NSN 9540-01-437-2658 Beam Structural, Angle Structural manufactured by Triumph Aerostructures Llc, Federal Specifications Promulgat, Society Of Automotive Engineers Inc, Sae International, Vought Aircraft Industries Inc is available within ASAP Part Service’s ready-to-ship inventory. Owned and operated by ASAP Semiconductor, ASAP Part Services has over 6 billion parts within its inventory including AMS-QQ-A-200 11, CVC10010-116CJ. ASAP is committed to streamlining the parts procurement process for our customers. We make it easy for our customers to search through billions of parts to find the exact part they are looking for.
A dedicated ASAP account manager is ready to help solve any procurement issues or needs that a customer may have. As a company we are quick and responsive meaning we can deliver a part within an AOG timeframe. Quality control is at the center of all that we do. Each and every NSN 9540-01-437-2658 part is subject to numerous quality checks that are designed to screen out any part imperfections or validity issues. Subject a request for quote for NSN 9540-01-437-2658 part today and allow us to simplify your procurement process.
Alternative NSN: 9540-01-437-2658 |
Item Name:Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NCB Code: USA (01) |
Manufacturers: Triumph Aerostructures Llc , Federal Specifications Promulgat , Society Of Automotive Engineers Inc , Sae International , Vought Aircraft Industries Inc |
Triumph Aerostructures Llc | Federal Specifications Promulgat | Society Of Automotive Engineers Inc |
Sae International | Vought Aircraft Industries Inc |
Part No Part No
|
Manufacturer NSN Parts
|
Item Name Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
AMS-QQ-A-200 11 | Triumph Aerostructures Llc | beam structural | Avl | RFQ |
AMS-QQ-A-200 11 | Federal Specifications Promulgat | angle structural | Avl | RFQ |
AMS-QQ-A-200 11 | Society Of Automotive Engineers Inc | angle structural | Avl | RFQ |
AMS-QQ-A-200 11 | Sae International | angle structural | Avl | RFQ |
CVC10010-116CJ | Federal Specifications Promulgat | beam structural | Avl | RFQ |
CVC10010-116CJ | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
CVC10010-116CJ | Triumph Aerostructures Llc | beam structural | Avl | RFQ |
CVC10010-116CJ | Vought Aircraft Industries Inc | beam structural | Avl | RFQ |
QQ-A-200 11 | Triumph Aerostructures Llc | beam structural | Avl | RFQ |
QQ-A-200 11 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
QQ-A-200 11 | Federal Specifications Promulgat | angle 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 |
ADXR | Left Side Top Flange Thickness | 0.063 INCHES NOMINAL |
HEAT | Heat Treatment | T-76511 SOLUTION HEAT TREATED |
ZZZT | Nondefinitive Spec/Std Data | ALLOY 7075 AND TEMPER T76511 |
ABRY | Length | 12.000 FEET NOMINAL |
ABKW | Overall Height | 0.880 INCHES NOMINAL |
BPXG | Right Side Top Flange Distance To Center Of Both Flanges | 1.580 INCHES NOMINAL |
AGTA | Basic Shape Style | T SHAPE |
AJJP | Leg Thickness | 0.063 INCHES NOMINAL |
CRZC | Right Top Inside Angle | 90.0 DEGREES NOMINAL |
BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 1.580 INCHES NOMINAL |
BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.063 INCHES NOMINAL |
ADXS | Right Side Top Flange Thickness | 0.063 INCHES NOMINAL |
BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.063 INCHES NOMINAL |
BQJG | Top Flange Width | 3.160 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 |
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