At NSN Unlimited, we maintain a large database of parts AMS QQ A 200 11, AMS-QQ-A-200 11, CVC10050-111CA, CVC10050-111CAX144, QQ A 200 11 with NSN 9540-01-435-9666 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Sae International, Society Of Automotive Engineers Inc, Federal Specifications, Triumph Aerostructures Llc. 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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Ready for a quote? Submit an Instant RFQ today for NSN 9540-01-435-9666.
| Alternative NSN: 9540-01-435-9666 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 014359666 |
| NCB Code: USA (01) |
| Manufacturers: Sae International , Society Of Automotive Engineers Inc , Federal Specifications , Triumph Aerostructures Llc |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| AMS QQ A 200 11 | 9540-01-435-9666 | beam structural | sae international | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-435-9666 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-01-435-9666 | beam structural | federal specifications | Avl | RFQ |
| CVC10050-111CA | 9540-01-435-9666 | beam structural | federal specifications | Avl | RFQ |
| CVC10050-111CA | 9540-01-435-9666 | beam structural | society of automotive engineers inc | Avl | RFQ |
| CVC10050-111CA | 9540-01-435-9666 | beam structural | triumph aerostructures llc | Avl | RFQ |
| CVC10050-111CAX144 | 9540-01-435-9666 | beam structural | federal specifications | Avl | RFQ |
| CVC10050-111CAX144 | 9540-01-435-9666 | beam structural | society of automotive engineers inc | Avl | RFQ |
| QQ A 200 11 | 9540-01-435-9666 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 11 | 9540-01-435-9666 | beam structural | society of automotive engineers inc | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
| BPXN | WEB FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 0.750 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 1.310 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE END |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER 0 |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CWKK | RIGHT BOTTOM INSIDE ANGLE | 84.0 DEGREES NOMINAL |
| ABKW | OVERALL HEIGHT | 2.190 INCHES NOMINAL |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AARN | FABRICATION METHOD | EXTRUDED |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| AGTA | BASIC SHAPE STYLE | Z SHAPE |
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