At NSN Unlimited, we maintain a large database of parts 14743, 16885, 31660, 35299, 60-894 with NSN 9540-00-148-4364 used in civil and defense applications for the aerospace, marine, and commercial manufactured by International Light Metals Corp, Aluminum Co Of America, Alcoa Reynolds Metals Company, Cessna Aircraft Company, Transtar Metals Corp. Utilize our interface to browse items by part number, part type, manufacturer, and more. Obtain insights on top MRO and FBO services, Manufacturer profiles, and part catalogs.
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| Alternative NSN: 9540-00-148-4364 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 001484364 |
| NCB Code: USA (00) |
| Manufacturers: International Light Metals Corp , Aluminum Co Of America , Alcoa Reynolds Metals Company , Cessna Aircraft Company , Transtar Metals Corp , Sae International , Society Of Automotive Engineers Inc , The Boeing Company , Bae Systems Technology Solutions And Services Inc Dba Bae Systems Information And , General Dynamics Corporation , Tracor Flight Systems Inc , Federal Specifications |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 14743 | 9540-00-148-4364 | beam structural | international light metals corp | Avl | RFQ |
| 16885 | 9540-00-148-4364 | beam structural | aluminum co of america | Avl | RFQ |
| 31660 | 9540-00-148-4364 | beam structural | aluminum co of america | Avl | RFQ |
| 31660 | 9540-00-148-4364 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| 31660 | 9540-00-148-4364 | beam structural | cessna aircraft company | Avl | RFQ |
| 35299 | 9540-00-148-4364 | beam structural | cessna aircraft company | Avl | RFQ |
| 35299 | 9540-00-148-4364 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| 35299 | 9540-00-148-4364 | beam structural | aluminum co of america | Avl | RFQ |
| 60-894 | 9540-00-148-4364 | beam structural | transtar metals corp | Avl | RFQ |
| AMS QQ A 200 3 | 9540-00-148-4364 | beam structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 3 | 9540-00-148-4364 | beam structural | society of automotive engineers inc | Avl | RFQ |
| BAC1505 29063 | 9540-00-148-4364 | beam structural | the boeing company | Avl | RFQ |
| BAC1505-29063 | 9540-00-148-4364 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| BAC1505-29063 | 9540-00-148-4364 | beam structural | aluminum co of america | Avl | RFQ |
| BAC1505-29063 | 9540-00-148-4364 | beam structural | cessna aircraft company | Avl | RFQ |
| E711208 | 9540-00-148-4364 | beam structural | bae systems technology solutions and services inc dba bae systems information and | Avl | RFQ |
| E711208 | 9540-00-148-4364 | beam structural | general dynamics corporation | Avl | RFQ |
| E711208 | 9540-00-148-4364 | beam structural | tracor flight systems inc | Avl | RFQ |
| PA6119 | 9540-00-148-4364 | beam structural | transtar metals corp | Avl | RFQ |
| QQ A 200 3LCCA | 9540-00-148-4364 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 3LCCA | 9540-00-148-4364 | beam structural | cessna aircraft company | Avl | RFQ |
| QQ-A-200 3LCCA | 9540-00-148-4364 | beam structural | aluminum co of america | Avl | RFQ |
| QQ-A-200 3LCCA | 9540-00-148-4364 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| S116 | 9540-00-148-4364 | beam structural | cessna aircraft company | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.500 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.125 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 | 0.156 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.156 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.000 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.520 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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