RFQ |
| PA6345 | transtar metals corp | beam structural | 06012 | F | F | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.530 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 | 2.000 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.000 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.190 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.190 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 4.000 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.790 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 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| ZZZK | SPECIFICATION/STANDARD DATA | 81755-K40 MANUFACTURERS STANDARD |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | O TEMPER |
| Relevant Components for NSN - 9540-01-071-2142, 9540010712142 | ||||
| 9540-01-419-5436 (9540014195436) | 9540-00-355-9508 (9540003559508) | 9540-00-540-5696 (9540005405696) | 9540-01-247-2816 (9540012472816) | |
| 9540-01-316-8247 (9540013168247) | 9540-00-145-8447 (9540001458447) | 9540-01-070-2164 (9540010702164) | 9540-01-276-0089 (9540012760089) | |
| 9540-01-496-2506 (9540014962506) | 9540-00-145-5802 (9540001455802) | 9540-01-276-0956 (9540012760956) | 9540-00-005-6284 (9540000056284) | |
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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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