| 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) | 01-616-7168 (016167168) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABKW | Overall Height | 1.250 INCHES NOMINAL |
| ADXR | Left Side Top Flange Thickness | 0.094 INCHES NOMINAL |
| MATT | Material | ALUMINUM ALLOY 2024 |
| ADXS | Right Side Top Flange Thickness | 0.094 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 |
| FEAT | Special Features | TEMPER T3511 |
| BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.125 INCHES NOMINAL |
| BQJG | Top Flange Width | 2.000 INCHES NOMINAL |
| BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.125 INCHES NOMINAL |
| MRC | Decoded Requirement | Clear Text Reply |
| AGAV | End Item Identification | C-17A AIRCRAFT |
| Relevant Components for NSN - 9540-01-616-7168, 9540016167168 | ||||
| 9505-00-186-9153 (9505001869153) | 9515-01-483-6843 (9515014836843) | 9535-01-255-1244 (9535012551244) | 9540-01-428-2775 (9540014282775) | |
| 9510-00-234-7945 (9510002347945) | 9510-01-362-4558 (9510013624558) | 9515-01-306-1647 (9515013061647) | 9535-00-079-1825 (9535000791825) | |
| 9515-00-913-8009 (9515009138009) | 9540-00-027-7489 (9540000277489) | 9540-01-071-1355 (9540010711355) | 9505-00-950-3671 (9505009503671) | |
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