NSN 4730-01-391-9914
Part Details | FLUID FLOW RESTRICTOR UNIT
4730-01-391-9914 An assembly consisting of an orifice in a fixed plate, disk, or tube with screens or filters on one or both sides, depending on the direction of filtered flow. See RESTRICTOR, FLUID FLOW.
Alternate Parts: DAA3222P704, JHBA1875710D, 4730-01-391-9914, 01-391-9914, 4730013919914, 013919914
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 47 | JUN 21, 1994 | 01-391-9914 | 20933 ( RESTRICTOR UNIT, FLUID FLOW ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 4730-01-391-9914
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| DAA3222P704 | 81205 | THE BOEING COMPANYDBA BOEING |
| JHBA1875710D | 92555 | THE LEE COMPANY |
Technical Data | NSN 4730-01-391-9914
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | STRAIGHT |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| OVERALL LENGTH | 1.050 INCHES NOMINAL |
| DIAMETER | 0.1867 INCHES MINIMUM AND 0.1874 INCHES MAXIMUM |
| END ITEM IDENTIFICATION | 1650-01-383-2777 CAP,LINEAR ACTUATING CYLINDER USED ON B-2 BOMBER AIRCRAFT |
| SPECIAL FEATURES | ONE PIN,0.250 IN. LONG,0.160 IN. DIA,WAX COATED,PROVIDED |