5990-00-504-6022 SYNCHRO,TRANSMITTER Index 5990-00-504-6024 SYNCHRO,TRANSMITTER

National Stock Number:
5990-00-504-6023

Federal Supply Class:
5990

National Item Identification Number:
005046023

Description:
SYNCHRO,TRANSMITTER

Detail:
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.


Manufacturer Information:
103778-0135351GE AVIATION SYSTEMS LLC
2008496214RAYTHEON COMPANY
20084-155972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
3563150-031055972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
20084-196774HONEYWELL INTERNATIONAL INC.
2G4005-899932MOOG INC.
704-5201365MARINE CORPS LOGISTICS COMMAND TECHNICAL DATA REPOSITORY CUSTOMER SERVICE-MICC LOGISTICS OPERATIONS CENTER
7406457P203508GENERAL ELECTRIC CO SEMI-CONDUCTOR PRODUCTS DEPT
7475539P103508GENERAL ELECTRIC CO SEMI-CONDUCTOR PRODUCTS DEPT
451-126811530LOCKHEED MARTIN CORPORATION DIV LOCKHEED MARTIN INFORMATION SYSTEMS & GLOBAL SOLUTIONS
476596-620418DRS SUSTAINMENT SYSTEMS, INC. USE CAGE CODE 98255 FOR CATALOGING
785671-555972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
4628596214RAYTHEON COMPANY
3563150-031096774HONEYWELL INTERNATIONAL INC.
848516018876U S ARMY AVIATION AND MISSILE COMMAND
CP35-9-11-1L25500LOCKHEED MARTIN CORPORATION
AY201S3B55972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
AY101D55972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
AY20153B55972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
M01092-280249BAE SYSTEMS INFORMATION AND ELECTRONIC SYSTEMS INTEGRATION INC.
AY201S3B96774HONEYWELL INTERNATIONAL INC.
AY20153B96774HONEYWELL INTERNATIONAL INC.
AY101D96774HONEYWELL INTERNATIONAL INC.
785671-596774HONEYWELL INTERNATIONAL INC.


Techincal Specification:
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-10.0 TO 10.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS15.0 CENTIMETER-GRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.0 CENTIMETER-GRAMS MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8660 INCHES MINIMUM AND 0.8750 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.1250 INCHES MAXIMUM
ALIGNMENT HOLE QUANTITY3
BODY MATERIALALUMINUM
BODY STYLESTANDARD ROUND C
BODY SIZE15
FLANGE DIAMETER1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
FRAGILITY FACTORMODERATELY RUGGED
FREQUENCY IN HERTZ400.0 NOMINAL
LENGTH0.1320 INCHES NOMINAL SHOULDER
OVERALL LENGTH2.1000 INCHES MINIMUM AND 2.1620 INCHES MAXIMUM
MAXIMUM TEMP RISE6.0 CELSIUS
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT40.00
MOUNTING SURFACE TO TERMINAL END DISTANCE1.5600 INCHES MINIMUM AND 1.6220 INCHES MAXIMUM
PILOT LENGTH0.0400 INCHES NOMINAL
PHASE SHIFT ANGLE IN DEG5.500 INPUT TO OUTPUT NOMINAL
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
PLUS J ZRO REACTANCE IN OHMS400.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS42.00 NOMINAL
ROTOR INPUT CURRENT RATING65.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING33.0 MILLIWATTS NOMINAL
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
SHAFT MAXIMUM RADIAL PLAY0.0010 INCHES
SHAFT MAXIMUM RUNOUT0.0010 INCHES
SHAFT RADIAL PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY0.0003 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM
SHOULDER DIAMETER1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM
STATOR DC RESISTANCE IN OHMS10.80 NOMINAL
ZRO RESISTANCE IN OHMS80.00 NOMINAL
TERMINAL LOCATIONREAR
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
UNDERCUT DIAMETER1.3144 INCHES MINIMUM AND 1.3150 INCHES MAXIMUM
UNDERCUT WIDTH0.0680 INCHES MINIMUM AND 0.0880 INCHES MAXIMUM


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