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) | 00-237-9550 (002379550) |
| NCB Code | USA (00) |
| Manufacturer | Federal Specifications, Triumph Aerostructures Llc, Sae International, Society Of Automotive Engineers Inc, Aluminum Co Of America, Alcoa Reynolds Metals Company, International Light Metals Corp |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| QQA200-11 | federal specifications | beam structural | RFQ |
| CVC2070 | triumph aerostructures llc | beam structural | RFQ |
| AMS QQ A 200 11 | sae international | beam structural | RFQ |
| AMS QQ A 200 11 | society of automotive engineers inc | beam structural | RFQ |
| 23160 | aluminum co of america | beam structural | RFQ |
| 16985 | alcoa reynolds metals company | beam structural | RFQ |
| 14859 | international light metals corp | beam structural | 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 | 0.064 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.064 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.064 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 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 | 1.500 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.230 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| 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 |
| Relevant Components for NSN - 9540-00-237-9550, 9540002379550 | ||||
| 9540-01-071-0129 (9540010710129) | 9515-01-681-5985 (9515016815985) | 9540-00-526-2604 (9540005262604) | 9530-00-528-8713 (9530005288713) | |
| 9540-01-138-6475 (9540011386475) | 9510-00-952-5947 (9510009525947) | 9530-01-269-2176 (9530012692176) | 9520-00-950-5291 (9520009505291) | |
| 9540-00-060-5492 (9540000605492) | 9510-00-926-4695 (9510009264695) | 9510-00-866-1053 (9510008661053) | 9515-00-079-0992 (9515000790992) | |
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