NSN 9540-01-353-5557 of Beam Structural - Parts Details
| Alternative NSN: 9540013535557 |
| 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: Federal Specifications Promulgat , Sae International , Society Of Automotive Engineers Inc , Transtar Metals Corp , Boeing Company |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers QQ-A-200 3, AMS QQ A 200 3, 60-6483, 4E-242 under NSN 9540-01-353-5557 of Beam Structural manufactured by Federal Specifications Promulgat, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp, Boeing Company.
Federal Supply Class of NSN 9540-01-353-5557 is FSC 9540 contains part details of Structural Shapes Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9540-01-353-5557, 9540013535557
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Part No Manufacturer Item Name QTY RFQ QQ-A-200 3 Federal Specifications Promulgat beam structural Avl RFQ AMS QQ A 200 3 Sae International beam structural Avl RFQ AMS QQ A 200 3 Society Of Automotive Engineers Inc beam structural Avl RFQ 60-6483 Transtar Metals Corp beam structural Avl RFQ 4E-242 Boeing Company beam structural Avl RFQ
Characteristics Data of NSN 9540013535557MRC 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
| 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 |