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) | 01-156-5484 (011565484) |
| NCB Code | USA (01) |
| Manufacturer | Alcoa Reynolds Metals Company, Federal Specifications, Transtar Metals Corp, Society Of Automotive Engineers Inc, Sae International, Boeing Company The |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 21394 | alcoa reynolds metals company | beam structural | RFQ |
| QQ-A-200/13 | federal specifications | beam structural | RFQ |
| PA20519 | transtar metals corp | beam structural | RFQ |
| AMS QQ A 200 13 | society of automotive engineers inc | beam structural | RFQ |
| 60.8893 | transtar metals corp | beam structural | RFQ |
| AMS-QQ-A-200 13 | sae international | beam structural | RFQ |
| 1M57238 | boeing company the | beam structural | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.370 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.090 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.090 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 | 1.460 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.620 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 25.000 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 3.080 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.564 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 | 35.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 145.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/13,ALLOY 7178 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6511 TEMPER |
| Relevant Components for NSN - 9540-01-156-5484, 9540011565484 | ||||
| 9520-01-538-3805 (9520015383805) | 9530-00-247-5514 (9530002475514) | 9535-01-380-4829 (9535013804829) | 9530-01-496-8011 (9530014968011) | |
| 9540-01-428-9530 (9540014289530) | 9540-00-403-5155 (9540004035155) | 9515-01-614-8950 (9515016148950) | 9515-01-465-0340 (9515014650340) | |
| 9520-01-104-1132 (9520011041132) | 9530-00-596-9061 (9530005969061) | 9540-00-595-8549 (9540005958549) | 9530-00-236-0363 (9530002360363) | |
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.
Request for Quote