NSN 9540-01-543-4430 · NIIN 015434430 · FSC 9540
NO DASHES 9540015434430
In Stock
BEAM,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: C-5 AIRCRAFT
Technical characteristics
13 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 |
|---|---|---|
| BQJG | TOP FLANGE WIDTH | INCHES MINIMUM 4.058 AND INCHES MAXIMUM 4.126 |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | INCHES MINIMUM 0.084 AND INCHES MAXIMUM 0.096 |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | INCHES MINIMUM 0.084 AND INCHES MAXIMUM 0.096 |
| AGAV | END ITEM IDENTIFICATION | C-5 AIRCRAFT |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| AJJP | LEG THICKNESS | INCHES MINIMUM 0.044 AND INCHES MAXIMUM 0.056 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | T SECTION-FLANGED, C.M. |
| FEAT | SPECIAL FEATURES | BASIC T CONFIGURATION WITH FLANGED VERTICAL LEG |
| ABKW | OVERALL HEIGHT | INCHES MINIMUM 1.288 AND INCHES MAXIMUM 1.312 |
| AGTA | BASIC SHAPE STYLE | |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL SPEC SINGLE MATERIAL RESPONSE -IL-A-12545 |
| HEAT | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES MINIMUM 2.036 AND INCHES MAXIMUM 2.084 |