AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
| 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) | 00-227-8940 (002278940) |
| NCB Code | USA (00) |
| Manufacturer | General Dynamics Corporation, Society Of Automotive Engineers Inc, Tracor Flight Systems Inc, Transtar Metals Corp, Sae International, Lockheed Martin Corporation, Reynolds Metals Co, Federal Specifications, Hiller Aircraft Corporation, Aluminum Co Of America, International Light Metals Corp, The Boeing Company, Hughes Missile Systems Co |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| E711113 | general dynamics corporation | beam structural | RFQ |
| AMS-QQ-A-200 3 | society of automotive engineers inc | beam structural | RFQ |
| E711113 | tracor flight systems inc | beam structural | RFQ |
| PA6570 | transtar metals corp | beam structural | RFQ |
| AMS-QQ-A-200 3 | sae international | beam structural | RFQ |
| LS3217 | lockheed martin corporation | beam structural | RFQ |
| P4077 | reynolds metals co | beam structural | RFQ |
| QQ-A-200/3 | federal specifications | beam structural | RFQ |
| FS50102-1510-1 | hiller aircraft corporation | beam structural | RFQ |
| DIE3660 | aluminum co of america | beam structural | RFQ |
| 13797-3 | international light metals corp | beam structural | RFQ |
| 60-699 | transtar metals corp | beam structural | RFQ |
| BAC1505-18722 | the boeing company | beam structural | RFQ |
| 15575 | international light metals corp | beam structural | RFQ |
| E711113 | hughes missile systems co | beam structural | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.000 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.093 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.093 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJB | FIRST TIP RADIUS | 0.046 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.093 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 | 0.270 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | FULL RADIUS |
| 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-3511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3,ALLOY 2024 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T3511 TEMPER |
| Relevant Components for NSN - 9540-00-227-8940, 9540002278940 | ||||
| 9510-00-224-1673 (9510002241673) | 9505-00-541-9654 (9505005419654) | 9540-01-353-5127 (9540013535127) | 9515-66-151-1706 (9515661511706) | |
| 9515-00-153-3357 (9515001533357) | 9535-01-012-2441 (9535010122441) | 9520-01-694-5689 (9520016945689) | 9510-01-484-4625 (9510014844625) | |
| 9530-00-993-4137 (9530009934137) | 9515-00-153-3227 (9515001533227) | 9515-01-555-3938 (9515015553938) | 9530-00-060-5594 (9530000605594) | |
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