At NSN Unlimited, we maintain a large database of parts 10872, AMS-QQ-A-200 11, QQA200-11, S1544600 with NSN 9540-00-881-3897 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Alcoa Reynolds Metals Company, Federal Specifications, Society Of Automotive Engineers Inc, Sae International, Boeing Company The. 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: 9540-00-881-3897 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 008813897 |
| NCB Code: USA (00) |
| Manufacturers: Alcoa Reynolds Metals Company , Federal Specifications , Society Of Automotive Engineers Inc , Sae International , Boeing Company The |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 10872 | 9540-00-881-3897 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| 10872 | 9540-00-881-3897 | beam structural | federal specifications | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-00-881-3897 | beam structural | federal specifications | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-00-881-3897 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-00-881-3897 | beam structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-00-881-3897 | beam structural | boeing company the | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-00-881-3897 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| QQA200-11 | 9540-00-881-3897 | beam structural | alcoa reynolds metals company | Avl | RFQ |
| QQA200-11 | 9540-00-881-3897 | beam structural | boeing company the | Avl | RFQ |
| QQA200-11 | 9540-00-881-3897 | beam structural | federal specifications | Avl | RFQ |
| S1544600 | 9540-00-881-3897 | beam structural | federal specifications | Avl | RFQ |
| S1544600 | 9540-00-881-3897 | beam structural | boeing company the | Avl | RFQ |
| S1544600 | 9540-00-881-3897 | beam structural | alcoa reynolds metals company | 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 | 0.125 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJB | FIRST TIP RADIUS | 0.062 INCHES NOMINAL |
| 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 | 0.125 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 |
| BQKL | OUTER FACE TOP FLANGE LEFT END CORNER RADIUS | 16.000 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.440 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 |
| 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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