At NSN Unlimited, we maintain a large database of parts 1325206, 18387, 40290, 6352, AMS-QQ-A-200 11 with NSN 9540-00-555-0819 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Boeing Company The, International Light Metals Corp, Bohn Aluminum And Brass Co, Reynolds Metals Co, Society Of Automotive Engineers Inc. Utilize our interface to browse items by part number, part type, manufacturer, and more. Obtain insights on top MRO and FBO services, Manufacturer profiles, and part catalogs.
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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 , International Light Metals Corp , Bohn Aluminum And Brass Co , Reynolds Metals Co , Society Of Automotive Engineers Inc , Sae International , Hiller Aircraft Corporation , Federal Specifications , Cessna Aircraft Company |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
1325206 | 9540-00-555-0819 | beam structural | boeing company the | Avl | RFQ |
18387 | 9540-00-555-0819 | beam structural | international light metals corp | Avl | RFQ |
40290 | 9540-00-555-0819 | beam structural | bohn aluminum and brass co | Avl | RFQ |
6352 | 9540-00-555-0819 | beam structural | reynolds metals co | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-00-555-0819 | beam structural | bohn aluminum and brass co | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-00-555-0819 | beam structural | boeing company the | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-00-555-0819 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-00-555-0819 | beam structural | sae international | Avl | RFQ |
AMS10136-2001 | 9540-00-555-0819 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS10136-2001 | 9540-00-555-0819 | beam structural | sae international | Avl | RFQ |
FS50102-2010 | 9540-00-555-0819 | beam structural | hiller aircraft corporation | Avl | RFQ |
QQ-A-200 11 | 9540-00-555-0819 | beam structural | federal specifications | Avl | RFQ |
RY32009 | 9540-00-555-0819 | beam structural | bohn aluminum and brass co | Avl | RFQ |
RY32009 | 9540-00-555-0819 | beam structural | boeing company the | Avl | RFQ |
S140 | 9540-00-555-0819 | beam structural | cessna aircraft company | 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 |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
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