NSN 9540-01-499-5415 · NIIN 014995415 · FSC 9540
NO DASHES 9540014995415
In Stock
BEAM,STRUCTURAL
Structural Shapes, Nonferrous Base Metal
Application: AIRCRAFT, GALAXY C-5
Technical characteristics
24 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 1.250 |
| ABRY | LENGTH | INCHES MAXIMUM 192.000 |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.200 |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | INCHES NOMINAL 0.200 |
| AGAV | END ITEM IDENTIFICATION | AIRCRAFT, GALAXY C-5 |
| AGTA | BASIC SHAPE STYLE | |
| AJJP | LEG THICKNESS | INCHES NOMINAL 0.070 |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 1.830 |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | INCHES NOMINAL 1.830 |
| 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 3.660 |
| CMZY | FIRST TIP STYLE | |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CRZC | RIGHT TOP INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| CSMZ | LEFT TOP INSIDE ANGLE | DEGREES NOMINAL 90.0 |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | "T" SECTION - EXTRUDED |
| FEAT | SPECIAL FEATURES | THE C-5 REQUIRES 243 FT/AC; MAXIMUM LENGTH IS 192.000 INCH |
| HEAT | HEAT TREATMENT | T-76511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY 7055 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MFR REF SINGLE MATERIAL RESPONSE ST-04-118 |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |