NSN 5990-00-268-9074

Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO

5990-00-268-9074 A synchro, the rotor of which is mechanically positioned for modifying electrical angular information, received from a transmitter synchro and transmitting to receiver synchro or control transformer synchro electrical information corresponding to the sum or difference of the electrical input angle and its rotor position angle. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: 5HDG, 5HDG, 5HDGMK9, MILS2335, MIL-S-2335, 5617926, 561792-6, 213403, 1357621, 1357620, SK139502, 5990-00-268-9074, 00-268-9074, 5990002689074, 002689074

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196300-268-907402071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND DOUBLE FLANGE B

Cross Reference | NSN 5990-00-268-9074
Part Number Cage Code Manufacturer
5HDG10112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
5HDG55972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
5HDGMK981349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-233581349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
561792-610001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
21340310001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
135762110001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
135762010001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
SK13950210001NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT
Technical Data | NSN 5990-00-268-9074
Characteristic Specifications
BODY SIZE5
STATOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
STATOR INPUT CURRENT RATING1.0 AMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING15.0 WATTS MAXIMUM
FREQUENCY IN HERTZ60.0 NOMINAL
MAXIMUM TEMP RISE50.0 DEG CELSIUS
TORQUE GRADIENT PER ANGULAR DEG0.300 INCH-OUNCES MINIMUM
BODY STYLE STANDARD ROUND DOUBLE FLANGE B
SHOULDER DIAMETER3.3750 INCHES MAXIMUM
PILOT DIAMETER1.6300 INCHES MAXIMUM
OVERALL LENGTH6.3600 INCHES MAXIMUM
FLANGE DIAMETER3.6230 INCHES MINIMUM AND 3.6250 INCHES MAXIMUM
FLANGE THICKNESS0.2450 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM
DISTANCE BETWEEN FLANGES1.8070 INCHES MINIMUM AND 1.8170 INCHES MAXIMUM
PILOT LENGTH0.1750 INCHES NOMINAL
SHOULDER LENGTH1.2450 INCHES MINIMUM AND 1.2550 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY6 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
SPECIAL FEATURESROUND,THREADED SHAFT WITH SLOT; SLOT DEPTH 0.050 INCH; SLOT WIDTH 0.035 INCH
TEST DATA DOCUMENT81349-MIL-S-2335 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.).
SPECIFICATION/STANDARD DATA81349-MIL--2335 GOVERNMENT SPECIFICATION
SHAFT END PLAY0.0081 INCHES NOMINAL
FRAGILITY FACTOR MODERATELY RUGGED