Item Name | Sheet Metal |
Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
Federal Supply Class (FSC) | 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
National Item Identification Number (NIIN) | 01-532-0513 (015320513) |
NCB Code | USA (01) |
Manufacturer | Sae International, Society Of Automotive Engineers Inc |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
AMS-QQ-A-250 8-H34-0.040X12X48 | sae international | sheet metal | RFQ |
AMS-QQ-A-250 8-CDH34-0 04X12X48 | society of automotive engineers inc | sheet metal | RFQ |
AMS-QQ-A-250 8-H34-0.040X12X48 | society of automotive engineers inc | sheet metal | RFQ |
AMS-QQ-A-250 8 | society of automotive engineers inc | sheet metal | RFQ |
AMS-QQ-A-250 8 | sae international | sheet metal | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
ADVM | Cross-Sectional Thickness | 0.0400 INCHES NOMINAL |
MATT | Material | ALUMINUM ALLOY 5052 |
HEAT | Heat Treatment | H-34 STRAIN HARDENED |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 48.000 INCHES NOMINAL |
ABGL | Width | 12.000 INCHES NOMINAL |
AGAV | End Item Identification | FUSELAGE, F4F JET AIRCRAFT |
CQBC | Minimum Tensile Strength | 34000 POUNDS PER SQUARE INCH |
MDCL | Material Document And Classification | QQ-A-250/8 FED SPEC 1ST MATERIAL RESPONSE |
ALBY | Usage Design | AIRCRAFT |
MRC | Decoded Requirement | Clear Text Reply |
FEAT | Special Features | MAXIMUM TENSILE STRENGTH 41000.0 POUNDS PER SQUARE INCH |
AARN | Fabrication Method | ROLLED |
Relevant Components for NSN - 9535-01-532-0513, 9535015320513 | ||||
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) | |
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