At NSN Unlimited, we maintain a large database of parts 1MA160D01-10100, 60-10118, AMS QQ A 200 11, AMS-QQ-A-200 11, ASTM B221 with NSN 9540-01-363-7434 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Federal Specifications, Boeing Company The, Transtar Metals Corp, Society Of Automotive Engineers Inc, 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: 9540-01-363-7434 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013637434 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications , Boeing Company The , Transtar Metals Corp , Society Of Automotive Engineers Inc , Sae International , National Aerospace Standards , American Society For Testing And |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
1MA160D01-10100 | 9540-01-363-7434 | beam structural | federal specifications | Avl | RFQ |
1MA160D01-10100 | 9540-01-363-7434 | beam structural | boeing company the | Avl | RFQ |
60-10118 | 9540-01-363-7434 | beam structural | transtar metals corp | Avl | RFQ |
AMS QQ A 200 11 | 9540-01-363-7434 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS QQ A 200 11 | 9540-01-363-7434 | beam structural | sae international | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-363-7434 | beam structural | national aerospace standards | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-363-7434 | beam structural | boeing company the | Avl | RFQ |
ASTM B221 | 9540-01-363-7434 | beam structural | american society for testing and | Avl | RFQ |
NAS344 54 | 9540-01-363-7434 | beam structural | national aerospace standards | Avl | RFQ |
NAS344-54 | 9540-01-363-7434 | beam structural | federal specifications | Avl | RFQ |
NAS344-54 | 9540-01-363-7434 | beam structural | boeing company the | Avl | RFQ |
QQ-A-200 11 | 9540-01-363-7434 | beam structural | federal specifications | Avl | RFQ |
QQ-A-200 11 | 9540-01-363-7434 | beam structural | boeing company the | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.125 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJB | FIRST TIP RADIUS | 0.094 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 | 0.125 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.372 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | LOWER RADIUS |
CNBB | THIRD TIP RADIUS | 0.047 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQM | THIRD TIP STYLE | FULL RADIUS |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
ZZZK | SPECIFICATION/STANDARD DATA | 80205-NAS344 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND ANNEALED CONDITION |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
AJJP | LEG THICKNESS | 0.094 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.250 INCHES NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
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