| 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) | 00-508-8873 (005088873) |
| NCB Code | USA (00) |
| Manufacturer | Federal Specifications, Boeing Company The, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| QQA200-11 | federal specifications | beam structural | 81348 | RFQ |
| 1MA160D03-10270 | boeing company the | beam structural | 76301 | RFQ |
| AMS-QQA200-11 | sae international | beam structural | 0u583 | RFQ |
| AMS QQA200 11 | society of automotive engineers inc | beam structural | 81343 | RFQ |
| PA28044 | transtar metals corp | beam structural | 06012 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.350 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.060 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.060 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.080 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.160 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.840 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 | 3.000 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.340 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| 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-6511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6511 TEMPER |
| Relevant Components for NSN - 9540-00-508-8873, 9540005088873 | ||||
| 9510-00-090-9954 (9510000909954) | 9540-01-597-5789 (9540015975789) | 9510-00-596-2247 (9510005962247) | 9530-00-060-5570 (9530000605570) | |
| 9510-00-596-2035 (9510005962035) | 9520-01-691-2390 (9520016912390) | 9520-00-596-1852 (9520005961852) | 9535-01-136-6202 (9535011366202) | |
| 9525-01-209-8204 (9525012098204) | 9510-01-435-1773 (9510014351773) | 9535-00-167-2131 (9535001672131) | 9535-01-517-5207 (9535015175207) | |
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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