| 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) | 00-005-6322 (000056322) |
| NCB Code | USA (00) |
| Manufacturer | Lockheed Martin Corporation, Sae International, International Light Metals Corp, Federal Specifications, Society Of Automotive Engineers Inc |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| LS32742-1 | lockheed martin corporation | beam structural | RFQ |
| AMS QQ A 200 11 | sae international | beam structural | RFQ |
| 54455 | international light metals corp | 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 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.540 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.063 INCHES NOMINAL |
| ALBY | USAGE DESIGN | STRUCTURAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.168 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.312 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.480 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.377 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | SQUARE END |
| 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-6511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMNIUM ALLOY AMS-QQ-A-200/11,ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6511 TEMPER |
| Relevant Components for NSN - 9540-00-005-6322, 9540000056322 | ||||
| 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