NSN 9540-01-486-6271 · NIIN 014866271 · FSC 9540
NO DASHES 9540014866271
In Stock
BEAM,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: C-130 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 |
|---|---|---|
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 1.600 |
| ABRY | LENGTH | INCHES NOMINAL 1.750 |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.125 |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.125 |
| AGAV | END ITEM IDENTIFICATION | C-130 AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | |
| AJJP | LEG THICKNESS | INCHES NOMINAL 0.094 |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 0.781 |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 0.781 |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.031 |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.031 |
| BQJG | TOP FLANGE WIDTH | INCHES NOMINAL 1.750 |
| CMZY | FIRST TIP STYLE | |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | EXTRUSION, ALUMINUM |
| FEAT | SPECIAL FEATURES | MATERIAL 7075-T6 |
| MATT | MATERIAL | ALUMINUM ALLOY |