NSN 9535-00-230-7578 · NIIN 002307578 · FSC 9535
NO DASHES 9535002307578
In Stock
SHEET,METAL
Plate, Sheet, Strip, and Foil; Nonferrous Base Metal
Application: F-16 AIRCRAFT
Technical characteristics
14 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 |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | F-16 AIRCRAFT |
| AARN | FABRICATION METHOD | ROLLED |
| ADVM | CROSS-SECTIONAL THICKNESS | INCHES NOMINAL 0.080 |
| ABGL | WIDTH | INCHES NOMINAL 48.000 |
| ABRY | LENGTH | FEET NOMINAL 12.000 |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC SINGLE MATERIAL RESPONSE A-S-QQ-A-250 TO 4 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | TEMPER T3 |
| ALBY | USAGE DESIGN | AIRCRAFT |
| BRFD | WEIGHT PER UNIT MEASURE | POUNDS PER SQUARE FOOT 1.150 |
| CQBC | MINIMUM TENSILE STRENGTH | POUNDS PER SQUARE INCH 64000 |
| CQHQ | MINIMUM YIELD STRENGTH | POUNDS PER SQUARE INCH 42000 |
| HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
| AGTA | BASIC SHAPE STYLE |