NSN 5340-01-510-9436 · NIIN 015109436 · FSC 5340
NO DASHES 5340015109436
In Stock
BRACKET,ANGLE
Hardware, Commercial
Application: C-17A AIRCRAFT
Technical characteristics
20 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 |
|---|---|---|
| ACHY | MOUNTING HOLE TYPE | PLAIN |
| ADLK | FIRST LEG LENGTH | INCHES NOMINAL 0.260 |
| ADLL | SECOND LEG LENGTH | INCHES NOMINAL 0.350 |
| AGAV | END ITEM IDENTIFICATION | C-17A AIRCRAFT |
| AHLN | SECOND LEG HOLE DIAMETER | INCHES MINIMUM 0.126 AND INCHES MAXIMUM 0.132 |
| AHLV | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH | INCHES NOMINAL 0.200 |
| AHLW | SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH | INCHES NOMINAL 0.350 |
| AHPW | FIRST LEG THICKNESS | INCHES NOMINAL 0.063 |
| AHPX | SECOND LEG THICKNESS | INCHES NOMINAL 0.063 |
| AJZU | FIRST LEG STYLE | |
| AKAU | FIRST LEG HOLE ARRANGEMENT STYLE | |
| AKBU | SECOND LEG STYLE | |
| AKCU | SECOND LEG HOLE ARRANGEMENT STYLE | |
| CSSP | SECOND LEG RELATIONSHIP TO FIRST LEG | NOT IDENTICAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | BRACKET, TRANSFORMER |
| MATT | MATERIAL | ALUMINUM ALLOY 5052 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | FED SPEC SINGLE MATERIAL RESPONSE QQ-A-250 TO 8 |
| SFTT | SURFACE TREATMENT | CHROMATE |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL SPEC SINGLE TREATMENT RESPONSE -IL-C-5541 CLASS 3 |
| STYL | STYLE DESIGNATOR |