NSN - 9540-00-148-4791, 9540001484791 of Beam Structural
Aviation Axis stocks 1566, 1M544, 4078, AMS-QQ-A-200 11, AMS QQ A 200 11 - Beam Structural made by Aluminum Co Of America, Monogram Aerospace Fasteners Inc, Alcoa Reynolds Metals Company, Society Of Automotive Engineers Inc, Sae International with 9540-00-148-4791. Owned and operated by ASAP Semiconductor, we have access to over 2 billion new and after-market parts applicable within the aerospace and defense industries. All our parts are shipped using our premier shipping and supply chain. We offer short lead-times and some of the fastest shipping times in the industry. We are well-equipped to handle any customer situation - including AOG. Submit an RFQ today and expect a response within 15 minutes or less. ASAP - the evolution of purchasing.
| Alternative NSN: 9540-00-148-4791 |
| Item Name: Beam Structural |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 001484791 |
| NCB Code: USA (00) |
| Manufacturers: Alcoa Reynolds Metals Company, Aluminum Co Of America, Bae Systems Technology Solutions And Services Inc Dba Bae Systems Information And, Boeing Aircraft, Federal Specifications, General Dynamics Corporation, Monogram Aerospace Fasteners Inc, Sae International, Society Of Automotive Engineers Inc, Tracor Flight Systems Inc |
| Part No | Manufacturer | Item Name | QTY | RFQ |
|---|---|---|---|---|
| 1566 | aluminum co of america | beam structural | Avl | RFQ |
| 1M544 | monogram aerospace fasteners inc | beam structural | Avl | RFQ |
| 4078 | alcoa reynolds metals company | beam structural | Avl | RFQ |
| AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | Avl | RFQ |
| AMS QQ A 200 11 | sae international | beam structural | Avl | RFQ |
| BAC1505 34393 | boeing aircraft | beam structural | Avl | RFQ |
| E731306 | tracor flight systems inc | beam structural | Avl | RFQ |
| E731306 | bae systems technology solutions and services inc dba bae systems information and | beam structural | Avl | RFQ |
| E731306 | general dynamics corporation | beam structural | Avl | RFQ |
| QQ-A-200 11 | federal specifications | beam structural | Avl | RFQ |
Technical Characteristics of NSN 9540001484791
| 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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