At NSN Unlimited, we maintain a large database of parts 59411, AMS STD 184, AMS-QQ-A-200 3, AMS-QQ-A-200A, AMS-STD-184 with NSN 9540-00-017-6413 used in civil and defense applications for the aerospace, marine, and commercial manufactured by The Boeing Company, Federal Specifications, Aluminum Co Of America, Sae International, Society Of Automotive Engineers 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: 9540-00-017-6413 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 000176413 |
NCB Code: USA (00) |
Manufacturers: The Boeing Company , Federal Specifications , Aluminum Co Of America , Sae International , Society Of Automotive Engineers Inc |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
59411 | 9540-00-017-6413 | beam structural | the boeing company | Avl | RFQ |
59411 | 9540-00-017-6413 | beam structural | federal specifications | Avl | RFQ |
59411 | 9540-00-017-6413 | beam structural | aluminum co of america | Avl | RFQ |
AMS STD 184 | 9540-00-017-6413 | beam structural | sae international | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-00-017-6413 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-00-017-6413 | beam structural | sae international | Avl | RFQ |
AMS-QQ-A-200A | 9540-00-017-6413 | beam structural | the boeing company | Avl | RFQ |
AMS-QQ-A-200A | 9540-00-017-6413 | beam structural | federal specifications | Avl | RFQ |
AMS-QQ-A-200A | 9540-00-017-6413 | beam structural | aluminum co of america | Avl | RFQ |
AMS-QQ-A-200A | 9540-00-017-6413 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-200A | 9540-00-017-6413 | beam structural | sae international | Avl | RFQ |
AMS-STD-184 | 9540-00-017-6413 | beam structural | society of automotive engineers inc | Avl | RFQ |
BAC1505-100104 | 9540-00-017-6413 | beam structural | aluminum co of america | Avl | RFQ |
BAC1505-100104 | 9540-00-017-6413 | beam structural | federal specifications | Avl | RFQ |
BAC1505-100104 | 9540-00-017-6413 | beam structural | the boeing company | Avl | RFQ |
QQ-A-200 3 | 9540-00-017-6413 | beam structural | the boeing company | Avl | RFQ |
QQ-A-200 3 | 9540-00-017-6413 | beam structural | federal specifications | Avl | RFQ |
QQ-A-200 3 | 9540-00-017-6413 | beam structural | aluminum co of america | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 2.950 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.350 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.350 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.485 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.100 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.100 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.500 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.500 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.200 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 2.560 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
CNBD | FIRST TIP INNER RADIUS | 0.031 INCHES NOMINAL |
CNBJ | FIRST TIP OUTER RADIUS | 0.031 INCHES NOMINAL |
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-3511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND 3511 TEMPER |
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