NSN 5990-00-855-6535
Part Details | RECEIVER SYNCHRO
5990-00-855-6535 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: AY607VE43A1, AY110AH94A2, AY110AH94A1, 17890513, 1789051-3, 17890512, 1789051-2, AY607VE43A2, AY607VE43A2, 17890513, 1789051-3, AY607VE43A1, AY110AH94A1, 17890513, 1789051-3, 17890512, 1789051-2, AY607VE43A2, 5990-00-855-6535, 00-855-6535, 5990008556535, 008556535
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-855-6535 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-855-6535
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY607VE43A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110AH94A2 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110AH94A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1789051-3 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1789051-2 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY607VE43A2 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY607VE43A2 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| 1789051-3 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| AY607VE43A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY110AH94A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1789051-3 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1789051-2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY607VE43A2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-855-6535
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 220.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.1 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 68.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 120.00 NOMINAL |
| MAXIMUM TEMP RISE | 95.0 DEG CELSIUS |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9060 INCHES NOMINAL |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 2.1190 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0620 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.0000 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0930 INCHES NOMINAL |
| PILOT LENGTH | 0.0470 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1250 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7440 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| SHAFT END PLAY | 0.0025 INCHES MINIMUM AND 0.0050 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 3.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |
