| 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) | 00-580-6525 (005806525) |
| NCB Code | USA (00) |
| Manufacturer | Airforce-Navy Aeronautical Design Standard, Boeing Company The, Bohn Aluminum And Brass Co, Nsk Corp, Federal Specifications, Reynolds Metals Co, Society Of Automotive Engineers Inc |
| Associated Parts Numbers of NSN 9540-00-580-6525 | ||||||
|---|---|---|---|---|---|---|
| Part Number | Manufacturer | Item Name | Cage Code | Type | Status | RFQ |
| AND10133-2402 | airforce-navy aeronautical design standard | beam structural | 99237 | NSN | Avl | RFQ |
| AND10136-1505 | airforce-navy aeronautical design standard | beam structural | 99237 | NSN | Avl | RFQ |
| 1298026 | boeing company the | beam structural | 88277 | A | A | RFQ |
| 40346 | bohn aluminum and brass co | beam structural | 99267 | A | F | RFQ |
| HT172 | nsk corp | beam structural | 10383 | A | A | RFQ |
| QQ-A-200/11 | federal specifications | beam structural | 81348 | A | A | RFQ |
| 10233 | reynolds metals co | beam structural | 01484 | A | H | RFQ |
| AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | 81343 | A | R | RFQ |
| AMS10136 1505 | society of automotive engineers inc | beam structural | 81343 | A | R | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.375 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJB | FIRST TIP RADIUS | 0.094 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.094 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.812 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.813 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 1.625 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.330 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CNBB | THIRD TIP RADIUS | 0.047 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
| CNQM | THIRD TIP STYLE | FULL RADIUS |
| 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 |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
| Relevant Components for NSN - 9540-00-580-6525, 9540005806525 | ||||
| 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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