| Item Name | Beam Structural |
| Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC) | 9540 Structural Shapes Nonferrous Base Metal |
| National Item Identification Number (NIIN) | 01-616-5487 (016165487) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| MRC | Criteria | Characteristic |
|---|---|---|
| ADXR | Left Side Top Flange Thickness | 0.188 INCHES NOMINAL |
| ADXS | Right Side Top Flange Thickness | 0.188 INCHES NOMINAL |
| FEAT | Special Features | TEMPER T3511 |
| ABKW | Overall Height | 2.438 INCHES NOMINAL |
| CXCY | Part Name Assigned By Controlling Agency | BEAM, STRUCTURAL |
| AGTA | Basic Shape Style | T SHAPE |
| MDCL | Material Document And Classification | QQ-A-430, ALLOY 2024 FED SPEC 1ST MATERIAL RESPONSE |
| MRC | Decoded Requirement | Clear Text Reply |
| AJJP | Leg Thickness | 0.250 INCHES NOMINAL |
| BQJG | Top Flange Width | 2.000 INCHES NOMINAL |
| AGAV | End Item Identification | C-17A GLOBEMASTERIII |
| MATT | Material | ALUMINUM ALLOY 2024 |
| Relevant Components for NSN - 9540-01-616-5487, 9540016165487 | ||||
| 9515-01-536-3375 (9515015363375) | 9515-00-814-7221 (9515008147221) | 9530-00-237-0734 (9530002370734) | 9540-00-197-9847 (9540001979847) | |
| 9520-01-274-4554 (9520012744554) | 9515-00-061-4892 (9515000614892) | 9530-01-135-8297 (9530011358297) | 9535-01-581-6877 (9535015816877) | |
| 9510-00-541-9207 (9510005419207) | 9540-01-071-2142 (9540010712142) | 9530-00-060-5585 (9530000605585) | 9530-00-233-1340 (9530002331340) | |
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