At NSN Unlimited, we maintain a large database of parts 1MA160B04-10551, AMS QQ A 200 3, AMS-QQ-A-200 3, ASTM B221, QQ-A-200 3 with NSN 9540-01-363-6177 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Federal Specifications, Boeing Company The, Society Of Automotive Engineers Inc, Sae International, American Society For Testing And. 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: 9540-01-363-6177 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 013636177 |
NCB Code: USA (01) |
Manufacturers: Federal Specifications , Boeing Company The , Society Of Automotive Engineers Inc , Sae International , American Society For Testing And |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
1MA160B04-10551 | 9540-01-363-6177 | beam structural | federal specifications | Avl | RFQ |
1MA160B04-10551 | 9540-01-363-6177 | beam structural | boeing company the | Avl | RFQ |
1MA160B04-10551 | 9540-01-363-6177 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS QQ A 200 3 | 9540-01-363-6177 | beam structural | society of automotive engineers inc | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-363-6177 | beam structural | federal specifications | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-363-6177 | beam structural | boeing company the | Avl | RFQ |
AMS-QQ-A-200 3 | 9540-01-363-6177 | beam structural | sae international | Avl | RFQ |
ASTM B221 | 9540-01-363-6177 | beam structural | boeing company the | Avl | RFQ |
ASTM B221 | 9540-01-363-6177 | beam structural | american society for testing and | Avl | RFQ |
ASTM B221 | 9540-01-363-6177 | beam structural | society of automotive engineers inc | Avl | RFQ |
ASTM B221 | 9540-01-363-6177 | beam structural | federal specifications | Avl | RFQ |
QQ-A-200 3 | 9540-01-363-6177 | beam structural | society of automotive engineers inc | Avl | RFQ |
QQ-A-200 3 | 9540-01-363-6177 | beam structural | federal specifications | Avl | RFQ |
QQ-A-200 3 | 9540-01-363-6177 | beam structural | boeing company the | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 2.250 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.063 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 |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CRZC | RIGHT TOP INSIDE ANGLE | 91.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | T-8511 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3, ALLOY 2024 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T8511 TEMPER |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.871 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE END |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.879 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 1.750 INCHES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 89.0 DEGREES NOMINAL |
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