| 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) | 00-111-7573 (001117573) |
| NCB Code | USA (00) |
| Manufacturer | Aluminum Co Of America, Bell Helicopter Textron Inc, Federal Specifications, Sae International, Society Of Automotive Engineers Inc |
| Associated Parts Numbers of NSN 9540-00-111-7573 | ||||||
|---|---|---|---|---|---|---|
| Part Number | Manufacturer | Item Name | Cage Code | Type | Status | RFQ |
| 29794 | aluminum co of america | beam structural | 01634 | A | Y | RFQ |
| 40-068-1 | bell helicopter textron inc | beam structural | 97499 | A | A | RFQ |
| QQ-A-200/3 | federal specifications | beam structural | 81348 | 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 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 0.312 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | Z SHAPE |
| AJJB | FIRST TIP RADIUS | 0.062 INCHES NOMINAL |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.031 INCHES NOMINAL |
| BPXN | WEB FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 0.562 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 0.812 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.120 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CWKK | RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T3511 TEMPER |
| Relevant Components for NSN - 9540-00-111-7573, 9540001117573 | ||||
| 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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