At NSN Unlimited, we maintain a large database of parts AMS QQ A 200 11, AMS-QQ-A-200 11, CVC10011 4CA, CVC10011-4CA, QQ A 200 11 with NSN 9540-01-443-6647 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Society Of Automotive Engineers Inc, Sae International, Federal Specifications, Triumph Aerostructures Llc, Vought Aircraft Industries Inc. 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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Alternative NSN: 9540-01-443-6647 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 014436647 |
NCB Code: USA (01) |
Manufacturers: Society Of Automotive Engineers Inc , Sae International , Federal Specifications , Triumph Aerostructures Llc , Vought Aircraft Industries Inc |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
AMS QQ A 200 11 | 9540-01-443-6647 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS QQ A 200 11 | 9540-01-443-6647 | beam structural | sae international | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-443-6647 | beam structural | federal specifications | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-443-6647 | beam structural | triumph aerostructures llc | Avl | RFQ |
CVC10011 4CA | 9540-01-443-6647 | beam structural | triumph aerostructures llc | Avl | RFQ |
CVC10011-4CA | 9540-01-443-6647 | beam structural | vought aircraft industries inc | Avl | RFQ |
CVC10011-4CA | 9540-01-443-6647 | beam structural | society of automotive engineers inc | Avl | RFQ |
CVC10011-4CA | 9540-01-443-6647 | beam structural | federal specifications | Avl | RFQ |
QQ A 200 11 | 9540-01-443-6647 | beam structural | federal specifications | Avl | RFQ |
QQ-A-200 11 | 9540-01-443-6647 | beam structural | triumph aerostructures llc | Avl | RFQ |
QQ-A-200 11 | 9540-01-443-6647 | beam structural | society of automotive engineers inc | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AJJP | LEG THICKNESS | 0.100 INCHES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.630 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 |
BQJG | TOP FLANGE WIDTH | 4.130 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE END |
ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND CONDITION ANNEALED |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
ABKW | OVERALL HEIGHT | 2.250 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.5000 INCHES NOMINAL |
ABRY | LENGTH | 12.000 FEET NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.100 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.100 INCHES NOMINAL |
AARN | FABRICATION METHOD | EXTRUDED |
HEAT | HEAT TREATMENT | ANNEALED |
AGTA | BASIC SHAPE STYLE | T SHAPE |
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