The NSN 9540-01-353-5557 part numbers such as QQ A 200 3, AMS QQ A 200 3, AMS QQ A 200 3, 60-6483, 4E 242 manufactured by Federal Specifications, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp, Boeing Company The are available in RFQ Experts’ inventory. An ASAP Semiconductor owned and operated website, RFQ Experts has over six billion parts in its inventory for NSN 9540-01-353-5557. ASAP is committed to streamlining the parts procurement process for our customers, making it easy for them to search through billions of parts to find exactly what they are looking for. We have dedicated account managers ready to solve procurement issues our clients face, whether it’s a need for obsolete parts, or an aircraft on ground situation. As an AS9120B, ISO 9001:2015, and FAA AC 0056B certified company, each and every part that we ship goes through numerous quality checks and inspections, to ensure that we sell only the highest-quality parts.
Alternative NSN: 9540-01-353-5557 |
Item Name: Beam Structural |
Federal Supply Class (FSC): 9540 Structural Shapes, Nonferrous Base Metal |
NIIN: 013535557 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp, Boeing Company The |
Federal Specifications | Sae International | Society Of Automotive Engineer.. |
Transtar Metals Corp | Boeing Company The |
Part No | NSN | Item Name | QTY | RFQ |
---|---|---|---|---|
QQ A 200 3 | 9540-01-353-5557 | beam structural | Avl | RFQ |
AMS QQ A 200 3 | 9540-01-353-5557 | beam structural | Avl | RFQ |
AMS QQ A 200 3 | 9540-01-353-5557 | beam structural | Avl | RFQ |
60-6483 | 9540-01-353-5557 | beam structural | Avl | RFQ |
4E 242 | 9540-01-353-5557 | beam structural | 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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