At NSN Unlimited, we maintain a large database of parts 4E 242, 4E-242, 60-6483, AMS QQ A 200 3, AMS-QQ-A-200 3 with NSN 9540-01-353-5557 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Boeing Company The, Society Of Automotive Engineers Inc, Federal Specifications, Transtar Metals Corp, 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: 9540-01-353-5557 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013535557 |
NCB Code: USA (01) |
Manufacturers: Boeing Company The , Society Of Automotive Engineers Inc , Federal Specifications , Transtar Metals Corp , Sae International |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
4E 242 | 9540-01-353-5557 | beam structural | boeing company the | Avl | RFQ |
4E-242 | 9540-01-353-5557 | beam structural | society of automotive engineers inc | Avl | RFQ |
4E-242 | 9540-01-353-5557 | beam structural | federal specifications | Avl | RFQ |
60-6483 | 9540-01-353-5557 | beam structural | transtar metals corp | Avl | RFQ |
60-6483 | 9540-01-353-5557 | beam structural | society of automotive engineers inc | Avl | RFQ |
60-6483 | 9540-01-353-5557 | beam structural | boeing company the | Avl | RFQ |
60-6483 | 9540-01-353-5557 | beam structural | federal specifications | Avl | RFQ |
AMS QQ A 200 3 | 9540-01-353-5557 | beam structural | sae international | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-353-5557 | beam structural | federal specifications | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-353-5557 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-353-5557 | beam structural | boeing company the | Avl | RFQ |
QQ A 200 3 | 9540-01-353-5557 | beam structural | federal specifications | Avl | RFQ |
QQ-A-200 3 | 9540-01-353-5557 | beam structural | society of automotive engineers inc | Avl | RFQ |
QQ-A-200 3 | 9540-01-353-5557 | beam structural | boeing company the | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 2.125 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.125 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.938 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.938 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 | 1.875 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.589 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | SQUARE END |
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-8511 SOLUTION HEAT TREATED |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T8511 TEMPER |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE |
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