NSN 9540-01-329-4391 of Beam Structural - Parts Details
Alternative NSN: 9540013294391 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013294391 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications Promulgat , Boeing Company , Sae International , Society Of Automotive Engineers Inc , Transtar Metals Corp |
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, LS043-0446, AMS-QQ-A-200 3, AMS QQ A 200 3, 60-6679 under NSN 9540-01-329-4391 of Beam Structural manufactured by Federal Specifications Promulgat, Boeing Company, Sae International, Society Of Automotive Engineers Inc, Transtar Metals Corp.
Federal Supply Class of NSN 9540-01-329-4391 is FSC 9540 contains part details of Structural Shapes Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9540-01-329-4391, 9540013294391
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Part No Manufacturer Item Name QTY RFQ QQ-A-200 3 Federal Specifications Promulgat beam structural Avl RFQ LS043-0446 Boeing Company 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 60-6679 Transtar Metals Corp beam structural Avl RFQ
Characteristics Data of NSN 9540013294391MRC Criteria Characteristic AARN FABRICATION METHOD EXTRUDED 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 AGAV III END ITEM IDENTIFICATION B-1B AIRCRAFT AGTA BASIC SHAPE STYLE T SHAPE AJJP LEG THICKNESS 0.125 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 4.100 INCHES NOMINAL BRFD WEIGHT PER UNIT MEASURE 0.919 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 CSMZ LEFT TOP INSIDE ANGLE 90.0 DEGREES NOMINAL HEAT HEAT TREATMENT T-81 SOLUTION HEAT TREATED MATT MATERIAL ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 ABKW OVERALL HEIGHT 2.100 INCHES NOMINAL BPXG RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 2.050 INCHES NOMINAL BPXD LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 2.050 INCHES NOMINAL CNQL THIRD TIP RELATIONSHIP TO PRECEDING TIPS IDENTICAL W/FIRST TIP ZZZT NONDEFINITIVE SPEC/STD DATA T81 TEMPER
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
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 |
AGAV | III END ITEM IDENTIFICATION | B-1B AIRCRAFT |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.125 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 | 4.100 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.919 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 |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | T-81 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
ABKW | OVERALL HEIGHT | 2.100 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.050 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.050 INCHES NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T81 TEMPER |