| 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) | 01-162-5823 (011625823) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The, Society Of Automotive Engineers Inc, Sae International, Airforce-Navy Aeronautical Design Standard, Federal Specifications |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| 1MA160006-10117 | boeing company the | beam structural | 76301 | RFQ |
| 1MA160D06-10117 | boeing company the | beam structural | 76301 | RFQ |
| AMS QQ A 200 15 | society of automotive engineers inc | beam structural | 81343 | RFQ |
| AMS-QQ-A-200 15 | sae international | beam structural | 0u583 | RFQ |
| AND10136-2409 | airforce-navy aeronautical design standard | beam structural | 99237 | RFQ |
| QQ-A-200/11 | federal specifications | beam structural | 81348 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.000 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJB | FIRST TIP RADIUS | 0.188 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.188 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.188 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.500 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.978 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CNBB | THIRD TIP RADIUS | 0.094 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-76511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/15,ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T76511 TEMPER |
| Relevant Components for NSN - 9540-01-162-5823, 9540011625823 | ||||
| 9510-00-287-2940 (9510002872940) | 9515-00-640-4320 (9515006404320) | 9510-00-951-0303 (9510009510303) | 9540-00-148-4818 (9540001484818) | |
| 9530-00-187-0174 (9530001870174) | 9510-00-056-1926 (9510000561926) | 9520-00-052-5388 (9520000525388) | 9515-01-679-1497 (9515016791497) | |
| 9535-01-531-7125 (9535015317125) | 9540-01-087-1310 (9540010871310) | 9540-01-071-3524 (9540010713524) | 9510-00-542-2444 (9510005422444) | |
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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