NSN 9540-01-029-9060 of Beam Structural - Parts Details
Alternative NSN: 9540010299060 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 010299060 |
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, AMS QQ A 200 3, 60-5850, 1MA160B01-10250 under NSN 9540-01-029-9060 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 9540-01-029-9060 is FSC 9540 contains part details of Structural Shapes Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9540-01-029-9060, 9540010299060
-
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 60-5850 Transtar Metals Corp beam structural Avl RFQ 1MA160B01-10250 Boeing Company beam structural Avl RFQ 1M57255 Boeing Company beam structural Avl RFQ
Characteristics Data of NSN 9540010299060MRC Criteria Characteristic AARN FABRICATION METHOD EXTRUDED ABKW OVERALL HEIGHT 1.086 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 AGTA BASIC SHAPE STYLE T SHAPE AJJP LEG THICKNESS 0.063 INCHES NOMINAL BPXD LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 1.5685 INCHES NOMINAL BPXG RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES 1.6515 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 3.220 INCHES NOMINAL BRFD WEIGHT PER UNIT MEASURE 0.330 POUNDS PER LINEAR FOOT 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 CRZC RIGHT TOP INSIDE ANGLE 76.0 DEGREES NOMINAL CSMZ LEFT TOP INSIDE ANGLE 104.0 DEGREES NOMINAL HEAT HEAT TREATMENT O-ANNEALED MATT MATERIAL ALUMINUM ALLOY 2024 MDCL MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE ZZZT NONDEFINITIVE SPEC/STD DATA O TEMPER
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.086 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 |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.063 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.5685 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.6515 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 | 3.220 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.330 POUNDS PER LINEAR FOOT |
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 |
CRZC | RIGHT TOP INSIDE ANGLE | 76.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 104.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATT | MATERIAL | ALUMINUM ALLOY 2024 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE |
ZZZT | NONDEFINITIVE SPEC/STD DATA | O TEMPER |