| 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) | 00-006-5027 (000065027) |
| NCB Code | USA (00) |
| Manufacturer | Sae International, Society Of Automotive Engineers Inc, Lockheed Martin Corporation, Federal Specifications, Airforce-Navy Aeronautical Design Standard |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| AMS QQ A 200 11 | sae international | beam structural | RFQ |
| AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | RFQ |
| LS10138-1402-5 | lockheed martin corporation | beam structural | RFQ |
| QQ-A-200/11 | federal specifications | beam structural | RFQ |
| AND10138-1402 | airforce-navy aeronautical design standard | beam structural | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.500 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.078 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | Z SHAPE |
| AJJB | FIRST TIP RADIUS | 0.078 INCHES NOMINAL |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.078 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 | 0.078 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 1.000 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 1.000 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.318 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CMZZ | SECOND TIP RADIUS | 0.078 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-6511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11,ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6511 TEMPER |
| Relevant Components for NSN - 9540-00-006-5027, 9540000065027 | ||||
| 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