| 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) | 00-720-4243 (007204243) |
| NCB Code | USA (00) |
| Manufacturer | Alcoa Reynolds Metals Company, Federal Specifications, International Light Metals Corp, Sae International, Sikorsky Aircraft Corporation, Transtar Metals Corp, Society Of Automotive Engineers Inc |
| Associated Parts Numbers of NSN 9540-00-720-4243 | ||||||
|---|---|---|---|---|---|---|
| Part Number | Manufacturer | Item Name | Cage Code | Type | Status | RFQ |
| 22562 | alcoa reynolds metals company | beam structural | 77783 | A | A | RFQ |
| QQ-A-200/11 | federal specifications | beam structural | 81348 | A | A | RFQ |
| 65687 | international light metals corp | beam structural | 27610 | A | F | RFQ |
| AMS QQ A 200 11 | sae international | beam structural | 0u583 | C | A | RFQ |
| S6105-2136 | sikorsky aircraft corporation | beam structural | 78286 | A | A | RFQ |
| PA6338 | transtar metals corp | beam structural | 06012 | F | F | RFQ |
| 60 12667 | transtar metals corp | beam structural | 29321 | A | A | RFQ |
| AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | 81343 | A | R | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABKW | OVERALL HEIGHT | 1.000 INCHES NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.050 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.050 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 | 0.062 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 1.500 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.160 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| AARN | FABRICATION METHOD | EXTRUDED |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.062 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-6 SOLUTION HEAT TREATED |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
| Relevant Components for NSN - 9540-00-720-4243, 9540007204243 | ||||
| 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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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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