NSN 9540-01-341-6983 of Beam Structural - Parts Details
Alternative NSN: 9540013416983 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013416983 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications Promulgat , Society Of Automotive Engineers Inc , Sae International , 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, AMS QQ A 200 3, 60-7544, 1MA160B04-10340 under NSN 9540-01-341-6983 of Beam Structural manufactured by Federal Specifications Promulgat, Society Of Automotive Engineers Inc, Sae International, Transtar Metals Corp, Boeing Company.
Federal Supply Class of NSN 9540-01-341-6983 is FSC 9540 contains part details of Structural Shapes Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9540-01-341-6983, 9540013416983
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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 60-7544 Transtar Metals Corp beam structural Avl RFQ 1MA160B04-10340 Boeing Company beam structural Avl RFQ
Characteristics Data of NSN 9540013416983MRC Criteria Characteristic AARN FABRICATION METHOD EXTRUDED ABKW OVERALL HEIGHT 1.900 INCHES NOMINAL ABRY LENGTH 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM ADXR LEFT SIDE TOP FLANGE THICKNESS 0.063 INCHES NOMINAL ADXS RIGHT SIDE TOP FLANGE THICKNESS 0.063 INCHES NOMINAL AGAV III END ITEM IDENTIFICATION F-15 AIRCRAFT AGTA BASIC SHAPE STYLE T SHAPE AJJP LEG THICKNESS 0.063 INCHES NOMINAL BPXD LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 1.219 INCHES NOMINAL BPXJ FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG 0.094 INCHES NOMINAL BPXL FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG 0.094 INCHES NOMINAL BQJG TOP FLANGE WIDTH 2.450 INCHES NOMINAL BRFD WEIGHT PER UNIT MEASURE 0.329 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 98.0 DEGREES NOMINAL CSMZ LEFT TOP INSIDE ANGLE 82.0 DEGREES NOMINAL MATT MATERIAL ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 HEAT HEAT TREATMENT T-8511 SOLUTION HEAT TREATED ZZZT NONDEFINITIVE SPEC/STD DATA T8511 TEMPER BPXG RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 1.231 INCHES NOMINAL CNQJ SECOND TIP RELATIONSHIP TO FIRST TIP IDENTICAL
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.900 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
AGAV | III END ITEM IDENTIFICATION | F-15 AIRCRAFT |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.063 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.219 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.094 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.094 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.450 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.329 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 | 98.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 82.0 DEGREES NOMINAL |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
HEAT | HEAT TREATMENT | T-8511 SOLUTION HEAT TREATED |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T8511 TEMPER |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.231 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |