NSN 9540-00-486-6406 of Beam Structural - Parts Details
| Alternative NSN: 9540004866406 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 004866406 |
| NCB Code: USA (00) |
| Manufacturers: Federal Specifications Promulgat , Society Of Automotive Engineers Inc , Sae International , 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, 1MA160B04-10124 under NSN 9540-00-486-6406 of Beam Structural manufactured by Federal Specifications Promulgat, Society Of Automotive Engineers Inc, Sae International, Boeing Company.
Federal Supply Class of NSN 9540-00-486-6406 is FSC 9540 contains part details of Structural Shapes Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9540-00-486-6406, 9540004866406
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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 Society Of Automotive Engineers Inc beam structural Avl RFQ AMS-QQ-A-200 3 Sae International beam structural Avl RFQ 1MA160B04-10124 Boeing Company beam structural Avl RFQ
Characteristics Data of NSN 9540004866406MRC Criteria Characteristic AARN FABRICATION METHOD EXTRUDED ABKW OVERALL HEIGHT 1.500 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 AJJB FIRST TIP RADIUS 0.125 INCHES NOMINAL AJJP LEG THICKNESS 0.125 INCHES NOMINAL BPXD LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 1.500 INCHES NOMINAL BPXG RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 1.500 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 3.000 INCHES NOMINAL BRFD WEIGHT PER UNIT MEASURE 0.650 POUNDS PER LINEAR FOOT CMZY FIRST TIP STYLE LOWER RADIUS CNBB THIRD TIP RADIUS 0.062 INCHES NOMINAL CNQJ SECOND TIP RELATIONSHIP TO FIRST TIP IDENTICAL CNQL THIRD TIP RELATIONSHIP TO PRECEDING TIPS NOT IDENTICAL CNQM THIRD TIP STYLE FULL RADIUS CRZC RIGHT TOP INSIDE ANGLE 90.0 DEGREES NOMINAL CSMZ LEFT TOP INSIDE ANGLE 90.0 DEGREES NOMINAL HEAT HEAT TREATMENT O-ANNEALED MATT MATERIAL ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 ZZZT NONDEFINITIVE SPEC/STD DATA O TEMPER
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.500 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 |
| AJJB | FIRST TIP RADIUS | 0.125 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.125 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.500 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.500 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 | 3.000 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.650 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CNBB | THIRD TIP RADIUS | 0.062 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
| CNQM | THIRD TIP STYLE | FULL RADIUS |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | O TEMPER |