| 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) | 01-048-6212 (010486212) |
| NCB Code | USA (01) |
| Manufacturer | Transtar Metals Corp, Sae International, Military Standards Corp, Lockheed Martin Corporation, Society Of Automotive Engineers Inc, Federal Specifications |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| PA20481 | transtar metals corp | beam structural | 06012 | RFQ |
| AMS QQ A 200 11 | sae international | beam structural | 0u583 | RFQ |
| MS14373E007 | military standards corp | beam structural | 96906 | RFQ |
| LS4299 | lockheed martin corporation | beam structural | 98897 | RFQ |
| AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | 81343 | RFQ |
| QQ-A-200/11 | federal specifications | beam structural | 81348 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.825 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.375 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.375 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.250 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.225 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.275 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 | 2.500 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 1.865 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBD | FIRST TIP INNER RADIUS | 0.032 INCHES NOMINAL |
| CNBJ | FIRST TIP OUTER RADIUS | 0.032 INCHES NOMINAL |
| 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-6 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11,ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
| Relevant Components for NSN - 9540-01-048-6212, 9540010486212 | ||||
| 9535-00-225-6717 (9535002256717) | 9540-01-009-7327 (9540010097327) | 9520-00-961-8960 (9520009618960) | 9510-00-226-4458 (9510002264458) | |
| 9540-01-037-7606 (9540010377606) | 9505-00-963-5236 (9505009635236) | 9530-00-060-4869 (9530000604869) | 9540-01-446-7172 (9540014467172) | |
| 9540-01-593-6916 (9540015936916) | 9520-01-613-3613 (9520016133613) | 9510-00-528-7541 (9510005287541) | 9535-00-950-5251 (9535009505251) | |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
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