NSN 9540-01-429-3717, 9540014293717 Beam Structural Parts Sourcing
If you have been looking for Society Of Automotive Engineers Inc, Federal Specifications, Triumph Aerostructures Llc, Sae International parts listed alongside the NSN 9540014293717, ASAP Distribution has you covered with our unmatched inventory of items Beam Structural. With over 2 billion parts readily available for purchase on our website, customers can get competitive pricing offers and rapid lead-times on top NSN part numbers such as AMS-QQ-A-200 11, QQ-A-200 11, CVC10010-113CA. Explore our NSN parts catalog at your leisure, or you may take advantage of our provided search engine to find specific parts in a matter of moments. If you are interested in this particular component or others listed across our website, you may begin the procurement process at any time through the submission of an Instant RFQ form. Using the information that you submit to us, our team of industry experts will quickly craft you a quote that accommodates your individual needs and requirements for NSN 9540014293717.
| Alternative NSN: 9540-01-429-3717 | Item Name : Beam Structural | FSG : 95 Metal Bars Sheets and Shapes | Federal Supply Class (FSC) : 9540 Structural Shapes Nonferrous Base Metal | NIIN: 014293717 | NCB Code: USA (01) |
Part Number's List for NSN 9540-01-429-3717, 9540014293717
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| AMS-QQ-A-200 11 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
| QQ-A-200 11 | Federal Specifications | beam structural | Avl | RFQ |
| CVC10010-113CA | Triumph Aerostructures Llc | beam structural | Avl | RFQ |
| AMS-QQ-A-200 11 | Sae International | beam structural | Avl | RFQ |
Characteristics Data of NSN 9540014293717
| MRC | Criteria | Characteristic |
|---|---|---|
| AJJP | LEG THICKNESS | 0.113 INCHES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
| 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 |
| AGAV | III END ITEM IDENTIFICATION | B-2 BOMBER |
| 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 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER 0 |
| CNBJ | FIRST TIP OUTER RADIUS | 0.020 INCHES NOMINAL |
| 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 |
| ABKW | OVERALL HEIGHT | 1.760 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.745 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.113 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.113 INCHES NOMINAL |
| AARN | FABRICATION METHOD | EXTRUDED |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
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