The NSN 9540-01-329-4391 part numbers such as QQ-A-200 3, LS043-0446, AMS-QQ-A-200 3, AMS QQ A 200 3, 60 6679 manufactured by Federal Specifications, Boeing Company The, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp are available in RFQ Experts’ inventory. An ASAP Semiconductor owned and operated website, RFQ Experts has over six billion parts in its inventory for NSN 9540-01-329-4391. ASAP is committed to streamlining the parts procurement process for our customers, making it easy for them to search through billions of parts to find exactly what they are looking for. We have dedicated account managers ready to solve procurement issues our clients face, whether it’s a need for obsolete parts, or an aircraft on ground situation. As an AS9120B, ISO 9001:2015, and FAA AC 0056B certified company, each and every part that we ship goes through numerous quality checks and inspections, to ensure that we sell only the highest-quality parts.
| Alternative NSN: 9540-01-329-4391 |
| Item Name: Beam Structural |
| Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
| NIIN: 013294391 |
| NCB Code: USA (01) |
| Manufacturers: Federal Specifications, Boeing Company The, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp |
| Federal Specifications | Boeing Company The | Sae International |
| Society Of Automotive Engineer.. | Transtar Metals Corp |
| Part No | NSN | Item Name | QTY | RFQ |
|---|---|---|---|---|
| QQ-A-200 3 | 9540-01-329-4391 | beam structural | Avl | RFQ |
| LS043-0446 | 9540-01-329-4391 | beam structural | Avl | RFQ |
| AMS-QQ-A-200 3 | 9540-01-329-4391 | beam structural | Avl | RFQ |
| AMS QQ A 200 3 | 9540-01-329-4391 | beam structural | Avl | RFQ |
| 60 6679 | 9540-01-329-4391 | beam structural | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | B-1B AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.125 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 | 4.100 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.919 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-81 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
| ABKW | OVERALL HEIGHT | 2.100 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.050 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.050 INCHES NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T81 TEMPER |
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