Alternative NSN: 9540-00-148-4791 |
Item Name:Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 001484791 |
NCB Code: USA (00) |
Manufacturers: The Boeing Company , Society Of Automotive Engineers Inc , Aluminum Co Of America , Boeing Company The , Bristol Industries , Alcoa Reynolds Metals Company , Sae International , Tracor Flight Systems Inc , Bae Systems Technology Solutions And Services Inc Dba Bae Systems Information And , Hughes Missile Systems Co San Diego , General Dynamics Corporation , Lockheed Martin Corp Div Lockheed Martin Aeronautics Company , Astm Institute For Standards , Federal Specifications |
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
1566 | The Boeing Company | beam structural | Avl | RFQ |
1566 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
1566 | Aluminum Co Of America | beam structural | Avl | RFQ |
1566 | Boeing Company The | beam structural | Avl | RFQ |
1M544 | Boeing Company The | beam structural | Avl | RFQ |
1M544 | Bristol Industries | beam structural | Avl | RFQ |
4078 | The Boeing Company | beam structural | Avl | RFQ |
4078 | Boeing Company The | beam structural | Avl | RFQ |
4078 | Alcoa Reynolds Metals Company | beam structural | Avl | RFQ |
4078 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
AMS QQ A 200 11 | Sae International | beam structural | Avl | RFQ |
AMS-QQ-A-200 11 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
BAC1505-34393 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
BAC1505-34393 | The Boeing Company | beam structural | Avl | RFQ |
E731306 | Tracor Flight Systems Inc | beam structural | Avl | RFQ |
E731306 | Bae Systems Technology Solutions And Services Inc Dba Bae Systems Information And | beam structural | Avl | RFQ |
E731306 | Hughes Missile Systems Co San Diego | beam structural | Avl | RFQ |
E731306 | General Dynamics Corporation | beam structural | Avl | RFQ |
LS3682-2 | Lockheed Martin Corp Div Lockheed Martin Aeronautics Company | beam structural | Avl | RFQ |
QQ-A-200-11 | Astm Institute For Standards | beam structural | Avl | RFQ |
QQ-A-200/11 | Federal Specifications | beam structural | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 2.500 INCHES NOMINAL |
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 |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJB | FIRST TIP RADIUS | 0.062 INCHES NOMINAL |
AJJP | LEG THICKNESS | 0.188 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.125 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.125 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.250 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.870 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | FULL RADIUS |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED OR T-6511 SOLUTION HEAT TREATED |
MATL | UNABLE TO DECODE | UNABLE TO DECODE |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11,ALLOY 7075 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6 TEMPER OR T6511 TEMPER |
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