At NSN Unlimited, we maintain a large database of parts 10136-2004 7075-T6511, 1MA160D03-10092, AMS QQ A 200 11, AMS-QQ-A-200 11, QQ A 200 11 with NSN 9540-01-363-8544 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Society Of Automotive Engineers Inc, Boeing Company The, Federal Specifications, Transtar Metals Corp, Sae International. 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: 9540-01-363-8544 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 013638544 |
| NCB Code: USA (01) |
| Manufacturers: Society Of Automotive Engineers Inc , Boeing Company The , Federal Specifications , Transtar Metals Corp , Sae International |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 10136-2004 7075-T6511 | 9540-01-363-8544 | beam structural | society of automotive engineers inc | Avl | RFQ |
| 10136-2004 7075-T6511 | 9540-01-363-8544 | beam structural | boeing company the | Avl | RFQ |
| 10136-2004 7075-T6511 | 9540-01-363-8544 | beam structural | federal specifications | Avl | RFQ |
| 10136-2004 7075-T6511 | 9540-01-363-8544 | beam structural | transtar metals corp | Avl | RFQ |
| 1MA160D03-10092 | 9540-01-363-8544 | beam structural | society of automotive engineers inc | Avl | RFQ |
| 1MA160D03-10092 | 9540-01-363-8544 | beam structural | boeing company the | Avl | RFQ |
| 1MA160D03-10092 | 9540-01-363-8544 | beam structural | federal specifications | Avl | RFQ |
| AMS QQ A 200 11 | 9540-01-363-8544 | beam structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-363-8544 | beam structural | federal specifications | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-363-8544 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-363-8544 | beam structural | boeing company the | Avl | RFQ |
| QQ A 200 11 | 9540-01-363-8544 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 11 | 9540-01-363-8544 | beam structural | society of automotive engineers inc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-363-8544 | beam structural | boeing company the | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.250 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJB | FIRST TIP RADIUS | 0.078 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.078 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 |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CNBB | THIRD TIP RADIUS | 0.039 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT 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 |
| MATT | MATERIAL | ALUMINUM ALLOY, AMS-QQ-A-200/11, ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6511 TEMPER |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.078 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.301 POUNDS PER LINEAR FOOT |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.078 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.000 INCHES NOMINAL |
| HEAT | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
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