Part Details | DISPLACEMENT GYROSCOPE
6615-00-061-1519 A gyroscope which senses, measures and transmits angular displacement data.
Alternate Parts: 1388160101, 138816-01-01, MILG27693TYPESBU6A, 6615-00-061-1519, 00-061-1519, 6615000611519, 000611519
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | JAN 01, 1963 | 00-061-1519 | 20599 ( GYROSCOPE, DISPLACEMENT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-00-061-1519
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 138816-01-01 | 35351 | GE AVIATION SYSTEMS LLC |
| MILG27693TYPESBU6A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
Technical Data | NSN 6615-00-061-1519
| Characteristic | Specifications |
|---|---|
| UNIT TYPE | VERTICAL |
| WHEEL POWER METHOD | ELECTRIC |
| CURRENT TYPE | AC |
| VOLTAGE IN VOLTS | B115.0$$B200.0 |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | THREE |
| FREEDOM AXIS QUANTITY | 2 |
| GIMBAL QUANTITY | 2 |
| AXIS DISPLACEMENT LIMITATION IN DEG | PORM 82 DEG MIN OF FREEDOM IN PITCH;UNLIMITED FREEDOM IN ROLL |
| DESIGN TYPE | NONCAGEABLE |
| GIMBAL TORQUE APPLICATION METHOD | GB ANY ACCEPTABLE |
| TORQUED GIMBAL QUANTITY | 2 |
| SENSING OUTPUT/SIGNAL LEVEL METHOD | SYNCHRO OUTPUT 115 V 400 CYCLES EXTERNALLY EXCITED 11.8 V AC OUTPUT |
| INSTRUMENT TYPE | UNFLOATED |
| SHOCK MOUNT | NOT PROVIDED |
| OVERALL LENGTH | 6.687 INCHES NOMINAL |
| OVERALL WIDTH | 3.875 INCHES NOMINAL |
| OVERALL HEIGHT | 3.875 INCHES NOMINAL |
| SPECIAL FEATURES | FAAZ 4 WIRE |
| NONDEFINITIVE SPEC/STD DATA | SBU-6 TO A TYPE |