| Alternative NSN: 9540-00-294-9938 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 002949938 |
| NCB Code: USA (00) |
| Manufacturers: International Light Metals Corp , General Dynamics Corporation , Tracor Flight Systems Inc , Bae Systems Technology Solutions And Services Inc Dba Bae Systems Information And , Aluminum Co Of America , Sae International , Society Of Automotive Engineers Inc , Federal Specifications |
Veritable Aviation, owned and operated by ASAP Semiconductor, makes the parts procurement process for NSN 9540-00-294-9938 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 15303, 240-8210022, 43070 or NSN 9540-00-294-9938 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, General Dynamics Corporation, Tracor Flight Systems Inc, Bae Systems Technology Solutions And Services Inc Dba Bae Systems Information And, Aluminum Co Of America.
We are dedicated to providing only the best products under NSN 9540-00-294-9938 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 |
|---|---|---|---|---|
| 15303 | International Light Metals Corp | beam structural | Avl | RFQ |
| 240-8210022 | General Dynamics Corporation | beam structural | Avl | RFQ |
| 240-8210022 | Tracor Flight Systems Inc | beam structural | Avl | RFQ |
| 240-8210022 | Bae Systems Technology Solutions And Services Inc Dba Bae Systems Information And | beam structural | Avl | RFQ |
| 43070 | Aluminum Co Of America | beam structural | Avl | RFQ |
| AMS QQ A 200 11 | Sae International | beam structural | Avl | RFQ |
| AMS-QQ-A-200 11 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
| QQ-A-200 11 | Federal Specifications | beam structural | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.750 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.087 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.087 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.087 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.485 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.485 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 | 2.970 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.602 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-6 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
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