At NSN Unlimited, we maintain a large database of parts 1MA160D06-10256, 60-8960, AMS QQ A 200 11, AMS-QQ-A-200 11, QQ A 200 11 with NSN 9540-01-459-5950 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Federal Specifications, Boeing Company The, Society Of Automotive Engineers Inc, 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: 9540-01-459-5950 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 014595950 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications , Boeing Company The , Society Of Automotive Engineers Inc , Transtar Metals Corp , Sae International |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
1MA160D06-10256 | 9540-01-459-5950 | beam structural | federal specifications | Avl | RFQ |
1MA160D06-10256 | 9540-01-459-5950 | beam structural | boeing company the | Avl | RFQ |
1MA160D06-10256 | 9540-01-459-5950 | beam structural | society of automotive engineers inc | Avl | RFQ |
60-8960 | 9540-01-459-5950 | beam structural | society of automotive engineers inc | Avl | RFQ |
60-8960 | 9540-01-459-5950 | beam structural | transtar metals corp | Avl | RFQ |
60-8960 | 9540-01-459-5950 | beam structural | boeing company the | Avl | RFQ |
60-8960 | 9540-01-459-5950 | beam structural | federal specifications | Avl | RFQ |
AMS QQ A 200 11 | 9540-01-459-5950 | beam structural | sae international | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-459-5950 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-459-5950 | beam structural | boeing company the | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-01-459-5950 | beam structural | federal specifications | Avl | RFQ |
QQ A 200 11 | 9540-01-459-5950 | beam structural | federal specifications | Avl | RFQ |
QQ-A-200 11 | 9540-01-459-5950 | beam structural | society of automotive engineers inc | Avl | RFQ |
QQ-A-200 11 | 9540-01-459-5950 | beam structural | boeing company the | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AJJB | FIRST TIP RADIUS | 0.030 INCHES NOMINAL |
AJJP | LEG THICKNESS | 0.080 INCHES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, AMS-QQ-A-200/11, ALLOY 7075 |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.130 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.130 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.920 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.580 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | LOWER RADIUS |
CNBG | THIRD TIP INNER RADIUS | 0.030 INCHES NOMINAL |
CNBL | THIRD TIP OUTER RADIUS | 0.030 INCHES NOMINAL |
ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER T76511 |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
ZZZV | III FSC APPLICATION DATA | F-15I |
ABKW | OVERALL HEIGHT | 2.060 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.080 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.840 INCHES NOMINAL |
CNQM | THIRD TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.110 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.110 INCHES NOMINAL |
AARN | FABRICATION METHOD | EXTRUDED |
HEAT | HEAT TREATMENT | T-76511 SOLUTION HEAT TREATED |
AGTA | BASIC SHAPE STYLE | T SHAPE |
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