NSN 5990-00-504-6023
Part Details | TRANSMITTER SYNCHRO
5990-00-504-6023 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: M010922, M01092-2, 4765966, 476596-6, 10377801, 103778-01, 7475539P1, 7406457P2, 200841, 20084-1, AY20153B, AY201S3B, AY201S3B, AY101D, 7856715, 785671-5, 35631500310, 3563150-0310, 200841, 20084-1, AY20153B, CP359111L, CP35-9-11-1L, 4511268, 451-1268, 70452, 704-52, 2G40058, 2G4005-8, 46285, 20084, 8485160, 5990-00-504-6023, 00-504-6023, 5990005046023, 005046023
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-504-6023 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-504-6023
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| M01092-2 | 80249 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION INC. |
| 476596-6 | 20418 | DRS SUSTAINMENT SYSTEMS, INC.Use CAGE Code 98255 for cataloging |
| 103778-01 | 35351 | GE AVIATION SYSTEMS LLC |
| 7475539P1 | 03508 | GENERAL ELECTRIC COSEMI-CONDUCTOR PRODUCTS DEPT |
| 7406457P2 | 03508 | GENERAL ELECTRIC COSEMI-CONDUCTOR PRODUCTS DEPT |
| 20084-1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY20153B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201S3B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201S3B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY101D | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 785671-5 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 3563150-0310 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 20084-1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY20153B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| CP35-9-11-1L | 25500 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 451-1268 | 11530 | LOCKHEED MARTIN CORPORATIONDIV LOCKHEED MARTIN INFORMATION |
| 704-52 | 01365 | MARINE CORPS LOGISTICS COMMANDTECHNICAL DATA REPOSITORY |
| 2G4005-8 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 46285 | 96214 | RAYTHEON COMPANYDBA RAYTHEON |
| 20084 | 96214 | RAYTHEON COMPANYDBA RAYTHEON |
| 8485160 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-504-6023
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 65.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 33.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 80.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 400.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 42.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 10.80 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 5.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 6.0 DEG CELSIUS |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 40.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1000 INCHES MINIMUM AND 2.1620 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.3144 INCHES MINIMUM AND 1.3150 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0680 INCHES MINIMUM AND 0.0880 INCHES MAXIMUM |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.5600 INCHES MINIMUM AND 1.6220 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8660 INCHES MINIMUM AND 0.8750 INCHES MAXIMUM |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |