NSN 9540-01-523-9583 · NIIN 015239583 · FSC 9540
NO DASHES 9540015239583
In Stock
ANGLE,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: C5 AIRCRAFT
Technical characteristics
17 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 |
|---|---|---|
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC SINGLE MATERIAL RESPONSE A-S-QQ-A-200 TO 11 |
| AARN | FABRICATION METHOD | EXTRUDED |
| AGAV | END ITEM IDENTIFICATION | C5 AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | INCHES NOMINAL 0.094 |
| AJGP | BASE FLANGE THICKNESS | INCHES MINIMUM 0.064 AND INCHES MAXIMUM 0.076 |
| CMZY | FIRST TIP STYLE | |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER T6511 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | DRAWING: ANGLE EXTRUDED |
| ABKW | OVERALL HEIGHT | INCHES MINIMUM 1.736 AND INCHES MAXIMUM 1.764 |
| ABMK | OVERALL WIDTH | INCHES MINIMUM 1.985 AND INCHES MAXIMUM 2.013 |
| ADXL | LEFT SIDE FLANGE THICKNESS | INCHES MINIMUM 0.064 AND INCHES MAXIMUM 0.076 |
| HEAT | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| CQHP | LEFT INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |