The NSN 9540-01-429-3717 part numbers such as QQ A 200 11, CVC10010-113CA, AMS-QQ-A-200 11, AMS QQ A 200 11 manufactured by Federal Specifications, Triumph Aerostructures Llc, Society Of Automotive Engineers Inc, Sae International 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 9540-01-429-3717. 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: 9540-01-429-3717 |
| Item Name: Beam Structural |
| Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
| NIIN: 014293717 |
| NCB Code: USA (01) |
| Manufacturers: Federal Specifications, Triumph Aerostructures Llc, Society Of Automotive Engineers Inc, Sae International |
| Federal Specifications | Triumph Aerostructures Llc | Society Of Automotive Engineer.. |
| Sae International |
| Part No | NSN | Item Name | QTY | RFQ |
|---|---|---|---|---|
| QQ A 200 11 | 9540-01-429-3717 | beam structural | Avl | RFQ |
| CVC10010-113CA | 9540-01-429-3717 | beam structural | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-429-3717 | beam structural | Avl | RFQ |
| AMS QQ A 200 11 | 9540-01-429-3717 | beam structural | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.760 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.113 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.113 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | B-2 BOMBER |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.113 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.745 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.745 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.120 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.120 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 5.490 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBD | FIRST TIP INNER RADIUS | 0.020 INCHES NOMINAL |
| CNBJ | FIRST TIP OUTER RADIUS | 0.020 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 | O-ANNEALED |
| MATT | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER 0 |
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