PRODUCT
INFORMATION
PAGE

System 50
FEATURES
  • Two axis, roll & pitch stabilization autopilot
  • 3" ATI programmer/computer
  • Provides command turn function up to 90% standard rate turn, VOR/LOC and back course (reverse) tracking
  • Rate-based system, deriving roll axis control inputs from separate electric turn coordinator
  • Gain enhancement feature for use when tracking GPS & LORAN input signals
  • Altitude Hold and trim indicator lights
  • Heading Pre-select is optional* by adding S-Tec course selector Dir. Gyro or HSI with autopilot outputs
  • Building block concept allows upgrading to System 55, System 60-2, System 65
  • Manual electric trim option* available


  • ** CALL FOR INSTALLATION PRICE - OVER THE COUNTER SALES ONLY FOR EXPERIMENTAL AIRCRAFT
*OPTIONS

SPECIFICATIONS

PROGRAMMER/COMPUTER:
Power Requirements: 14/28 VDC Weight: 2.4 lbs.
Dimensions: 3.3" x 3.3" x 7.5" System Requirements: current= avg. 1.0 amp; max. 5.0 amp

TURN COORDINATOR:
Power Requirements: 14/28 VDC Flag Voltage Detector: (operating limits) 9.0 VDC approx.
Flag RPM Detector: (operating limits) nominal RPM less 10% Current Requirements: 3 Amp
Weight: 1.8 lbs. Dimensions: 3.275" x 3.275" x 5.62"

ROLL SERVO:
Power Requirements: 14/28 VDC Current Requirements: system value equivalent
Weight: 2.9 lbs. Dimensions: 3.75" x 3.75" x 7.25"

ALTITUDE PRESSURE TRANSDUCER:
Power Requirements: 10 VDC (supplied by programmer/computer) Pressure Range: 0.15 PSI absolute
Overpressure: 150% operating maximum