The NSN 9540-01-437-2661 part numbers such as QQ A 200 11, CVC10010-129CA, 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 9540-01-437-2661. 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: 9540-01-437-2661 |
| Item Name: Beam Structural |
| Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
| NIIN: 014372661 |
| 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 | 9540-01-437-2661 | beam structural | Avl | RFQ |
| CVC10010-129CA | 9540-01-437-2661 | beam structural | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-437-2661 | beam structural | Avl | RFQ |
| AMS QQ A 200 11 | 9540-01-437-2661 | beam structural | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| CNQJ | Second Tip Relationship To First Tip | IDENTICAL |
| CNQL | Third Tip Relationship To Preceding Tips | IDENTICAL W/FIRST TIP |
| MRC | Decoded Requirement | Clear Text Reply |
| MATT | Material | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
| HEAT | Heat Treatment | O-ANNEALED |
| ADXR | Left Side Top Flange Thickness | 0.110 INCHES NOMINAL |
| ZZZT | Nondefinitive Spec/Std Data | ALLOY 7075 AND TEMPER T0 |
| ABRY | Length | 12.000 FEET NOMINAL |
| BPXG | Right Side Top Flange Distance To Center Of Both Flanges | 1.375 INCHES NOMINAL |
| AGTA | Basic Shape Style | T SHAPE |
| ABKW | Overall Height | 1.350 INCHES NOMINAL |
| AJJP | Leg Thickness | 0.110 INCHES NOMINAL |
| CRZC | Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 1.375 INCHES NOMINAL |
| BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.125 INCHES NOMINAL |
| ADXS | Right Side Top Flange Thickness | 0.110 INCHES NOMINAL |
| BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.125 INCHES NOMINAL |
| BQJG | Top Flange Width | 2.750 INCHES NOMINAL |
| CNBD | First Tip Inner Radius | 0.020 INCHES NOMINAL |
| AARN | Fabrication Method | EXTRUDED |
| CSMZ | Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| CMZY | First Tip Style | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBJ | First Tip Outer Radius | 0.020 INCHES NOMINAL |
All Orders are Fulfilled in the U.S.A.
All shipments must comply with U.S.A export laws.
No exceptions.
The only independent distributor
with a NO CHINA SOURCING Pledge
“We Proudly Support Intrepid Fallen Heroes Fund that serves United States Military Personal experiencing the Invisible Wounds of War : Traumatic Brain Injury (TBI) and Post Traumatic Stress (PTS). Please visit website (www.fallenheroesfund.org) and help in their valiant effort”.
You Can Click Here to Get Quote For Your Required Aircraft Parts Within 15 Minutes.
Request for Quote