NSN 5990-00-236-8152

Part Details | TRANSMITTER SYNCHRO

5990-00-236-8152 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: AY080AC49A1, 35630800039, 3563080-0039, 22770210001, 2277021-0001, AY080AC49A1, 35630800039, 3563080-0039, 22770210001, 2277021-0001, 5990-00-236-8152, 00-236-8152, 5990002368152, 002368152

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59MAR 10, 197100-236-815202073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

SYNCHRO,TRANSMITTER | 5990-00-236-8152, 002368152
Cross Reference | NSN 5990-00-236-8152
Part Number Cage Code Manufacturer
AY080AC49A196774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
3563080-003996774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
2277021-000196774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY080AC49A155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
3563080-003955972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
2277021-000155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
Technical Data | NSN 5990-00-236-8152
Characteristic Specifications
BODY SIZE8
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
ROTOR INPUT CURRENT RATING29.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING740.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS874.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS3860.00 NOMINAL
ZSO RESISTANCE IN OHMS9.50 NOMINAL
PLUS J ZSO REACTANCE IN OHMS34.00 NOMINAL
ZRS RESISTANCE IN OHMS1480.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS325.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS687.00 NOMINAL
STATOR DC RESISTANCE IN OHMS10.30 NOMINAL
PHASE SHIFT ANGLE IN DEG9.200 INPUT TO OUTPUT NOMINAL
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT75.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM7.0/P7.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS7.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.0 MILLIMETER-MILLIGRAMS NOMINAL
TORQUE GRADIENT PER ANGULAR DEG2400.000 MILLIMETER-MILLIGRAMS NOMINAL
BODY STYLE STANDARD ROUND A
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.6150 INCHES NOMINAL
FLANGE DIAMETER0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
UNDERCUT DIAMETER0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM
UNDERCUT WIDTH0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
PILOT LENGTH0.0390 INCHES MINIMUM AND 0.0430 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2400 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.0500 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.5670 INCHES MINIMUM AND 0.5730 INCHES MAXIMUM
ALIGNMENT HOLE QUANTITY2
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
SHAFT MAXIMUM RADIAL PLAY0.0005 INCHES
SHAFT RADIAL PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY0.0003 INCHES MINIMUM AND 0.0008 INCHES MAXIMUM
SHAFT END PLAY DETERMINING WEIGHT8.0 OUNCES
SHAFT MAXIMUM RUNOUT0.0010 INCHES
FRAGILITY FACTOR MODERATELY RUGGED