Part Details | TRANSMITTER SYNCHRO
5990-00-241-3767 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: 8TX100D1, AY080BE40A2, AY080BE-40-A2, CM41014037, CM41014037, CGH8A1L943, CGH-8-A-1/L943, 42734702, 4273-47-02, 2293044010, 229-3044-010, 5990-00-241-3767, 00-241-3767, 5990002413767, 002413767
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 12, 1969 | 00-241-3767 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-241-3767
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 8TX100D1 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| AY080BE-40-A2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| CM41014037 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CM41014037 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| CGH-8-A-1/L943 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 4273-47-02 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 229-3044-010 | 13499 | ROCKWELL COLLINS, INC.DBA GOVERNMENT SYSTEMS |
Technical Data | NSN 5990-00-241-3767
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 170.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 930.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 32.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 150.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 7.30 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 26.20 NOMINAL |
| ZRS RESISTANCE IN OHMS | 55.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 17.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 24.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 8.50 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 9.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.5880 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7470 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
| PILOT LENGTH | 0.0380 INCHES MINIMUM AND 0.0480 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0008 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |