NSN 9535-01-531-7799 · NIIN 015317799 · FSC 9535
NO DASHES 9535015317799
In Stock
SHEET,METAL
Plate, Sheet, Strip, and Foil; Nonferrous Base Metal
Application: FUSELAGE F4F JET AIRCRAFT
Technical characteristics
13 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 |
|---|---|---|
| AARN | FABRICATION METHOD | ROLLED |
| ABGL | WIDTH | INCHES NOMINAL 6.000 |
| ABRY | LENGTH | INCHES NOMINAL 36.000 |
| CQHQ | MINIMUM YIELD STRENGTH | POUNDS PER SQUARE INCH 40000 |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
| CQBC | MINIMUM TENSILE STRENGTH | POUNDS PER SQUARE INCH 61000 |
| AGTA | BASIC SHAPE STYLE | |
| ALBY | USAGE DESIGN | AIRCRAFT |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC 1ST MATERIAL RESPONSE QQ-A-250 TO 5 |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| ADVM | CROSS-SECTIONAL THICKNESS | INCHES NOMINAL 0.1250 |
| 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 2.5 PERCENT OF COMPOSITE THICKNESS OR 2.0 PERCENT OF FINISHED SHEET THICKNESS |
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-CDT3-0,125X6X36 | 81343 |
| AMS-QQ-A-250/5 | 81343 |
| AMS-QQ-A-250/5-T3-0.125X6X36 | 81343 |
| AMS-QQ-A-250/5 | 0U583 |
| AMS-QQ-A-250/5-T3-0.125X6X36 | 0U583 |