NSN 9535-01-531-7065 · NIIN 015317065 · FSC 9535
NO DASHES 9535015317065
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 |
|---|---|---|
| ALBY | USAGE DESIGN | AIRCRAFT |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| ABRY | LENGTH | INCHES NOMINAL 48.000 |
| ADVM | CROSS-SECTIONAL THICKNESS | INCHES NOMINAL 0.0900 |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | |
| AARN | FABRICATION METHOD | ROLLED |
| FEAT | SPECIAL FEATURES | MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC 1ST MATERIAL RESPONSE QQ-A-250 TO 4 |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| ABGL | WIDTH | INCHES NOMINAL 12.000 |