NSN 9540-01-342-0428 of Beam Structural - Parts Details
Alternative NSN: 9540013420428 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013420428 |
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, 60-8959, 1MA160B04-10325 under NSN 9540-01-342-0428 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 9540-01-342-0428 is FSC 9540 contains part details of Structural Shapes Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9540-01-342-0428, 9540013420428
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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 60-8959 Transtar Metals Corp beam structural Avl RFQ 1MA160B04-10325 Boeing Company beam structural Avl RFQ
Characteristics Data of NSN 9540013420428MRC Criteria Characteristic AARN FABRICATION METHOD EXTRUDED ABKW OVERALL HEIGHT 1.000 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 AJJP LEG THICKNESS 0.063 INCHES NOMINAL BPXD LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 1.100 INCHES NOMINAL BPXG RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 1.100 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 CMZY FIRST TIP STYLE SQUARE END CNQJ SECOND TIP RELATIONSHIP TO FIRST TIP IDENTICAL CNQL THIRD TIP RELATIONSHIP TO PRECEDING TIPS IDENTICAL W/FIRST TIP CSMZ LEFT TOP INSIDE ANGLE 83.0 DEGREES NOMINAL HEAT HEAT TREATMENT T-8511 SOLUTION HEAT TREATED MATT MATERIAL ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 ZZZT NONDEFINITIVE SPEC/STD DATA T8511 TEMPER BQJG TOP FLANGE WIDTH 2.200 INCHES NOMINAL AGTA BASIC SHAPE STYLE T SHAPE BRFD WEIGHT PER UNIT MEASURE 0.242 POUNDS PER LINEAR FOOT CRZC RIGHT TOP INSIDE ANGLE 97.0 DEGREES NOMINAL
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.000 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 |
AJJP | LEG THICKNESS | 0.063 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.100 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.100 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 |
CMZY | FIRST TIP STYLE | SQUARE END |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CSMZ | LEFT TOP INSIDE ANGLE | 83.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | T-8511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T8511 TEMPER |
BQJG | TOP FLANGE WIDTH | 2.200 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
BRFD | WEIGHT PER UNIT MEASURE | 0.242 POUNDS PER LINEAR FOOT |
CRZC | RIGHT TOP INSIDE ANGLE | 97.0 DEGREES NOMINAL |