NSN 9540-01-543-2924 · NIIN 015432924 · FSC 9540
NO DASHES 9540015432924
In Stock
ANGLE,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: C-5 AIRCRAFT
Technical characteristics
12 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 |
|---|---|---|
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ANGLE UNEQUAL KEG EXTRUDED |
| AGTA | BASIC SHAPE STYLE | |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | INCHES MINIMUM 0.104 AND INCHES MAXIMUM 0.136 |
| ABKW | OVERALL HEIGHT | INCHES MINIMUM 2.096 AND INCHES MAXIMUM 2.144 |
| ABMK | OVERALL WIDTH | INCHES MINIMUM 2.401 AND INCHES MAXIMUM 2.449 |
| ADXL | LEFT SIDE FLANGE THICKNESS | INCHES MINIMUM 0.118 AND INCHES MAXIMUM 0.132 |
| AGAV | END ITEM IDENTIFICATION | C-5 AIRCRAFT |
| FEAT | SPECIAL FEATURES | 90 DEGREE ANGLE |
| AJGP | BASE FLANGE THICKNESS | INCHES MINIMUM 0.118 AND INCHES MAXIMUM 0.132 |
| HEAT | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC 1ST MATERIAL RESPONSE QQ-A-200 TO 11 |