| 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) | 01-187-4994 (011874994) |
| NCB Code | USA (01) |
| Manufacturer | Boeing Company The, Society Of Automotive Engineers Inc, Transtar Metals Corp, Sae International, Federal Specifications |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 1MA160D06-10415 | boeing company the | beam structural | RFQ |
| AMS-QQ-A-200 15 | society of automotive engineers inc | beam structural | RFQ |
| 60-13818 | transtar metals corp | beam structural | RFQ |
| AMS QQ A 200 15 | sae international | beam structural | RFQ |
| QQ A 200 15 | federal specifications | beam structural | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.500 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.600 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.600 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.250 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.770 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.605 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.190 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.190 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 4.375 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 3.737 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBD | FIRST TIP INNER RADIUS | 0.032 INCHES NOMINAL |
| CNBJ | FIRST TIP OUTER RADIUS | 0.032 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| 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,QQ-A-200/15,ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | T76511 TEMPER |
| Relevant Components for NSN - 9540-01-187-4994, 9540011874994 | ||||
| 9515-00-952-8574 (9515009528574) | 9510-00-595-8306 (9510005958306) | 9505-01-082-8812 (9505010828812) | 9535-01-644-5938 (9535016445938) | |
| 9515-00-287-2924 (9515002872924) | 9505-00-813-5321 (9505008135321) | 9530-01-241-2003 (9530012412003) | 9535-01-353-5540 (9535013535540) | |
| 9530-00-055-6696 (9530000556696) | 9530-01-497-1224 (9530014971224) | 9515-01-681-0019 (9515016810019) | 9540-01-296-9127 (9540012969127) | |
The only independent
“We Proudly Support Intrepid Fallen Heroes Fund that serves United States Military Personal experiencing the Invisible Wounds of War : Traumatic Brain Injury (TBI) and Post Traumatic Stress (PTS). Please visit website (www.fallenheroesfund.org) and help in their valiant effort”.
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