The NSN 9540-00-881-3896 part numbers such as 72236, AMS-QQ-A-200 11, AMS-QQ-A-200 11, QQ A 200 11, S1419366S manufactured by Aluminum Co Of America, Sae International, Society Of Automotive Engineers Inc, Federal Specifications, 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 9540-00-881-3896. 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: 9540-00-881-3896 |
| Item Name: Beam Structural |
| Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
| NIIN: 008813896 |
| NCB Code: USA (00) |
| Manufacturers: Aluminum Co Of America, Sae International, Society Of Automotive Engineers Inc, Federal Specifications, Boeing Company The |
| Aluminum Co Of America | Sae International | Society Of Automotive Engineer.. |
| Federal Specifications | Boeing Company The |
| Part No | NSN | Item Name | QTY | RFQ |
|---|---|---|---|---|
| 72236 | 9540-00-881-3896 | beam structural | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-00-881-3896 | beam structural | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-00-881-3896 | beam structural | Avl | RFQ |
| QQ A 200 11 | 9540-00-881-3896 | beam structural | Avl | RFQ |
| S1419366S | 9540-00-881-3896 | beam structural | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 4.094 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.125 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.062 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.063 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP 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 |
| BQJG | TOP FLANGE WIDTH | 2.125 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 1.070 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBD | FIRST TIP INNER RADIUS | 0.032 INCHES NOMINAL |
| CNBJ | FIRST TIP OUTER RADIUS | 0.156 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| 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 | O 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