Part Details | ATTITUDE-HEADING GYROSCOPE CONTROL
6615-00-663-8277 A control designed for use with automatic pilots and/or remote attitude indicators consisting primarily of a gyroscope which provides signals for controlling an aircraft about its lateral and longitudinal axis and/or signals for providing a visual presentation of attitude to the pilot.
Alternate Parts: 124021FB1A, 12402-1FB1A, 124021FB1A, 12402-1FB1A, 6615-00-663-8277, 00-663-8277, 6615006638277, 006638277
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | JAN 01, 1963 | 00-663-8277 | 37254 ( CONTROL, GYROSCOPE, ATTITUDE-HEADING ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-00-663-8277
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 12402-1FB1A | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| 12402-1FB1A | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 6615-00-663-8277
| Characteristic | Specifications |
|---|---|
| POWER SOURCE | EXTERNAL |
| MAXIMUM VOLTAGE RATING IN VOLTS | 26.0 AC |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | THREE |
| INTELLIGENCE DATA HANDLING CAPABILITY | AABD GYROSCOPE-ALTITUDE DATA TRANSMITTING AND AABD PITCH-ROLL SIGNAL DATA TRANSMITTING |
| INDICATION METHOD | TRANSMITTING DIAL |
| TERMINAL TYPE AND QUANTITY | 3 PIN |
| MAXIMUM OVERALL LENGTH | 8.358 INCHES |
| MAXIMUM OVERALL WIDTH | 3.438 INCHES |
| MAXIMUM OVERALL HEIGHT | 3.438 INCHES |
| MOUNTING METHOD | FLUSH PANEL |
| FSC APPLICATION DATA | AUTO PILOT SYSTEM,AIRCRAFT |