The NSN 9540-01-363-8541 part numbers such as QQ A 200 11, AMS-QQ-A-200 11, AMS QQ A 200 11, 60-26400, 1MA160D01-10566 manufactured by Federal Specifications, Society Of Automotive Engineers Inc, Sae International, Transtar Metals Corp, Boeing Company The are available in RFQ Experts’ inventory. An ASAP Semiconductor owned and operated website, RFQ Experts has over six billion parts in its inventory for NSN 9540-01-363-8541. ASAP is committed to streamlining the parts procurement process for our customers, making it easy for them to search through billions of parts to find exactly what they are looking for. We have dedicated account managers ready to solve procurement issues our clients face, whether it’s a need for obsolete parts, or an aircraft on ground situation. As an AS9120B, ISO 9001:2015, and FAA AC 0056B certified company, each and every part that we ship goes through numerous quality checks and inspections, to ensure that we sell only the highest-quality parts.
| Alternative NSN: 9540-01-363-8541 |
| Item Name: Beam Structural |
| Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
| NIIN: 013638541 |
| NCB Code: USA (01) |
| Manufacturers: Federal Specifications, Society Of Automotive Engineers Inc, Sae International, Transtar Metals Corp, Boeing Company The |
| Federal Specifications | Society Of Automotive Engineer.. | Sae International |
| Transtar Metals Corp | Boeing Company The |
| Part No | NSN | Item Name | QTY | RFQ |
|---|---|---|---|---|
| QQ A 200 11 | 9540-01-363-8541 | beam structural | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-363-8541 | beam structural | Avl | RFQ |
| AMS QQ A 200 11 | 9540-01-363-8541 | beam structural | Avl | RFQ |
| 60-26400 | 9540-01-363-8541 | beam structural | Avl | RFQ |
| 1MA160D01-10566 | 9540-01-363-8541 | beam structural | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.350 INCHES NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.250 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.863 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.037 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 |
| BRFD | WEIGHT PER UNIT MEASURE | 1.197 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| 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 | 7075 ALLOY AND ANNEALED CONDITION |
| AJJP | LEG THICKNESS | 0.125 INCHES NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BQJG | TOP FLANGE WIDTH | 3.900 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
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