Part Details | DISPLACEMENT GYROSCOPE
6615-00-596-7223 A gyroscope which senses, measures and transmits angular displacement data.
Alternate Parts: 45377, MILA22858, MIL-A-22858, CN1169AA, CN-1169A/A, 45377, 6615-00-596-7223, 00-596-7223, 6615005967223, 005967223
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | JAN 11, 1975 | 00-596-7223 | 20599 ( GYROSCOPE, DISPLACEMENT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-00-596-7223
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 45377 | 50027 | FLIGHTLINE ELECTRONICS, INC.DBA ULTRA ELECTRONICS, FLIGHTLINE |
| MIL-A-22858 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| CN-1169A/A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 45377 | 78286 | SIKORSKY AIRCRAFT CORPORATIONDBA SIKORSKY |
Technical Data | NSN 6615-00-596-7223
| Characteristic | Specifications |
|---|---|
| UNIT TYPE | VERTICAL |
| WHEEL POWER METHOD | ELECTRIC |
| CURRENT TYPE | AC |
| VOLTAGE IN VOLTS | 115.0 |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | SINGLE |
| FREEDOM AXIS QUANTITY | 2 |
| GIMBAL QUANTITY | 2 |
| AXIS DISPLACEMENT LIMITATION IN DEG | PORM 82 DEG FOR PITCH AXIS,PORM 180 DEG FOR ROLL AXIS |
| DESIGN TYPE | NONCAGEABLE |
| GIMBAL TORQUE APPLICATION METHOD | AC TORQUE MOTOR |
| TORQUED GIMBAL QUANTITY | 2 |
| SENSING OUTPUT/SIGNAL LEVEL METHOD | SYNCHRO OUTPUT 11.5V INTERNAL EXCITATION |
| INSTRUMENT TYPE | UNFLOATED |
| SHOCK MOUNT | NOT PROVIDED |
| OVERALL LENGTH | 7.510 INCHES NOMINAL |
| OVERALL WIDTH | 6.000 INCHES MAXIMUM |
| OVERALL HEIGHT | 4.400 INCHES MAXIMUM |
| FSC APPLICATION DATA | AUTOMATIC FLIGHT CONTROL SYSTEM,AIRCRAFT |