NSN 9540-01-687-5538 · NIIN 016875538 · FSC 9540
NO DASHES 9540016875538
In Stock
ANGLE,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: C-130J-30 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 |
|---|---|---|
| FEAT | SPECIAL FEATURES | QQ-A-362 SUPERSEEDED BY QQ-A-250/5 |
| AGTA | BASIC SHAPE STYLE | |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | INCHES NOMINAL 0.125 |
| AJGM | OUTER RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | INCHES NOMINAL 0.125 |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 0.750 |
| ADXL | LEFT SIDE FLANGE THICKNESS | INCHES NOMINAL 0.040 |
| AGAV | END ITEM IDENTIFICATION | C-130J-30 AIRCRAFT |
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 0.750 |
| HEAT | HEAT TREATMENT | T-3 SOLUTION HEAT TREATED |
| CMZY | FIRST TIP STYLE | |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CQHP | LEFT INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SHEET METAL-ANGLES 90 DEGREE |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC 1ST MATERIAL RESPONSE QQ-A-250 TO 5 |
| AJGP | BASE FLANGE THICKNESS | INCHES NOMINAL 0.040 |