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) | 01-119-8475 (011198475) |
NCB Code | USA (01) |
Manufacturer | Society Of Automotive Engineers Inc, Airforce-Navy Aeronautical Design Standard, Sae International, Nimikkeistokeskus Ncb Finland, Federal Specifications, Boeing Company The |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | RFQ |
AND10139-0604 | airforce-navy aeronautical design standard | beam structural | RFQ |
AMS-QQ-A-200 11 | sae international | beam structural | RFQ |
10164586 | nimikkeistokeskus ncb finland | beam structural | RFQ |
QQ-A-200/11 | federal specifications | beam structural | RFQ |
1MA180D03-10034 | boeing company the | beam structural | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 0.750 INCHES NOMINAL |
ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | Z SHAPE |
AJJB | FIRST TIP RADIUS | 0.063 INCHES NOMINAL |
BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.063 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 | 0.063 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 0.375 INCHES NOMINAL |
BQJH | BOTTOM FLANGE WIDTH | 0.750 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.139 POUNDS PER LINEAR FOOT |
CMZY | FIRST TIP STYLE | LOWER RADIUS |
CMZZ | SECOND TIP RADIUS | 0.063 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 7075 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
ZZZK | SPECIFICATION/STANDARD DATA | 76301-1MA180 MANUFACTURERS STANDARD |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T6511 TEMPER |
Relevant Components for NSN - 9540-01-119-8475, 9540011198475 | ||||
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