NSN 5990-01-207-5336
Part Details | TRANSMITTER SYNCHRO
5990-01-207-5336 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: CM41091005, CM410910050, CM41091005-0, CM41091005, NF2036942, NF203694-2, 5990-01-207-5336, 01-207-5336, 5990012075336, 012075336
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | MAY 02, 1985 | 01-207-5336 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-01-207-5336
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CM41091005 | 09301 | KEARFOTT CORP SOMA FORWARDING DIV |
| CM41091005-0 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| CM41091005 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| NF203694-2 | 78567 | SPECO CORP |
Technical Data | NSN 5990-01-207-5336
| Characteristic | Specifications |
|---|---|
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 109.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 1375.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 115.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 225.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 70.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 65.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 180.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 140.00 NOMINAL |
| ZSS RESISTANCE IN OHMS | 75.00 NOMINAL |
| PLUS J ZSS REACTANCE IN OHMS | 20.00 NOMINAL |
| ZSO-90 RESISTANCE IN OHMS | 47.00 NOMINAL |
| PLUS J ZSO-90 REACTANCE IN OHMS | 47.00 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 238.00 NOMINAL |
| ZRO IMPEDANCE ANGLE IN DEG | 61.00 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 87.00 NOMINAL |
| ZSO IMPEDANCE ANGLE IN DEG | 41.80 NOMINAL |
| ZRS IMPEDANCE MAGNITUDE IN OHMS | 78.50 NOMINAL |
| ZRS IMPEDANCE ANGLE IN DEG | 15.50 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 42.50 MINIMUM AND 57.50 MAXIMUM |
| STATOR DC RESISTANCE IN OHMS | 35.70 MINIMUM AND 48.30 MAXIMUM |
| TRANSFORMATION RATIO | 0.440 STATOR TO ROTOR MINIMUM AND 0.468 STATOR TO ROTOR MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 20.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 1.8750 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7470 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| PILOT LENGTH | 0.0380 INCHES MINIMUM AND 0.0430 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.5000 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | SIDE |
| BODY MATERIAL | ANY ACCEPTABLE |
| END ITEM IDENTIFICATION | B-1B ACFT |
