NSN 1640-01-536-1305 · NIIN 015361305 · FSC 1640
NO DASHES 1640015361305
In Stock
WIRE ROPE ASSEMBLY,SINGLE LEG,AV
Aircraft Control Cable Products
Application: C-17A 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 |
|---|---|---|
| BZQQ | BREAKING STRENGTH | POUNDS (LB) NOMINAL 500.0 |
| TEST | TEST DATA DOCUMENT | DRAWING (THIS IS THE BASIC GOVERNING DRAWING, SUCH AS A CONTRACTOR DRAWING, ORIGINAL EQUIPMENT MANUFACTURER DRAWING, ETC.; EXCLUDES ANY SPECIFICATION, STANDARD OR OTHER DOCUMENT THAT MAY BE REFERENCED IN A BASIC GOVERNING DRAWING) 84256-LT1504 |
| ABHP | OVERALL LENGTH | FEET NOMINAL 0.500 |
| ABMZ | DIAMETER | ROPE INCHES NOMINAL 0.062 |
| AGAV | END ITEM IDENTIFICATION | C-17A AIRCRAFT |
| AMXF | ATTACHMENT STYLE | |
| MATT | MATERIAL | OVERALL STEEL CORROSION RESISTING |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | TERMINAL ATTACHMENT SECOND END MIL SPEC 1ST TREATMENT RESPONSE -IL-A-8625 AND FED SPEC 2ND TREATMENT RESPONSE QQ--35 |
| CTXX | CORE CONSTRUCTION | INDEPENDENT WIRE ROPE |
| CTXY | PREFABRICATION FORM | PREFORMED |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | LANYARD ASSEMBLY |
| BWCM | LOOP RETENTION METHOD | SWAGE |
| STYL | STYLE DESIGNATOR |