Part Details | FLUID FILTER ELEMENT
1650-01-113-0418 A replaceable device designed to remove solid particles from fluids ranging in density from heavy liquids to gases. The removal of particles is accomplished by porous material (metallic or non-metallic), stacked disks, wound wire, or the like, constructed so the fluid can flow through the device while the solid particles are retained. It may be designed to fit into a FILTER, FLUID (or similar cavity), or it may have an integral outer casing and mounting facilities and be designed to connect directly to an engine, compressor, or the like. The degree of removal of particles must be nominally rated at less than 50 microns or absolutely rated at less than 75 microns. Excludes FILTER ELEMENT, AIR CONDITIONING. See also STRAINER ELEMENT, SEDIMENT.
Alternate Parts: ACA671F3, AC-A671F-3, 145DS1092, 145DS109-2, 1650-01-113-0418, 01-113-0418, 1650011130418, 011130418
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 16 | MAY 15, 1981 | 01-113-0418 | 32624 ( FILTER ELEMENT, FLUID ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1650-01-113-0418
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AC-A671F-3 | 18350 | PALL AEROPOWER CORPORATION |
| 145DS109-2 | 77272 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 1650-01-113-0418
| Characteristic | Specifications |
|---|---|
| MESH SIZE | 42.0 |
| FILTRATION RATING IN MICRONS | 15.0 NOMINAL AND 30.0 ABSOLUTE |
| MEDIA FOR WHICH DESIGNED | Y ANY ACCEPTABLE |
| DROP PRESSURE | 5.0 POUNDS PER SQUARE INCH |
| FILTERING SYSTEM FOR WHICH DESIGNED | BY-PASS FLOW |
| END ITEM IDENTIFICATION | CH-47D HELICOPTER |