NSN 5990-00-852-2369

Part Details | RECEIVER-TRANSMITTER SYNCHRO

5990-00-852-2369 A synchro having a dual purpose. It may be used in applications requiring either a receiver or transmitter. For synchros having a single purpose, see SYNCHRO, RECEIVER and SYNCHRO, TRANSMITTER.

Alternate Parts: C325108, C3251-08, 37TRX6A, AY3701A7D1, 37TRX6, VTRX376A1, VTRX37-6A1, 37TXCB, 5990PL1373980, 101532 PIECE 37, 10-1532 PIECE 37, 37TX6B, 37TRX6B, M2070874C001, M20708/74C-001, M207087401A, M20708/74-01A, M2070873A, M20708/73A, MILS2070874, MIL-S-20708/74, MILS2070873, MIL-S-20708/73, 37TR6, 1878084 PIECE 77, AS2070874, AS20708/74, M207087401A, M20708/74-01A, AS2070874, AS20708/74, 5990-00-852-2369, 00-852-2369, 5990008522369, 008522369

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59NOV 25, 196600-852-236927218 ( SYNCHRO, RECEIVER-TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND DOUBLE FLANGE A

Cross Reference | NSN 5990-00-852-2369
Part Number Cage Code Manufacturer
C3251-0882005ALLARD NAZARIAN GROUP, INC.DBA GRANITE STATE MANUFACTURING
37TRX6A07749BACHAN AEROSPACE CORP
AY3701A7D106840BENDIX CORP THE
37TRX610112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
VTRX37-6A110112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
37TXCB06848HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
5990PL13739809009HINSPEKTORAT WSPARCIA SIL ZBROJNYCH
10-1532 PIECE 3728199L3 TECHNOLOGIES, INC.DBA L3 HENSCHEL
37TX6B81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
37TRX6B81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/74C-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/74-01A81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/73A81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/7481349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/7381349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
37TR603956NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS
1878084 PIECE 7703956NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS
AS20708/740VH01SAE CUSTOMER SERVICEDEPT 2045
M20708/74-01A81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AS20708/7481343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 5990-00-852-2369
Characteristic Specifications
BODY SIZE37
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
ROTOR INPUT CURRENT RATING830.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING9.25 WATTS MAXIMUM
FREQUENCY IN HERTZ60.0 NOMINAL
ZSS IMPEDANCE MAGNITUDE IN OHMS7.00 MINIMUM AND 10.00 MAXIMUM
ZSS IMPEDANCE ANGLE IN DEG30.00 MINIMUM AND 40.00 MAXIMUM
TRANSFORMATION RATIO0.783 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG3.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE35.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT35.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT170.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM10.0/P10.0
RECEIVER ERROR ANGULAR RANGE IN MINUTESM36.0/P36.0
TORQUE GRADIENT PER ANGULAR DEG0.900 INCH-OUNCES NOMINAL
BODY STYLE STANDARD ROUND DOUBLE FLANGE A
SHOULDER DIAMETER3.3290 INCHES MINIMUM AND 3.3340 INCHES MAXIMUM
PILOT DIAMETER1.6250 INCHES NOMINAL
SECOND SHOULDER DIAMETER3.3740 INCHES MINIMUM AND 3.3750 INCHES MAXIMUM
SECOND SHOULDER LENGTH0.3750 INCHES NOMINAL
OVERALL LENGTH5.9500 INCHES NOMINAL
FLANGE DIAMETER3.6240 INCHES MINIMUM AND 3.6250 INCHES MAXIMUM
FLANGE THICKNESS0.2500 INCHES NOMINAL
BODY DIAMETER3.3850 INCHES MINIMUM AND 3.3900 INCHES MAXIMUM
DISTANCE BETWEEN FLANGES1.8120 INCHES NOMINAL
PILOT LENGTH0.1600 INCHES NOMINAL
SHOULDER LENGTH0.6550 INCHES NOMINAL
AFT OF SECOND FLANGE DIAMETER3.3740 INCHES MINIMUM AND 3.3750 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE5.0600 INCHES NOMINAL
TERMINAL TYPE AND QUANTITY5 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
TEST DATA DOCUMENT81349-MIL-S-20708 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--20708 TO 74 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED