Alternative NSN: 9540-00-230-2339 |
Item Name:Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 002302339 |
NCB Code: USA (00) |
Manufacturers: Aluminum Co Of America , Sae International , Society Of Automotive Engineers Inc , Airforce-Navy Aeronautical Design Standard , Defense Logistics Agency Dba Defense Supply Center Philadelphia , American Society For Testing And , Lockheed Martin Corp Div Lockheed Martin Aeronautics Company , Astm Institute For Standards , Federal Specifications |
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
31106 | Aluminum Co Of America | 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 |
AMS10136-2407 | Sae International | beam structural | Avl | RFQ |
AMS10136-2407 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
AMS10136-2407 | Aluminum Co Of America | beam structural | Avl | RFQ |
AND10136-2407 | Aluminum Co Of America | beam structural | Avl | RFQ |
AND10136-2407 | Airforce-Navy Aeronautical Design Standard | beam structural | Avl | RFQ |
AND10136-2407/QQ-A-200/11-T6511 | Defense Logistics Agency Dba Defense Supply Center Philadelphia | beam structural | Avl | RFQ |
ASTM B221 | American Society For Testing And | beam structural | Avl | RFQ |
LS10136-2407 | Lockheed Martin Corp Div Lockheed Martin Aeronautics Company | beam structural | Avl | RFQ |
LS10136-2407-5 | 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 | 2.000 INCHES NOMINAL |
ABRY | LENGTH | 12.000 FEET NOMINAL |
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 | 0.125 INCHES NOMINAL |
AJJP | LEG THICKNESS | 0.125 INCHES NOMINAL |
ALBY | USAGE DESIGN | AIRCRAFT |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 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 | 2.500 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.650 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | LOWER RADIUS |
CNBB | THIRD TIP RADIUS | 0.063 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
CNQM | THIRD TIP STYLE | FULL RADIUS |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | 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 T6511 TEMPER |
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