NSN 1650-00-476-9253

Part Details | LINEAR ACTUATING CYLINDER ASSEMBLY

1650-00-476-9253 A cylinder containing a piston and other component parts designed to develop linear motion required to operate a given object(s) with energy generated from either pneumatic or hydraulic pressure(s). See also CYLINDER, ACTUATING, LINEAR. Do not use if a more specific name applies.

Alternate Parts: 536900781, 53-690078-1, 536900683, 53-690068-3, 1650-00-476-9253, 00-476-9253, 1650004769253, 004769253

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
16MAR 09, 197200-476-925331310 ( CYLINDER ASSEMBLY, ACTUATING, LINEAR )
REFERENCE DRAWINGS & PICTURES

TWO HOLE

Cross Reference | NSN 1650-00-476-9253
Part Number Cage Code Manufacturer
53-690078-176301BOEING COMPANY, THEDBA BOEING
53-690068-376301BOEING COMPANY, THEDBA BOEING
Technical Data | NSN 1650-00-476-9253
Characteristic Specifications
DESIGN CHARACTERISTICS DOUBLE ACTING SINGLE CYLINDER
EXTENDED LENGTH16.430 INCHES NOMINAL
INTEGRAL VALVE OPERATION METHOD HYDRAULIC
OVERALL WIDTH4.625 INCHES NOMINAL
OVERALL HEIGHT3.520 INCHES NOMINAL
OVERALL DIAMETER3.000 INCHES NOMINAL
BODY OUTSIDE DIAMETER2.670 INCHES NOMINAL
PISTON ROD END SIMILARITY IDENTICAL
MOUNTING TYPE AND LOCATION FORK PISTON ROD END
MOUNTING PROVISION UNTHREADED MOUNTING HOLES
MOUNTING PROVISION ARRANGEMENT STYLE TWO HOLE
CENTER TO CENTER DISTANCE BETWEEN MOUNTING PROVISIONS3.520 INCHES NOMINAL
PORT LOCATION AND QUANTITY1 CENTER SECTION AND 1 CYLINDER HEAD END AND 1 PISTON ROD END
TEMP RATING-65.0 DEG FAHRENHEIT AND 275.0 DEG FAHRENHEIT
PRESSURE RATING3000.0 POUNDS PER SQUARE INCH NOMINAL
TEST DATA DOCUMENT76301-53-690068-3 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.).
FSC APPLICATION DATAHYDRAULIC SYSTEM,AIRCRAFT