At NSN Unlimited, we maintain a large database of parts 1418898-7200, 67950, AMS QQ A 200 11, AMS-QQ-A-200 11, QQ A 277 with NSN 9540-00-529-9672 used in civil and defense applications for the aerospace, marine, and commercial manufactured by Federal Specifications, Boeing Company The, Aluminum Co Of America, 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: 9540-00-529-9672 |
| Item Name: Beam Structural |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9540 Structural Shapes Nonferrous Base Metal |
| NIIN: 005299672 |
| NCB Code: USA (00) |
| Manufacturers: Federal Specifications , Boeing Company The , Aluminum Co Of America , Society Of Automotive Engineers Inc , Sae International |
| Part No | NSN | Item Name | Manufacturer | QTY | RFQ |
|---|---|---|---|---|---|
| 1418898-7200 | 9540-00-529-9672 | beam structural | federal specifications | Avl | RFQ |
| 1418898-7200 | 9540-00-529-9672 | beam structural | boeing company the | Avl | RFQ |
| 1418898-7200 | 9540-00-529-9672 | beam structural | aluminum co of america | Avl | RFQ |
| 67950 | 9540-00-529-9672 | beam structural | boeing company the | Avl | RFQ |
| 67950 | 9540-00-529-9672 | beam structural | aluminum co of america | Avl | RFQ |
| 67950 | 9540-00-529-9672 | beam structural | federal specifications | Avl | RFQ |
| AMS QQ A 200 11 | 9540-00-529-9672 | beam structural | society of automotive engineers inc | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-00-529-9672 | beam structural | aluminum co of america | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-00-529-9672 | beam structural | boeing company the | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-00-529-9672 | beam structural | federal specifications | Avl | RFQ |
| AMS-QQ-A-200 11 | 9540-00-529-9672 | beam structural | sae international | Avl | RFQ |
| QQ A 277 | 9540-00-529-9672 | beam structural | federal specifications | Avl | RFQ |
| QQ-A-200 11 | 9540-00-529-9672 | beam structural | federal specifications | Avl | RFQ |
| S1418898 | 9540-00-529-9672 | beam structural | federal specifications | Avl | RFQ |
| S1418898 | 9540-00-529-9672 | beam structural | boeing company the | Avl | RFQ |
| S1418898 | 9540-00-529-9672 | beam structural | aluminum co of america | Avl | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.500 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJB | FIRST TIP RADIUS | 0.063 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.125 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.875 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.875 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 |
| BQJG | TOP FLANGE WIDTH | 1.750 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.470 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | FULL RADIUS |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11, ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
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