Part Details | RECEIVER SYNCHRO
5990-00-253-0261 A synchro consisting of a stator and rotor inductively coupled. The rotor is free to turn in accordance with the electrical input from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: AY110BC42B2, AY110BC42B2, 6028942, 602894-2, 413503, 4135-03, URH11CM4B531, URH11CM4/B531, URH11CM4F552, URH-11-CM-4/F552, URH11CM4B531, URH-11-CM-4/B531, 11TR2530261, 11TR253-0261, 5990-00-253-0261, 00-253-0261, 5990002530261, 002530261
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUL 18, 1969 | 00-253-0261 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-253-0261
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY110BC42B2 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110BC42B2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 602894-2 | 06401 | L3 TECHNOLOGIES, INC.DBA COMMUNICATION SYSTEMS-WEST |
| 4135-03 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| URH11CM4/B531 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| URH-11-CM-4/F552 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| URH-11-CM-4/B531 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 11TR253-0261 | 2X130 | MOTION DEVICES TECHNOLOGY, INC. |
Technical Data | NSN 5990-00-253-0261
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 120.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 0.6 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 35.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 288.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 8.10 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 47.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 49.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 24.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 18.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 7.50 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 5.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 15.0 DEG CELSIUS |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M30.0/P30.0 |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M60.0/P60.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 5400.0 MILLIMETER-MILLIGRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 2700.0 MILLIMETER-MILLIGRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 2250.0 MILLIMETER-MILLIGRAMS MINIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1860 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9860 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0500 INCHES MINIMUM |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7490 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0020 INCHES MINIMUM AND 0.0050 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| FRAGILITY FACTOR | MODERATELY RUGGED |