Alternative NSN: 9540-00-555-0819 |
Item Name:Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 005550819 |
NCB Code: USA (00) |
Manufacturers: Boeing Company The , Emerson Process Management Ltd , Mc Gill Aircraft Parts Inc , International Light Metals Corp , Bohn Aluminum And Brass Co , Reynolds Metals Co , Sae International , Society Of Automotive Engineers Inc , Airforce-Navy Aeronautical Design Standard , Hiller Aircraft Corporation , Astm Institute For Standards , Federal Specifications , Northrop Grumman Systems Corporation , Textron Aviation Inc , Cessna Aircraft Company |
Part No | Manufacturer | Item Name | QTY | RFQ |
---|---|---|---|---|
1325206 | Boeing Company The | beam structural | Avl | RFQ |
1325206 | Emerson Process Management Ltd | beam structural | Avl | RFQ |
1325206 | Mc Gill Aircraft Parts Inc | beam structural | Avl | RFQ |
18387 | International Light Metals Corp | beam structural | Avl | RFQ |
40290 | Bohn Aluminum And Brass Co | beam structural | Avl | RFQ |
6352 | Reynolds Metals Co | beam structural | Avl | RFQ |
6352 | Boeing Company The | beam structural | Avl | RFQ |
6352 | Bohn Aluminum And Brass Co | 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 |
AMS10136-2001 | Sae International | beam structural | Avl | RFQ |
AMS10136-2001 | Society Of Automotive Engineers Inc | beam structural | Avl | RFQ |
AND10136-2001 | Airforce-Navy Aeronautical Design Standard | beam structural | Avl | RFQ |
FS50102-2010 | Hiller Aircraft Corporation | 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 |
RY32009 | Boeing Company The | beam structural | Avl | RFQ |
RY32009 | Bohn Aluminum And Brass Co | beam structural | Avl | RFQ |
RY32009 | Northrop Grumman Systems Corporation | beam structural | Avl | RFQ |
S140 | Textron Aviation Inc | beam structural | Avl | RFQ |
S140 | Cessna Aircraft Company | beam structural | Avl | RFQ |
S140 | Bohn Aluminum And Brass Co | beam structural | Avl | RFQ |
S140 | Boeing Company The | beam structural | Avl | RFQ |
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 | 0.078 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.078 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJB | FIRST TIP RADIUS | 0.078 INCHES NOMINAL |
AJJP | LEG THICKNESS | 0.078 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 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 | 2.000 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.277 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | LOWER RADIUS |
CNBB | THIRD TIP RADIUS | 0.039 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-6 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 | T6 TEMPER |
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