At NSN Unlimited, we maintain a large database of parts 1566, 1M544, 4078, AMS-QQ-A-200 11, BAC1505 34393 with NSN 9540-00-148-4791 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Aluminum Co Of America, Boeing Company The, Alcoa Reynolds Metals Company, Sae International, 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: 9540-00-148-4791 |
Item Name: Beam Structural |
FSG: 95 Metal Bars Sheets and Shapes |
Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
NIIN: 001484791 |
NCB Code: USA (00) |
Manufacturers: Aluminum Co Of America , Boeing Company The , Alcoa Reynolds Metals Company , Sae International , Society Of Automotive Engineers Inc , The Boeing Company , Tracor Flight Systems Inc , Bae Systems Technology Solutions And Services Inc Dba Bae Systems Information And , General Dynamics Corporation , Federal Specifications |
Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
---|---|---|---|---|---|
1566 | 9540-00-148-4791 | beam structural | aluminum co of america | Avl | RFQ |
1M544 | 9540-00-148-4791 | beam structural | boeing company the | Avl | RFQ |
4078 | 9540-00-148-4791 | beam structural | alcoa reynolds metals company | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-00-148-4791 | beam structural | sae international | Avl | RFQ |
AMS-QQ-A-200 11 | 9540-00-148-4791 | beam structural | society of automotive engineers inc | Avl | RFQ |
BAC1505 34393 | 9540-00-148-4791 | beam structural | the boeing company | Avl | RFQ |
BAC1505-34393 | 9540-00-148-4791 | beam structural | society of automotive engineers inc | Avl | RFQ |
E731306 | 9540-00-148-4791 | beam structural | tracor flight systems inc | Avl | RFQ |
E731306 | 9540-00-148-4791 | beam structural | bae systems technology solutions and services inc dba bae systems information and | Avl | RFQ |
E731306 | 9540-00-148-4791 | beam structural | general dynamics corporation | Avl | RFQ |
QQ-A-200 11 | 9540-00-148-4791 | beam structural | society of automotive engineers inc | Avl | RFQ |
QQ-A-200 11 | 9540-00-148-4791 | beam structural | federal specifications | Avl | RFQ |
QQ-A-200 11 | 9540-00-148-4791 | beam structural | boeing company the | Avl | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
STRUCTURAL | AARN | FABRICATION METHODEXTRUDED |
STRUCTURAL | ABKW | OVERALL HEIGHT2 500 INCHES NOMINAL |
STRUCTURAL | ABRY | LENGTH10 000 FEET MINIMUM AND 12 000 FEET MAXIMUM |
STRUCTURAL | ADXR | LEFT SIDE TOP FLANGE THICKNESS0 125 INCHES NOMINAL |
STRUCTURAL | ADXS | RIGHT SIDE TOP FLANGE THICKNESS0 125 INCHES NOMINAL |
STRUCTURAL | AGTA | BASIC SHAPE STYLET SHAPE |
STRUCTURAL | AJJB | FIRST TIP RADIUS0 062 INCHES NOMINAL |
STRUCTURAL | AJJP | LEG THICKNESS0 188 INCHES NOMINAL |
STRUCTURAL | BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1 125 INCHES NOMINAL |
STRUCTURAL | BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1 125 INCHES NOMINAL |
STRUCTURAL | BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGELEG0 062 INCHES NOMINAL |
STRUCTURAL | BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGELEG0 062 INCHES NOMINAL |
STRUCTURAL | BQJG | TOP FLANGE WIDTH2 250 INCHES NOMINAL |
STRUCTURAL | BRFD | WEIGHT PER UNIT MEASURE0 870 POUNDS PER LINEAR FOOT |
STRUCTURAL | CMZY | FIRST TIP STYLEFULL RADIUS |
STRUCTURAL | CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL |
STRUCTURAL | CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPSIDENTICAL WFIRST TIP |
STRUCTURAL | CRZC | RIGHT TOP INSIDE ANGLE90 0 DEGREES NOMINAL |
STRUCTURAL | CSMZ | LEFT TOP INSIDE ANGLE90 0 DEGREES NOMINAL |
STRUCTURAL | HEAT | HEAT TREATMENTT-6 SOLUTION HEAT TREATED OR T-6511 SOLUTION HEAT TREATED |
STRUCTURAL | MATT | MATERIALALUMINUM ALLOY AMS-QQ-A-20011 ALLOY 7075 |
STRUCTURAL | ZZZT | NONDEFINITIVE SPECSTD DATA7075 ALLOY AND T6 TEMPER OR T6511 TEMPER |
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