NSN 9535-00-232-0455 of Sheet Metal - Parts Details
| Alternative NSN: 9535002320455 |
| Item Name: Sheet Metal |
| FSG: 95 Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC): 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
| NIIN: 002320455 |
| NCB Code: USA (00) |
| Manufacturers: Federal Specifications Promulgat , Sae International , Society Of Automotive Engineers Inc |
ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Check out high demanding part numbers QQ-A-250 5, AMS-QQ-A-250 5 under NSN 9535-00-232-0455 of Sheet Metal manufactured by Federal Specifications Promulgat, Sae International, Society Of Automotive Engineers Inc.
Federal Supply Class of NSN 9535-00-232-0455 is FSC 9535 contains part details of Plate Sheet Strip and Foil Nonferrous Base Metal. Quote for your desired part numbers.
Part Number's List for NSN 9535-00-232-0455, 9535002320455
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Part No Manufacturer Item Name QTY RFQ QQ-A-250 5 Federal Specifications Promulgat sheet metal Avl RFQ AMS-QQ-A-250 5 Sae International sheet metal Avl RFQ AMS-QQ-A-250 5 Society Of Automotive Engineers Inc sheet metal Avl RFQ
Characteristics Data of NSN 9535002320455MRC Criteria Characteristic AARN FABRICATION METHOD ROLLED ABGL WIDTH 48.000 INCHES NOMINAL ABRY LENGTH 12.000 FEET NOMINAL ADVM CROSS-SECTIONAL THICKNESS 0.0630 INCHES NOMINAL AGAV III END ITEM IDENTIFICATION B-1B AIRCRAFT AGTA BASIC SHAPE STYLE SOLID AGXW PHYSICAL FORM FLAT STOCK ALBY III USAGE DESIGN AIRCRAFT AQQR EDGE TYPE SHEARED BMNH CLADDING THICKNESS 0.0016 INCHES BOTH SIDES BRFD WEIGHT PER UNIT MEASURE 0.907 POUNDS PER SQUARE FOOT CQBC MINIMUM TENSILE STRENGTH 66000 POUNDS PER SQUARE INCH CQHQ MINIMUM YIELD STRENGTH 50000 POUNDS PER SQUARE INCH HEAT HEAT TREATMENT T-361 SOLUTION HEAT TREATED MATT MATERIAL ALUMINUM ALLOY 2024 MDCL MATERIAL DOCUMENT AND CLASSIFICATION AMS-QQ-A-250/5 ASSN STD SINGLE MATERIAL RESPONSE ZZZT NONDEFINITIVE SPEC/STD DATA 2024 ALLOY AND T361 TEMPER
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | 48.000 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0630 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | B-1B AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| AGXW | PHYSICAL FORM | FLAT STOCK |
| ALBY | III USAGE DESIGN | AIRCRAFT |
| AQQR | EDGE TYPE | SHEARED |
| BMNH | CLADDING THICKNESS | 0.0016 INCHES BOTH SIDES |
| BRFD | WEIGHT PER UNIT MEASURE | 0.907 POUNDS PER SQUARE FOOT |
| CQBC | MINIMUM TENSILE STRENGTH | 66000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 50000 POUNDS PER SQUARE INCH |
| HEAT | HEAT TREATMENT | T-361 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-250/5 ASSN STD SINGLE MATERIAL RESPONSE |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T361 TEMPER |