Alternative NSN: 9540-00-188-6276 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 001886276 |
NCB Code: USA (00) |
Manufacturers: Reynolds Metals Co , Sae International , Society Of Automotive Engineers Inc , American Society For Testing And , The Boeing Company , Triumph Aerostructures Llc , Aluminum Co Of America , Tracor Flight Systems Inc , General Dynamics Corporation , Federal Specifications |
Veritable Aviation, owned and operated by ASAP Semiconductor, makes the parts procurement process for NSN 9540-00-188-6276 as streamlined as possible. Our easy to use search engine opens up our 6-billion-part inventory open to our loyal customers. Simply type in a part number such as 5940, AMS-QQ-A-200 3, ASTM B221, BAC1505-28902 or NSN 9540-00-188-6276 and receive a quote within fifteen minutes or less from one of our dedicated account managers. We work with well-known industry names Reynolds Metals Co, Sae International, Society Of Automotive Engineers Inc, American Society For Testing And, The Boeing Company.
We are dedicated to providing only the best products under NSN 9540-00-188-6276 through our quality assurance practices, earning us our FAA-AC 0056B accreditation and ISO 9001:2015 certification. To get your parts procurement process started, fill out the request for quote form below.
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
5940 | Reynolds Metals Co | beam structural | Avl | RFQ |
AMS-QQ-A-200 3 | Sae International | beam structural | Avl | RFQ |
AMS-QQ-A-200 3 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
ASTM B221 | American Society For Testing And | beam structural | Avl | RFQ |
BAC1505-28902 | The Boeing Company | beam structural | Avl | RFQ |
CVC2134 | Triumph Aerostructures Llc | beam structural | Avl | RFQ |
DIE13891 | Aluminum Co Of America | beam structural | Avl | RFQ |
E711219 | Tracor Flight Systems Inc | beam structural | Avl | RFQ |
E711219 | General Dynamics Corporation | beam structural | Avl | RFQ |
QQ-A-200 3 | Federal Specifications | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.000 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 20.000 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 | 1.000 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.000 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.320 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | SQUARE END |
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-3511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T3511 TEMPER |
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