NSN 9540-01-334-2882 · NIIN 013342882 · FSC 9540
NO DASHES 9540013342882
In Stock
ANGLE,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: F-16 AIRCRAFT
Technical characteristics
19 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 | EXTRUDED |
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 2.000 |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 2.000 |
| ABRY | LENGTH | FEET MINIMUM 10.000 AND FEET MAXIMUM 12.000 |
| ADXL | LEFT SIDE FLANGE THICKNESS | INCHES NOMINAL 0.094 |
| AGAV | END ITEM IDENTIFICATION | F-16 AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | INCHES NOMINAL 0.250 |
| AJGP | BASE FLANGE THICKNESS | INCHES NOMINAL 0.094 |
| AJJB | FIRST TIP RADIUS | INCHES NOMINAL 0.094 |
| CMZY | FIRST TIP STYLE | |
| CMZZ | SECOND TIP RADIUS | INCHES NOMINAL 0.094 |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| CNQK | SECOND TIP STYLE | |
| CQHP | LEFT INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| HEAT | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 6061 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC SINGLE MATERIAL RESPONSE A-S-QQ-A-200 TO 8 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | TEMPER T6511 |