PRODUCT
INFORMATION
PAGE

System 30
FEATURES
  • Two-axis autopilot combining Altitude Hold with the roll axis function of the System 20
  • Independent system- does not require interfacing to altimeter or attitude gyro
  • Derives all input from solid state absolute pressure transducer and accelerometer
  • Compact, remote-mounted pitch computer and amplifier
  • Smoothly holds existing altitude when engaged; can be activated during climb or descent
  • System senses out-of-trim conditions and annunciates direction to adjust pitch trim
  • Utilizes single, remotely-mounted Of/Off Switch to engage and disengage Altitude Hold
  • NOTE: Please reference System 20 page to view additional features included in this system


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

SPECIFICATIONS

SYSTEM:
Avg. Operating Current: 1.0 Amp @14VDC; 0.5 Amp @28VDC Max. Current: 5.0 Amps @14VDC; 3.0 Amps @28VDC

TURN COORDINATOR/ROLL COMPUTER:
Power Requirements: 14/28 VDC Flag Voltage Detector: (operating limits) 9.0 VDC approx.
Flag RPM Detector: (operating limits) nominal RPM less 20% Current Requirements: 0.3 Amp
Weight: 2.2 lbs. Dimensions: 3.28" x 3.28" x 7.4"
TSO: C3d, C9c

ROLL SERVO:
Power Requirements: 14/28 VDC Current Requirements: Included in System current requirements
Weight: 2.9 lbs. Dimensions: 3.75" x 3.75" x 7.25"

PITCH COMPUTER:
Power Requirements: 14/28 VDC Weight: 1.1 lb.
Dimensions: 5.8"W x 1.75"H x 3.25"L TSO: C9c

PITCH SERVO/TRIM SENSOR:
Power Requirements: 14/28 VDC Weight: 2.9 lbs.
Dimensions: 3.75"W x 3.75"H x 7.25"L Current Requirements: Included in system current requirements

ALTITUDE PRESSURE TRANSDUCER:
Power Requirements: 10 VDC (supplied by programmer/computer) Pressure Range: 0-15 PSI absolute
Over-Pressure: 150% of operating maximum Weight: 0.2 lbs.