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) | 00-111-7573 (001117573) |
| NCB Code | USA (00) |
| Manufacturer | Aluminum Co Of America, Society Of Automotive Engineers Inc, Federal Specifications, Sae International, Bell Helicopter Textron Inc |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 29794 | aluminum co of america | beam structural | RFQ |
| AMS QQ A 200 3 | society of automotive engineers inc | beam structural | RFQ |
| QQ-A-200/3 | federal specifications | beam structural | RFQ |
| AMS QQ A 200 3 | sae international | beam structural | RFQ |
| 40-068-1 | bell helicopter textron inc | beam structural | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3,ALLOY 2024 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T3511 TEMPER |
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 0.312 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | Z SHAPE |
| AJJB | FIRST TIP RADIUS | 0.062 INCHES NOMINAL |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.031 INCHES NOMINAL |
| BPXN | WEB FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 0.562 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 0.812 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.120 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CWKK | RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
| Relevant Components for NSN - 9540-00-111-7573, 9540001117573 | ||||
| 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.
Request for Quote