At NSN Unlimited, we maintain a large database of parts 1MA160D01-10431, 60 14822 7075 O, 60-14822 7075-O, AMS QQ A 200 11, AMS-QQ-A-200 11 with NSN 9540-01-363-8532 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Society Of Automotive Engineers Inc, Federal Specifications, Boeing Company The, Transtar Metals Corp, Sae International. 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: 9540-01-363-8532 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013638532 |
NCB Code: USA (01) |
Manufacturers: Society Of Automotive Engineers Inc , Federal Specifications , Boeing Company The , Transtar Metals Corp , Sae International |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
1MA160D01-10431 | 9540-01-363-8532 | beam structural | society of automotive engineers inc | Avl | RFQ |
1MA160D01-10431 | 9540-01-363-8532 | beam structural | federal specifications | Avl | RFQ |
1MA160D01-10431 | 9540-01-363-8532 | beam structural | boeing company the | Avl | RFQ |
60 14822 7075 O | 9540-01-363-8532 | beam structural | transtar metals corp | Avl | RFQ |
60-14822 7075-O | 9540-01-363-8532 | beam structural | federal specifications | Avl | RFQ |
60-14822 7075-O | 9540-01-363-8532 | beam structural | boeing company the | Avl | RFQ |
60-14822 7075-O | 9540-01-363-8532 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS QQ A 200 11 | 9540-01-363-8532 | beam structural | sae international | Avl | RFQ |
AMS QQ A 200 11 | 9540-01-363-8532 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-363-8532 | beam structural | federal specifications | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-363-8532 | beam structural | boeing company the | Avl | RFQ |
QQ A 200 11 | 9540-01-363-8532 | beam structural | federal specifications | Avl | RFQ |
QQ-A-200 11 | 9540-01-363-8532 | beam structural | society of automotive engineers inc | Avl | RFQ |
QQ-A-200 11 | 9540-01-363-8532 | beam structural | boeing company the | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 2.000 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.090 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.090 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.090 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.845 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.607 POUNDS PER LINEAR FOOT |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
MATT | MATERIAL | ALUMINUM ALLOY, AMS-QQ-A-200/11, ALLOY 7075 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND ANNEALED CONDITION |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.855 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 3.700 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | LOWER RADIUS |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | O-ANNEALED |
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