NSN 6615-00-514-5388
Part Details | ATTITUDE-HEADING GYROSCOPE CONTROL
6615-00-514-5388 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: 124021AB1A, 12402-1AB1A, 124021AB1A, 12402-1AB1A, 6615-00-514-5388, 00-514-5388, 6615005145388, 005145388
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | JAN 01, 1963 | 00-514-5388 | 37254 ( CONTROL, GYROSCOPE, ATTITUDE-HEADING ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6615-00-514-5388
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 12402-1AB1A | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| 12402-1AB1A | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 6615-00-514-5388
| Characteristic | Specifications |
|---|---|
| POWER SOURCE | EXTERNAL |
| MAXIMUM VOLTAGE RATING IN VOLTS | 26.0 AC |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | THREE |
| INCLOSURE TYPE | ENCASED |
| MAXIMUM OVERALL LENGTH | 8.358 INCHES |
| MAXIMUM OVERALL WIDTH | 3.437 INCHES |
| MAXIMUM OVERALL HEIGHT | 3.437 INCHES |
| MOUNTING METHOD | PANEL |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY FINISH OF GRADUATIONS |
