| 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) | 01-437-2670 (014372670) |
| NCB Code | USA (01) |
| Manufacturer | Sae International, Society Of Automotive Engineers Inc, Triumph Aerostructures Llc, Federal Specifications |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| AMS QQ A 200 11 | sae international | beam structural | 0u583 | RFQ |
| AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | 81343 | RFQ |
| CVC10010-106CA | triumph aerostructures llc | beam structural | 80378 | RFQ |
| QQ-A-200/11 | federal specifications | beam structural | 81348 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.200 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.078 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.078 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.078 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.400 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.400 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.130 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.130 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.800 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBD | FIRST TIP INNER RADIUS | 0.030 INCHES NOMINAL |
| CNBJ | FIRST TIP OUTER RADIUS | 0.030 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 | 0-ANNEALED |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER 0 |
| Relevant Components for NSN - 9540-01-437-2670, 9540014372670 | ||||
| 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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