| 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) | 00-241-9373 (002419373) |
| NCB Code | USA (00) |
| Manufacturer | Federal Specifications, Boeing Company The, Society Of Automotive Engineers Inc, Sae International, Airforce-Navy Aeronautical Design Standard |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| QQA200-11 | federal specifications | beam structural | 81348 | RFQ |
| 1468513 | boeing company the | beam structural | 88277 | RFQ |
| AMS-QQA200-11 | society of automotive engineers inc | beam structural | 81343 | RFQ |
| AMS-QQA200-11 | sae international | beam structural | 0u583 | RFQ |
| AND10136-1605 | airforce-navy aeronautical design standard | beam structural | 99237 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.375 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJB | FIRST TIP RADIUS | 0.094 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.094 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.875 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.875 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 | 1.750 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.348 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CNBB | THIRD TIP RADIUS | 0.047 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
| CNQM | THIRD TIP STYLE | FULL RADIUS |
| 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 7075 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T6 TEMPER |
| Relevant Components for NSN - 9540-00-241-9373, 9540002419373 | ||||
| 9510-00-954-8048 (9510009548048) | 9515-01-081-1397 (9515010811397) | 9515-00-204-4616 (9515002044616) | 9540-01-271-2603 (9540012712603) | |
| 9535-01-570-0544 (9535015700544) | 9520-01-554-3985 (9520015543985) | 9530-00-528-8724 (9530005288724) | 9510-01-432-7478 (9510014327478) | |
| 9540-01-265-1979 (9540012651979) | 9540-00-910-8165 (9540009108165) | 9530-00-059-6681 (9530000596681) | 9515-00-580-5527 (9515005805527) | |
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.
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