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) | 00-006-8483 (000068483) |
| NCB Code | USA (00) |
| Manufacturer | Airforce-Navy Aeronautical Design Standard, Sae International, Federal Specifications, Society Of Automotive Engineers Inc, Lockheed Martin Corporation |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| AND10138-1003 | airforce-navy aeronautical design standard | beam structural | RFQ |
| AMS-QQ-A-200 11 | sae international | beam structural | RFQ |
| QQ-A-200/11 | federal specifications | beam structural | RFQ |
| AMS QQ A 200 11 | society of automotive engineers inc | beam structural | RFQ |
| LS10138-1003-5 | lockheed martin corporation | 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 | 0.050 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | Z SHAPE |
| AJJB | FIRST TIP RADIUS | 0.050 INCHES NOMINAL |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.050 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.094 INCHES NOMINAL |
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.094 INCHES NOMINAL |
| BPXN | WEB FLANGE THICKNESS | 0.050 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 0.750 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 0.750 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.148 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CMZZ | SECOND TIP RADIUS | 0.050 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| CNQK | SECOND TIP STYLE | UPPER RADIUS |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CWKK | RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11,ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6511 TEMPER |
| Relevant Components for NSN - 9540-00-006-8483, 9540000068483 | ||||
| 9510-00-224-1673 (9510002241673) | 9505-00-541-9654 (9505005419654) | 9540-01-353-5127 (9540013535127) | 9515-66-151-1706 (9515661511706) | |
| 9515-00-153-3357 (9515001533357) | 9535-01-012-2441 (9535010122441) | 9520-01-694-5689 (9520016945689) | 9510-01-484-4625 (9510014844625) | |
| 9530-00-993-4137 (9530009934137) | 9515-00-153-3227 (9515001533227) | 9515-01-555-3938 (9515015553938) | 9530-00-060-5594 (9530000605594) | |
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