At NSN Unlimited, we maintain a large database of parts 1MA160B04-10386, 60-19675 2024-T8511, AMS QQ A 200 3, AMS-QQ-A-200 3, ASTM B221 with NSN 9540-01-363-6174 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Boeing Company The, Transtar Metals Corp, Society Of Automotive Engineers Inc, Sae International, American Society For Testing And. 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: 9540-01-363-6174 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013636174 |
NCB Code: USA (01) |
Manufacturers: Boeing Company The , Transtar Metals Corp , Society Of Automotive Engineers Inc , Sae International , American Society For Testing And , Federal Specifications |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
1MA160B04-10386 | 9540-01-363-6174 | beam structural | boeing company the | Avl | RFQ |
60-19675 2024-T8511 | 9540-01-363-6174 | beam structural | transtar metals corp | Avl | RFQ |
60-19675 2024-T8511 | 9540-01-363-6174 | beam structural | boeing company the | Avl | RFQ |
60-19675 2024-T8511 | 9540-01-363-6174 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS QQ A 200 3 | 9540-01-363-6174 | beam structural | sae international | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-363-6174 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-363-6174 | beam structural | boeing company the | Avl | RFQ |
ASTM B221 | 9540-01-363-6174 | beam structural | society of automotive engineers inc | Avl | RFQ |
ASTM B221 | 9540-01-363-6174 | beam structural | american society for testing and | Avl | RFQ |
ASTM B221 | 9540-01-363-6174 | beam structural | boeing company the | Avl | RFQ |
OT99817-13 | 9540-01-363-6174 | beam structural | society of automotive engineers inc | Avl | RFQ |
OT99817-13 | 9540-01-363-6174 | beam structural | boeing company the | Avl | RFQ |
QQ-A-200 3 | 9540-01-363-6174 | beam structural | federal specifications | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.820 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.070 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.070 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.110 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.765 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 1.530 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.361 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | SQUARE END |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | T-8511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T8511 TEMPER |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.765 INCHES NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
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