AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
| Item Name | Beam Structural |
| Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC) | 9540 Structural Shapes Nonferrous Base Metal |
| National Item Identification Number (NIIN) | 00-555-0819 (005550819) |
| NCB Code | USA (00) |
| Manufacturer | Textron Aviation Inc, Sae International, Society Of Automotive Engineers Inc, Boeing Company The, Bohn Aluminum And Brass Co, International Light Metals Corp, Hiller Aircraft Corporation, Northrop Grumman Systems Corporation, Reynolds Metals Co, Federal Specifications, Cessna Aircraft Company, Airforce-Navy Aeronautical Design Standard |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| S140 | textron aviation inc | beam structural | RFQ |
| AMS-QQ-A-200 11 | sae international | beam structural | RFQ |
| AMS10136-2001 | society of automotive engineers inc | beam structural | RFQ |
| 1325206 | boeing company the | beam structural | RFQ |
| 40290 | bohn aluminum and brass co | beam structural | RFQ |
| AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | RFQ |
| AMS10136-2001 | sae international | beam structural | RFQ |
| 18387 | international light metals corp | beam structural | RFQ |
| FS50102-2010 | hiller aircraft corporation | beam structural | RFQ |
| RY32009 | northrop grumman systems corporation | beam structural | RFQ |
| 6352 | reynolds metals co | beam structural | RFQ |
| QQ-A-200/11 | federal specifications | beam structural | RFQ |
| S140 | cessna aircraft company | beam structural | RFQ |
| AND10136-2001 | airforce-navy aeronautical design standard | beam structural | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.000 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.078 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.078 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJB | FIRST TIP RADIUS | 0.078 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.078 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 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 | 2.000 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.277 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CNBB | THIRD TIP RADIUS | 0.039 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
| CNQM | THIRD TIP STYLE | FULL RADIUS |
| 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 |
| Relevant Components for NSN - 9540-00-555-0819, 9540005550819 | ||||
| 9520-01-538-3805 (9520015383805) | 9530-00-247-5514 (9530002475514) | 9535-01-380-4829 (9535013804829) | 9530-01-496-8011 (9530014968011) | |
| 9540-01-428-9530 (9540014289530) | 9540-00-403-5155 (9540004035155) | 9515-01-614-8950 (9515016148950) | 9515-01-465-0340 (9515014650340) | |
| 9520-01-104-1132 (9520011041132) | 9530-00-596-9061 (9530005969061) | 9540-00-595-8549 (9540005958549) | 9530-00-236-0363 (9530002360363) | |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
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