At NSN Unlimited, we maintain a large database of parts 1MA160D03-10066, AMS-QQ-A-200 11, AND10136-1603, ASTM B221, QQ-A-200 11 with NSN 9540-01-367-1250 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Society Of Automotive Engineers Inc, Boeing Company The, Sae International, American Society For Testing And, Federal Specifications. 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: 9540-01-367-1250 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 013671250 |
| NCB Code: USA (01) |
| Manufacturers: Society Of Automotive Engineers Inc , Boeing Company The , Sae International , American Society For Testing And , Federal Specifications |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 1MA160D03-10066 | 9540-01-367-1250 | beam structural | society of automotive engineers inc | Avl | RFQ |
| 1MA160D03-10066 | 9540-01-367-1250 | beam structural | boeing company the | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-367-1250 | beam structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-367-1250 | beam structural | boeing company the | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-367-1250 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AND10136-1603 | 9540-01-367-1250 | beam structural | boeing company the | Avl | RFQ |
| AND10136-1603 | 9540-01-367-1250 | beam structural | society of automotive engineers inc | Avl | RFQ |
| ASTM B221 | 9540-01-367-1250 | beam structural | american society for testing and | Avl | RFQ |
| QQ-A-200 11 | 9540-01-367-1250 | beam structural | society of automotive engineers inc | Avl | RFQ |
| QQ-A-200 11 | 9540-01-367-1250 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 11 | 9540-01-367-1250 | beam structural | boeing company the | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.125 INCHES NOMINAL |
| ADXR | LEFT 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 | 0.875 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 1.750 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE END W/ LOWER RADIUS |
| CMZZ | SECOND TIP RADIUS | 0.094 INCHES NOMINAL |
| CNBG | THIRD TIP INNER RADIUS | 0.047 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| CNQK | SECOND TIP STYLE | SQUARE END W/ LOWER RADIUS |
| CNQM | THIRD TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6511 TEMPER |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.875 INCHES NOMINAL |
| CNBL | THIRD TIP OUTER RADIUS | 0.047 INCHES NOMINAL |
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