The NSN 9540-00-241-2712 part numbers such as 10081, 35302, AMS QQ A 200 11, AMS QQ A 200 11, AMS10134-3002 manufactured by Reynolds Metals Co, Aluminum Co Of America, Society Of Automotive Engineers Inc, Sae International, Federal Specifications 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 9540-00-241-2712. 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: 9540-00-241-2712 |
| Item Name: Beam Structural |
| Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
| NIIN: 002412712 |
| NCB Code: USA (00) |
| Manufacturers: Reynolds Metals Co, Aluminum Co Of America, Society Of Automotive Engineers Inc, Sae International, Federal Specifications |
| Reynolds Metals Co | Aluminum Co Of America | Society Of Automotive Engineer.. |
| Sae International | Federal Specifications |
| Part No | NSN | Item Name | QTY | RFQ |
|---|---|---|---|---|
| 10081 | 9540-00-241-2712 | beam structural | Avl | RFQ |
| 35302 | 9540-00-241-2712 | beam structural | Avl | RFQ |
| AMS QQ A 200 11 | 9540-00-241-2712 | beam structural | Avl | RFQ |
| AMS QQ A 200 11 | 9540-00-241-2712 | beam structural | Avl | RFQ |
| AMS10134-3002 | 9540-00-241-2712 | beam structural | Avl | RFQ |
| AMS10134-3002 | 9540-00-241-2712 | beam structural | Avl | RFQ |
| QQ-A-200 11 | 9540-00-241-2712 | beam structural | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 4.000 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.250 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.250 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | I SHAPE |
| AJJB | FIRST TIP RADIUS | 0.250 INCHES NOMINAL |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.250 INCHES NOMINAL |
| BMPR | LEFT SIDE BOTTOM FLANGE THICKNESS | 0.250 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.750 INCHES NOMINAL |
| BPXF | LEFT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.750 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.750 INCHES NOMINAL |
| BPXH | RIGHT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.750 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BPXK | FILLET RADIUS WHERE BOTTOM LEFT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BPXN | WEB FLANGE THICKNESS | 0.250 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 3.500 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 3.500 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 3.120 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CNBB | THIRD TIP RADIUS | 0.250 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
| CNQM | THIRD TIP STYLE | UPPER RADIUS |
| CNQN | FOURTH TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/THIRD TIP |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CTBR | LEFT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CWKK | RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T-6 TEMPER |
All Orders are Fulfilled in the U.S.A.
All shipments must comply with U.S.A export laws.
No exceptions.
The only independent distributor
with a NO CHINA SOURCING Pledge
“We Proudly Support Intrepid Fallen Heroes Fund that serves United States Military Personal experiencing the Invisible Wounds of War : Traumatic Brain Injury (TBI) and Post Traumatic Stress (PTS). Please visit website (www.fallenheroesfund.org) and help in their valiant effort”.
You Can Click Here to Get Quote For Your Required Aircraft Parts Within 15 Minutes.
Request for Quote