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Quality guaranteed We sell only warrantied and traceable partsMfg Part Number: QQ-A-200 11
Alternate P/N: QQA20011
NSN : 9540-01-437-4386
NIIN : 014374386
CAGE Code : 80378
Manufacturer: Triumph Aerostructures Llc
Item Name : Beam Structural
In our inventory, we have more than two billion new and obsolete NSN part like QQ-A-200 11. Aviation Sphere can offer an impressive selection of NSN parts. This includes parts like QQ-A-200 11 Beam Structural from manufacturer Triumph Aerostructures Llc and many more, all of which are available with short lead times and competitive prices. For parts not in our inventory, our dedicated account managers can help you track them down through our international supply chain network that extends across the United States, Canada, and the United Kingdom. Furthermore, Aviation Sphere is an AS9120B, ISO 9001:2015, and FAA AC 0056B accredited business, as well as the only independent distributor with a strict No China Sourcing Pledge, allowing us to ensure that each part part like QQ-A-200 11, you purchase from us is fully traceable or comes directly from its manufacturer.
Our website offers a number of parametric search capabilities, one of which allows you to search specifically for NSN part like QQ-A-200 11. This means you can quickly sort through National Stock Numbers such as 9540014374386 and find parts from quality manufacturers like Triumph Aerostructures Llc and many others. To begin the purchasing process immediately, submit an RFQ today. Our team of dedicated account managers is standing by and will respond to all inquiries in 15 minutes or less.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-437-4386 Item Description: Beam Structural | 9540 | 014374386 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| Qq-A-200 11 | 5 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AJJP | LEG THICKNESS | 0.190 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.190 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.190 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 4.010 INCHES NOMINAL |
| MATL | MATERIAL | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | COMPOSITION AB-1 AND CONDITION ANNEALED |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| ABKW | OVERALL HEIGHT | 2.560 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.005 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.005 INCHES NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.190 INCHES NOMINAL |
| AARN | FABRICATION METHOD | EXTRUDED |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.190 INCHES NOMINAL |
| HEAT | HEAT TREATMENT | ANNEALED |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
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