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) | 00-954-9687 (009549687) |
NCB Code | USA (00) |
Manufacturer | Northrop Grumman Systems Corporation, Aluminum Co Of America, Society Of Automotive Engineers Inc, Transtar Metals Corp, Sae International, Federal Specifications, American Society For Testing |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
89V1074 | northrop grumman systems corporation | beam structural | RFQ |
62248 | aluminum co of america | beam structural | RFQ |
AMS-QQ-A-200 3 | society of automotive engineers inc | beam structural | RFQ |
60-11170 | transtar metals corp | beam structural | RFQ |
AMS-QQ-A-200 3 | sae international | beam structural | RFQ |
60-6452 | transtar metals corp | beam structural | RFQ |
QQ-A-200/3 | federal specifications | beam structural | RFQ |
PA18851 | transtar metals corp | beam structural | RFQ |
ASTM B221 | american society for testing | beam structural | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 2.313 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.064 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.064 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.064 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.312 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.313 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.063 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.063 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.625 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.370 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-4 SOLUTION HEAT TREATED |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3,ALLOY 2024 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T4 TEMPER AND T3511 TEMPER |
Relevant Components for NSN - 9540-00-954-9687, 9540009549687 | ||||
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) | |
“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