The NSN 9540-01-429-2423 part numbers such as QQ-A-200 11, CVC10011 16CA, AMS-QQ-A-200 11, AMS-QQ-A-200 11 manufactured by Federal Specifications, Triumph Aerostructures Llc, Sae International, Society Of Automotive Engineers Inc 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 9540-01-429-2423. 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: 9540-01-429-2423 |
Item Name: Beam Structural |
Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
NIIN: 014292423 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications, Triumph Aerostructures Llc, Sae International, Society Of Automotive Engineers Inc |
Federal Specifications | Triumph Aerostructures Llc | Sae International |
Society Of Automotive Engineer.. |
Part No | NSN | Item Name | QTY | RFQ |
---|---|---|---|---|
QQ-A-200 11 | 9540-01-429-2423 | beam structural | Avl | RFQ |
CVC10011 16CA | 9540-01-429-2423 | beam structural | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-429-2423 | beam structural | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-429-2423 | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
CNQJ | Second Tip Relationship To First Tip | IDENTICAL |
CSMZ | Left Top Inside Angle | 90.0 DEGREES NOMINAL |
ADXR | Left Side Top Flange Thickness | 0.064 INCHES NOMINAL |
MATT | Material | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
ABRY | Length | 12.000 FEET NOMINAL |
BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 1.100 INCHES NOMINAL |
AGTA | Basic Shape Style | T SHAPE |
HEAT | Heat Treatment | O-ANNEALED |
AJJP | Leg Thickness | 0.064 INCHES NOMINAL |
BPXG | Right Side Top Flange Distance To Center Of Both Flanges | 1.900 INCHES NOMINAL |
ADXS | Right Side Top Flange Thickness | 0.064 INCHES NOMINAL |
BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.090 INCHES NOMINAL |
BQJG | Top Flange Width | 3.000 INCHES NOMINAL |
BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.090 INCHES NOMINAL |
ZZZT | Nondefinitive Spec/Std Data | ALLOY 7075 AND TEMPER 0 |
AGAV | End Item Identification | B-2 BOMBER |
CRZC | Right Top Inside Angle | 90.0 DEGREES NOMINAL |
CMZY | First Tip Style | SQUARE W/ INNER AND OUTER CORNER RADII |
ABKW | Overall Height | 2.650 INCHES NOMINAL |
MRC | Decoded Requirement | Clear Text Reply |
AARN | Fabrication Method | EXTRUDED |
CNBD | First Tip Inner Radius | 0.030 INCHES NOMINAL |
CNQL | Third Tip Relationship To Preceding Tips | IDENTICAL W/FIRST TIP |
CNBJ | First Tip Outer Radius | 0.030 INCHES NOMINAL |
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