Garmin GAD 43 Installation Manual - Page 39
RATE/BARO CORRECTION output.
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Manufacturer Collins Cessna/ARC King Sperry Century Table 5-1. Gyro Emulation Types Model(s) 332D-11T G519 KI 256 KVG 350 VG-14A 52C77-4 (Triden), 52D67/M,52D77-4, 52D167/M, 52D188( ), 52D254, 52D267/M (Triden), 52D267/M (2000) 2. YAW RATE SCALE FACTOR, specifies the scaling in mV/deg/sec used on the YAW RATE/BARO CORRECTION output. Selections: None, 100, 200, 333, 666 (mV/deg/sec) OUTPUT TEST Window: 1. PITCH ANGLE, specifies the pitch angle on all of the analog pitch outputs from the GAD 43. Selections: 89°U to 90°D in 1° increments. 2. ROLL ANGLE, specifies the roll angle on all of the analog roll outputs from the GAD 43. Selections: 179°R to 180°L in 1° increments. 3. RELAY POSITION, specifies the position of the Attitude Valid and AP Interlock Relay contacts. Selections: Attitude Invalid or Attitude Valid. 4. YAW RATE, specifies the yaw rate on the Yaw Rate/Baro Correction output from the GAD 43. Selections: 127°/sec R to 128°/sec L in 1°/sec increments 5. HEADING, specifies the heading angle on the synchro heading output from the GAD 43. Selections: 0° to 359° in 1° increments. 6. HEADING VALID, specifies the state of the Heading Valid discrete output. Selections: Invalid or Valid. 7. SPARE DISC OUT 2*, specifies the state of the Spare Disc Out 2 discrete output. Selections: Active or Inactive. GAD 43 Installation Manual 190-00899-00 Page 5-3 Rev. B
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