NSN 1650-00-540-0156

Part Details | HYDRAULIC MOTOR

1650-00-540-0156 A mechanical device designed to convert the energy of fluid pressure to rotary motion.

Alternate Parts: 1011732, 10-1173-2, 157147, MF30391530S2122, MF30-3915-30S212-2, 1011732, 10-1173-2, 1650-00-540-0156, 00-540-0156, 1650005400156, 005400156

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
16JAN 01, 196300-540-015606128 ( MOTOR, HYDRAULIC )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 1650-00-540-0156
Part Number Cage Code Manufacturer
10-1173-282918BOEING COMPANY, THEDBA BOEING
15714762983EATON AEROSPACE LLC
MF30-3915-30S212-262983EATON AEROSPACE LLC
10-1173-281205THE BOEING COMPANYDBA BOEING
Technical Data | NSN 1650-00-540-0156
Characteristic Specifications
DISPLACEMENT TYPE CONSTANT
SHAFT ROTATION DIRECTION CLOCKWISE AND COUNTERCLOCKWISE
OPERATING SPEED AT RATED CAPACITY IN RPM2820.0
MAXIMUM WORKING PRESSURE RATING AT SPECIFIED TEMP RANGE3000 PSI AT MINUS 65 DEG F TO PLUS 275 DEG F
TORQUE LOAD RATING725.0 INCH-POUNDS
CONSTANT DISPLACEMENT PER REVOLUTION1.519 CUBIC INCHES
CONNECTION QUANTITYA2$$A1$$A1
CONNECTION GOVERNMENT SPEC/STDAND10050-6,AND10050-10 AND AND10050-10
CONNECTION DESIGN THREADED AND THREADED AND THREADED
THREAD SIZEA0.563-18$$A0.875-14$$A0.875-14
SCREW THREAD SERIES DESIGNATOR UNF AND UNF AND UNF
THREAD LOCATION INTERNAL AND INTERNAL AND INTERNAL
THREAD DIRECTION RIGHT-HAND AND RIGHT-HAND AND RIGHT-HAND
DRIVE SHAFT TYPE SPLINED, INVOLUTE EXTERNAL
SPLINE QUANTITY16
SPLINE MAJOR DIAMETER0.727 INCHES NOMINAL
SPLINE MINOR DIAMETER0.867 INCHES NOMINAL
SPLINE PITCH20/30
PITCH DIAMETER0.800 INCHES NOMINAL
SPLINE PRESSURE ANGLE IN DEG30.0
SPLINE LENGTH0.625 INCHES NOMINAL
DRIVE SHAFT GOVERNMENT STANDARDAND10262
SHAFT PROTRUSION LENGTH1.000 INCHES NOMINAL
MOUNTING TYPE FLANGE
MOUNTING GOVERNMENT STANDARDAND10621
MOUNTING HOLE QUANTITY4
MOUNTING BOLT HOLE SPACING3.536 IN. BY 3.536 IN. C TO C
MOUNTING HOLE DIAMETER0.344 INCHES NOMINAL
HOUSING MATERIAL ALUMINUM ALLOY
HOUSING SURFACE TREATMENT ANODIZED
FSC APPLICATION DATAAIRCRAFT HYDRAULIC SYSTEM B52