| Alternative NSN: 9540-00-720-1332 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 007201332 |
| NCB Code: USA (00) |
| Manufacturers: Transtar Metals Corp , Bohn Aluminum And Brass Co , Reynolds Metals Co , Society Of Automotive Engineers Inc , Sae International , American Society For Testing And , Federal Specifications , Boeing Company The |
Veritable Aviation, owned and operated by ASAP Semiconductor, makes the parts procurement process for NSN 9540-00-720-1332 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 10136-2401, 40196, 8726, AMS 10136-2401 or NSN 9540-00-720-1332 and receive a quote within fifteen minutes or less from one of our dedicated account managers. We work with well-known industry names Transtar Metals Corp, Bohn Aluminum And Brass Co, Reynolds Metals Co, Society Of Automotive Engineers Inc, Sae International.
We are dedicated to providing only the best products under NSN 9540-00-720-1332 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 |
|---|---|---|---|---|
| 10136-2401 | Transtar Metals Corp | beam structural | Avl | RFQ |
| 40196 | Bohn Aluminum And Brass Co | beam structural | Avl | RFQ |
| 8726 | Reynolds Metals Co | beam structural | Avl | RFQ |
| AMS 10136-2401 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
| AMS 10136-2401 | Sae International | 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 |
| ASTM B221 | American Society For Testing And | beam structural | Avl | RFQ |
| QQ-A-200 11 | Federal Specifications | beam structural | Avl | RFQ |
| S1245835 | Boeing Company The | beam structural | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.250 INCHES NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJB | FIRST TIP RADIUS | 0.094 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.094 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 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 | 2.500 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.420 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CNBB | THIRD TIP RADIUS | 0.047 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQM | THIRD TIP STYLE | FULL RADIUS |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | O TEMPER |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
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