NSN 5990-00-877-6971
Part Details | RECEIVER SYNCHRO
5990-00-877-6971 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: 11TR1149BR, 11TR-1149-BR, 35631100018, 3563110-0018, AY110JH17A1, 35631100018, 3563110-0018, AY110JH17A1, 5990-00-877-6971, 00-877-6971, 5990008776971, 008776971
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | AUG 18, 1967 | 00-877-6971 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-877-6971
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 11TR-1149-BR | 51761 | CDA INTERCORP LLC |
| 3563110-0018 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110JH17A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563110-0018 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY110JH17A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-877-6971
| 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 | 600.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 44.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 243.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 11.70 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 40.50 NOMINAL |
| ZRS RESISTANCE IN OHMS | 57.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 28.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 18.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 9.30 NOMINAL |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.000 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M4.5/P4.5 |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M9.0/P9.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 2000.0 MILLIMETER-MILLIGRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 1.8680 INCHES MINIMUM AND 1.8880 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0600 INCHES MINIMUM AND 0.0640 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6200 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0900 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM |
| SECURING HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |
