NSN 9540-01-363-8532 Beam Structural, Angle Structural manufactured by Boeing Company, Federal Specifications Promulgat, Society Of Automotive Engineers Inc, Transtar Metals Corp, Sae International 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 1MA160D01-10431, 60 14822 7075 O, 60-14822 7075-O. 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 9540-01-363-8532 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 9540-01-363-8532 part today and allow us to simplify your procurement process.
Alternative NSN: 9540-01-363-8532 |
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: Boeing Company , Federal Specifications Promulgat , Society Of Automotive Engineers Inc , Transtar Metals Corp , Sae International |
Boeing Company | Federal Specifications Promulgat | Society Of Automotive Engineers Inc |
Transtar Metals Corp | Sae International |
Part No Part No
|
Manufacturer NSN Parts
|
Item Name Item Name
|
QTY QTY
|
RFQ RFQ
|
---|---|---|---|---|
1MA160D01-10431 | Boeing Company | beam structural | Avl | RFQ |
1MA160D01-10431 | Federal Specifications Promulgat | beam structural | Avl | RFQ |
1MA160D01-10431 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
60 14822 7075 O | Transtar Metals Corp | beam structural | Avl | RFQ |
60-14822 7075-O | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
60-14822 7075-O | Federal Specifications Promulgat | beam structural | Avl | RFQ |
60-14822 7075-O | Boeing Company | 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 |
AMS-QQ-A-200 11 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
AMS-QQ-A-200 11 | Boeing Company | beam structural | Avl | RFQ |
QQ A 200 11 | Federal Specifications Promulgat | beam structural | Avl | RFQ |
QQ-A-200 11 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
QQ-A-200 11 | Boeing Company | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 2.000 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.090 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.090 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.090 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.845 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.607 POUNDS PER LINEAR FOOT |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
MATT | MATERIAL | ALUMINUM ALLOY, AMS-QQ-A-200/11, ALLOY 7075 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND ANNEALED CONDITION |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.855 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 3.700 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | LOWER RADIUS |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | O-ANNEALED |
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