NSN 9540-01-543-4432 · NIIN 015434432 · FSC 9540
NO DASHES 9540015434432
In Stock
BEAM,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: C-5 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 |
|---|---|---|
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES MINIMUM 2.034 AND INCHES MAXIMUM 2.086 |
| AGTA | BASIC SHAPE STYLE | |
| AJJP | LEG THICKNESS | INCHES MINIMUM 0.045 AND INCHES MAXIMUM 0.055 |
| AGAV | END ITEM IDENTIFICATION | C-5 AIRCRAFT |
| BQJG | TOP FLANGE WIDTH | INCHES MINIMUM 4.056 AND INCHES MAXIMUM 4.128 |
| ABKW | OVERALL HEIGHT | INCHES MINIMUM 1.288 AND INCHES MAXIMUM 1.312 |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | INCHES MINIMUM 0.085 AND INCHES MAXIMUM 0.095 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | T SECTION-CHEM MILL |
| FEAT | SPECIAL FEATURES | BASIC T CONFIGURATION WITH FLANGE ON VERTICAL LEG |
| HEAT | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ASSN STD SINGLE MATERIAL RESPONSE A-S 4139 |