NSN 9540-01-437-2660 Beam Structural, Angle Structural manufactured by Society Of Automotive Engineers Inc, Triumph Aerostructures Llc, Sae International, Federal Specifications Promulgat, 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, AMS-QQ-A-200 11, CVC10010-106CJ. 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 9540-01-437-2660 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 9540-01-437-2660 part today and allow us to simplify your procurement process.
Alternative NSN: 9540-01-437-2660 |
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: Society Of Automotive Engineers Inc , Triumph Aerostructures Llc , Sae International , Federal Specifications Promulgat , Vought Aircraft Industries Inc |
Society Of Automotive Engineers Inc | Triumph Aerostructures Llc | Sae International |
Federal Specifications Promulgat | Vought Aircraft Industries Inc |
Part No Part No
|
Manufacturer NSN Parts
|
Item Name Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
AMS QQ A 200 11 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
AMS-QQ-A-200 11 | Triumph Aerostructures Llc | beam structural | Avl | RFQ |
AMS-QQ-A-200 11 | Sae International | beam structural | Avl | RFQ |
AMS-QQ-A-200 11 | Federal Specifications Promulgat | angle structural | Avl | RFQ |
CVC10010-106CJ | Federal Specifications Promulgat | beam structural | Avl | RFQ |
CVC10010-106CJ | Triumph Aerostructures Llc | beam structural | Avl | RFQ |
CVC10010-106CJ | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
CVC10010-106CJ | 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 | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
CNBJ | FIRST TIP OUTER RADIUS | 0.030 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 | T-76511 SOLUTION HEAT TREATED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER T76511 |
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 2.200 INCHES NOMINAL |
ABRY | LENGTH | 12.0000 FEET NOMINAL |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.078 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.078 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.078 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.400 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.400 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.130 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.130 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.800 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
CNBD | FIRST TIP INNER RADIUS | 0.030 INCHES NOMINAL |
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