NSN 9540-01-494-7775 · NIIN 014947775 · FSC 9540
NO DASHES 9540014947775
In Stock
BEAM,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: B1-B AIRCRAFT
Technical characteristics
14 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 |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 1.500 |
| ABRY | LENGTH | FEET MINIMUM 10.000 AND FEET MAXIMUM 12.000 |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.080 |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.080 |
| AGAV | END ITEM IDENTIFICATION | B1-B AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | |
| AJJP | LEG THICKNESS | INCHES NOMINAL 0.080 |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 2.312 |
| BQJG | TOP FLANGE WIDTH | INCHES NOMINAL 3.750 |
| CRZC | RIGHT TOP INSIDE ANGLE | DEGREES NOMINAL 86.0 |
| HEAT | HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC SINGLE MATERIAL RESPONSE A-S-QQ-A-200 TO 3 |