NSN 9540-01-339-0389 of Beam Structural - Parts Details
Alternative NSN: 9540013390389 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013390389 |
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, 60-5537, 1MA160B04-10297 under NSN 9540-01-339-0389 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 9540-01-339-0389 is FSC 9540 contains part details of Structural Shapes Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9540-01-339-0389, 9540013390389
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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 60-5537 Transtar Metals Corp beam structural Avl RFQ 1MA160B04-10297 Boeing Company beam structural Avl RFQ
Characteristics Data of NSN 9540013390389MRC Criteria Characteristic AARN FABRICATION METHOD EXTRUDED ABKW OVERALL HEIGHT 1.630 INCHES NOMINAL ABRY LENGTH 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM ADXR LEFT SIDE TOP FLANGE THICKNESS 0.080 INCHES NOMINAL ADXS RIGHT SIDE TOP FLANGE THICKNESS 0.080 INCHES NOMINAL AGAV III END ITEM IDENTIFICATION F-15 AIRCRAFT AGTA BASIC SHAPE STYLE T SHAPE AJJP LEG THICKNESS 0.080 INCHES NOMINAL BPXG RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 1.250 INCHES NOMINAL BPXL FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG 0.090 INCHES NOMINAL BQJG TOP FLANGE WIDTH 2.530 INCHES NOMINAL CNQJ SECOND TIP RELATIONSHIP TO FIRST TIP IDENTICAL CNQL THIRD TIP RELATIONSHIP TO PRECEDING TIPS IDENTICAL W/FIRST TIP HEAT HEAT TREATMENT T-8511 SOLUTION HEAT TREATED MATT MATERIAL ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 ZZZT NONDEFINITIVE SPEC/STD DATA 8511 TEMPER BPXJ FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG 0.090 INCHES NOMINAL BRFD WEIGHT PER UNIT MEASURE 0.396 POUNDS PER LINEAR FOOT CSMZ LEFT TOP INSIDE ANGLE 89.0 DEGREES NOMINAL BPXD LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 1.200 INCHES NOMINAL CMZY FIRST TIP STYLE SQUARE END CRZC RIGHT TOP INSIDE ANGLE 91.0 DEGREES NOMINAL
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.630 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.080 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.080 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | F-15 AIRCRAFT |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.080 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.530 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
HEAT | HEAT TREATMENT | T-8511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 8511 TEMPER |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.396 POUNDS PER LINEAR FOOT |
CSMZ | LEFT TOP INSIDE ANGLE | 89.0 DEGREES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.200 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE END |
CRZC | RIGHT TOP INSIDE ANGLE | 91.0 DEGREES NOMINAL |