At NSN Unlimited, we maintain a large database of parts 33481, AMS-QQ-A-200 11, DIE PA6218, QQ-A-200 11 with NSN 9540-00-288-0495 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Transtar Metals Corp, Cessna Aircraft Company, Aluminum Co Of America, Society Of Automotive Engineers Inc, Sae International. 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: 9540-00-288-0495 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 002880495 |
NCB Code: USA (00) |
Manufacturers: Transtar Metals Corp , Cessna Aircraft Company , Aluminum Co Of America , Society Of Automotive Engineers Inc , Sae International , Federal Specifications |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
33481 | 9540-00-288-0495 | beam structural | transtar metals corp | Avl | RFQ |
33481 | 9540-00-288-0495 | beam structural | cessna aircraft company | Avl | RFQ |
33481 | 9540-00-288-0495 | beam structural | aluminum co of america | Avl | RFQ |
33481 | 9540-00-288-0495 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-00-288-0495 | beam structural | sae international | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-00-288-0495 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-00-288-0495 | beam structural | transtar metals corp | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-00-288-0495 | beam structural | cessna aircraft company | Avl | RFQ |
DIE PA6218 | 9540-00-288-0495 | beam structural | transtar metals corp | Avl | RFQ |
QQ-A-200 11 | 9540-00-288-0495 | beam structural | transtar metals corp | Avl | RFQ |
QQ-A-200 11 | 9540-00-288-0495 | beam structural | society of automotive engineers inc | Avl | RFQ |
QQ-A-200 11 | 9540-00-288-0495 | beam structural | federal specifications | Avl | RFQ |
QQ-A-200 11 | 9540-00-288-0495 | beam structural | cessna aircraft company | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.750 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.062 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.062 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.062 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.125 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.125 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.250 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.300 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | SQUARE END |
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 | T-6 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
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