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) | 00-595-8597 (005958597) |
| NCB Code | USA (00) |
| Manufacturer | Aluminum Co Of America, Society Of Automotive Engineers Inc, Northrop Grumman Systems Corporation, Sae International, Federal Specifications |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 38355 | aluminum co of america | beam structural | RFQ |
| AMS QQA200 11 | society of automotive engineers inc | beam structural | RFQ |
| 120001 | northrop grumman systems corporation | beam structural | RFQ |
| AMS-QQA200-11 | sae international | beam structural | RFQ |
| QQA200-11 | federal specifications | beam structural | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXN | WEB FLANGE THICKNESS | 0.064 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 0.750 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 0.938 INCHES NOMINAL |
| BQKQ | OUTER RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE | 0.125 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.310 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | FLANGE LEFT DOWNWARD W/ SQUARE END AND INNER AND OUTER CORNER RADII |
| CNNN | FIRST TIP INNER CORNER RADIUS | 0.125 INCHES NOMINAL |
| CNNP | SECOND TIP INNER CORNER RADIUS | 0.125 INCHES NOMINAL |
| CNNS | FIRST TIP OUTER CORNER RADIUS | 0.125 INCHES NOMINAL |
| CNPS | FIRST TIP THICKNESS | 0.064 INCHES NOMINAL |
| CNPT | SECOND TIP THICKNESS | 0.064 INCHES NOMINAL |
| CNPY | FIRST TIP FLANGE HEIGHT | 0.250 INCHES NOMINAL |
| CNPZ | SECOND TIP FLANGE HEIGHT | 0.189 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| CNQK | SECOND TIP STYLE | FLANGE RIGHT UPWARD WITH SQUARE END,INNER CORNER RADIUS,AND SQUARE OUTER CORNER |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CWKK | RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.875 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.064 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | Z SHAPE |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.064 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| Relevant Components for NSN - 9540-00-595-8597, 9540005958597 | ||||
| 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