NSN 9540-01-616-7168 · NIIN 016167168 · FSC 9540
NO DASHES 9540016167168
In Stock
BEAM,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: C-17A 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 |
|---|---|---|
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 1.250 |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.094 |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.094 |
| AGAV | END ITEM IDENTIFICATION | C-17A AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.125 |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | INCHES NOMINAL 0.125 |
| BQJG | TOP FLANGE WIDTH | INCHES NOMINAL 2.000 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | BEAM, STRUCTURAL |
| FEAT | SPECIAL FEATURES | TEMPER T3511 |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC 1ST MATERIAL RESPONSE QQ-A-430, ALLOY 2024 |