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) | 00-008-2215 (000082215) |
| NCB Code | USA (00) |
| Manufacturer | Airforce-Navy Aeronautical Design Standard, Society Of Automotive Engineers Inc, Federal Specifications, Lockheed Martin Corporation, Sae International |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| AND10138-1004 | airforce-navy aeronautical design standard | beam structural | RFQ |
| AMS-QQA200-3 | society of automotive engineers inc | beam structural | RFQ |
| QQA200-3 | federal specifications | beam structural | RFQ |
| LS10138-1004-2 | lockheed martin corporation | beam structural | RFQ |
| AMS-QQA200-3 | sae international | 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 | 0.063 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | Z SHAPE |
| AJJB | FIRST TIP RADIUS | 0.063 INCHES NOMINAL |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXN | WEB FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 0.750 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 0.750 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.186 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CMZZ | SECOND TIP RADIUS | 0.063 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-3511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T3511 TEMPER |
| Relevant Components for NSN - 9540-00-008-2215, 9540000082215 | ||||
| 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) | |
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