At NSN Unlimited, we maintain a large database of parts AMS QQ A 200 11, AMS-QQ-A-200 11, CVC10010 554CA, CVC10010-554CA, QQ A 200 11 with NSN 9540-01-437-8722 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Sae International, Federal Specifications, Triumph Aerostructures Llc, Society Of Automotive Engineers Inc, 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: 9540-01-437-8722 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 014378722 |
NCB Code: USA (01) |
Manufacturers: Sae International , Federal Specifications , Triumph Aerostructures Llc , Society Of Automotive Engineers Inc , Vought Aircraft Industries Inc |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
AMS QQ A 200 11 | 9540-01-437-8722 | beam structural | sae international | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-437-8722 | beam structural | federal specifications | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-437-8722 | beam structural | triumph aerostructures llc | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-437-8722 | beam structural | society of automotive engineers inc | Avl | RFQ |
CVC10010 554CA | 9540-01-437-8722 | beam structural | triumph aerostructures llc | Avl | RFQ |
CVC10010-554CA | 9540-01-437-8722 | beam structural | vought aircraft industries inc | Avl | RFQ |
CVC10010-554CA | 9540-01-437-8722 | beam structural | society of automotive engineers inc | Avl | RFQ |
CVC10010-554CA | 9540-01-437-8722 | beam structural | federal specifications | Avl | RFQ |
QQ A 200 11 | 9540-01-437-8722 | beam structural | federal specifications | Avl | RFQ |
QQ-A-200 11 | 9540-01-437-8722 | beam structural | triumph aerostructures llc | Avl | RFQ |
QQ-A-200 11 | 9540-01-437-8722 | beam structural | society of automotive engineers inc | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AJJB | FIRST TIP RADIUS | 0.125 INCHES NOMINAL |
AJJP | LEG THICKNESS | 0.156 INCHES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
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 | 2.500 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | LOWER RADIUS |
CNBB | THIRD TIP RADIUS | 0.156 INCHES NOMINAL |
ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER 0 |
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 | 2.000 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
ABRY | LENGTH | 12.000 FEET NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
CNQM | THIRD TIP STYLE | FULL RADIUS |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.156 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.156 INCHES NOMINAL |
AARN | FABRICATION METHOD | EXTRUDED |
HEAT | HEAT TREATMENT | 0-ANNEALED |
AGTA | BASIC SHAPE STYLE | T SHAPE |
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