Alternative NSN: 9540-00-227-8940 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 002278940 |
NCB Code: USA (00) |
Manufacturers: International Light Metals Corp , Transtar Metals Corp , Sae International , Society Of Automotive Engineers Inc , The Boeing Company , Aluminum Co Of America , Tracor Flight Systems Inc , General Dynamics Corporation , Hiller Aircraft Corporation , Reynolds Metals Co , Federal Specifications |
Veritable Aviation, owned and operated by ASAP Semiconductor, makes the parts procurement process for NSN 9540-00-227-8940 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 13797-3, 15575, 60-699, AMS-QQ-A-200 3 or NSN 9540-00-227-8940 and receive a quote within fifteen minutes or less from one of our dedicated account managers. We work with well-known industry names International Light Metals Corp, Transtar Metals Corp, Sae International, Society Of Automotive Engineers Inc.
We are dedicated to providing only the best products under NSN 9540-00-227-8940 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 |
---|---|---|---|---|
13797-3 | International Light Metals Corp | beam structural | Avl | RFQ |
15575 | International Light Metals Corp | beam structural | Avl | RFQ |
60-699 | Transtar Metals Corp | 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 |
BAC1505-18722 | The Boeing Company | beam structural | Avl | RFQ |
DIE3660 | Aluminum Co Of America | beam structural | Avl | RFQ |
E711113 | Tracor Flight Systems Inc | beam structural | Avl | RFQ |
E711113 | General Dynamics Corporation | beam structural | Avl | RFQ |
FS50102-1510-1 | Hiller Aircraft Corporation | beam structural | Avl | RFQ |
P4077 | Reynolds Metals Co | beam structural | Avl | RFQ |
PA6570 | Transtar Metals Corp | 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 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.093 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.093 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJB | FIRST TIP RADIUS | 0.046 INCHES NOMINAL |
AJJP | LEG THICKNESS | 0.093 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 1.500 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.270 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | FULL RADIUS |
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 | T3511 TEMPER |
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