NSN 5990-00-138-2730
Part Details | TRANSMITTER SYNCHRO
5990-00-138-2730 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: 5RS9107E, 5RS910-7E, 5RS9107E, 5RS910-7E, CR90910029, 1470430001, 147-043-0001, BGC11F2B633, BGC-11-F-2/B633, 1470430001, 147-043-0001, 5990-00-138-2730, 00-138-2730, 5990001382730, 001382730
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUL 24, 1971 | 00-138-2730 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-138-2730
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5RS910-7E | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| 5RS910-7E | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| CR90910029 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| 147-043-0001 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| BGC-11-F-2/B633 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 147-043-0001 | 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
Technical Data | NSN 5990-00-138-2730
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 32.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 7.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 35.00 NOMINAL |
| ZSS RESISTANCE IN OHMS | 40.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 19.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 5.75 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.700 INPUT TO OUTPUT NOMINAL |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 16.00 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.00 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.4600 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0450 INCHES MINIMUM AND 0.0550 INCHES MAXIMUM |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.8350 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 TAB, SOLDER LUG |
| TERMINAL LOCATION | FRONT |
| BODY MATERIAL | STEEL, STAINLESS |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES NOMINAL |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0015 INCHES NOMINAL |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| END ITEM IDENTIFICATION | EA-6B, A6E AND F-111 AIRCRAFT |