NSN 9535-01-532-0308 · NIIN 015320308 · FSC 9535
NO DASHES 9535015320308
In Stock
SHEET,METAL
Plate, Sheet, Strip, and Foil; Nonferrous Base Metal
Application: FUSELAGE F4F JET AIRCRAFT
Technical characteristics
11 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| HEAT | HEAT TREATMENT | O-ANNEALED |
| ABRY | LENGTH | INCHES NOMINAL 36.000 |
| FEAT | SPECIAL FEATURES | THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS; MAXIMUM TENSILE STRENGTH 30000.0 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000.0 POUNDS PER SQUARE INCH |
| AGTA | BASIC SHAPE STYLE | |
| ABGL | WIDTH | INCHES NOMINAL 6.000 |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AARN | FABRICATION METHOD | ROLLED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC 1ST MATERIAL RESPONSE QQ-A-250 TO 5 |
| ALBY | USAGE DESIGN | AIRCRAFT |
| ADVM | CROSS-SECTIONAL THICKNESS | INCHES NOMINAL 0.0500 |
Cross-references
5 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.
| Manufacturer part number | CAGE |
|---|---|
| AMS-QQ-A-250/5-CD0-0,05X6X36 | 81343 |
| AMS-QQ-A-250/5 | 81343 |
| AMS-QQ-A-250/5-O-0.050X6X36 | 81343 |
| AMS-QQ-A-250/5 | 0U583 |
| AMS-QQ-A-250/5-O-0.050X6X36 | 0U583 |