0 to 90.
0 to 180.
45 to 90
45 to 180.
Rotation of the Earth, and geographic longitude.
Rotation of the Earth, and geographic latitude
Aircraft attitude, and geographic longitude
Aircraft attitude, and geographic latitude
Meridian convergence error
Transmission error.
Coriolis error.
Index error
Directional gyro
Digital controller
Remote compensator
Magnetic azimuth detector.
Two variable resistors and three isolation resistors
Three variable resistors and two isolation resistors
Two variable diodes and three isolation diodes.
Three variable diodes and two isolation diodes
DG mode
RGA mode.
MAG mode
AUTO mode.
Tripod
Aircraft
Compass rose
Magnetic field monitor
42-power and rotates 180 degrees
42-power and rotates 360 degrees
22-power and rotates 180 degrees
22-power and rotates 360 degrees.
Power
Monitor
Intercom
Transmitter
Magnetic azimuth detector or remote magnetic compensator.
Remote magnetic compensator or digital controller
Magnetic azimuth detector or digital controller
Compass controller or compass amplifier
20 degrees up to 5 degrees down
15 degrees up to 5 degrees down
20 degrees up to 10 degrees down.
15 degrees up to 10 degrees down
Approach speed.
Approach track
Ground speed
Ground track.
Remote heading slew switch
Pitch command control
Heading slew controls
Rate-of-turn indicator
Pilot only
Copilot only.
Pilot and copilot.
Pilot and navigator
Horizontal situation indicator (HSI) lubber line.
Attitude director indicator (ADI) command bars
Horizontal situation indicator (HSI) compass card.
Attitude director indicator (ADI) speed deviation scale.
7
8
8.5
9.5
Wings-level dive attitude of 7 degrees
Wings-level dive attitude of 8 degrees.
Wings-level climb attitude of 7 degrees.
Wings-level climb attitude of 8 degrees.
70
80
90
100
RGA computer
RGA control panel.
RGA interface logic unit
Longitudinal accelerometer
15 or 25 degree flap discrete signals.
20 or 25 degree flap discrete signals
25 or 30 degree flap discrete signals.
25 or 35 degree flap discrete signals
Dim switch
Flap test switch.
Test reset switch.
Weight-on-wheels test switch.
Compass, localizer, glide slope, and autopilot systems
Compass, localizer, glide slope, and radio altimeter systems
Compass, localizer, glide slope, and flight management systems.
Compass, localizer, glide slope, and barometric altimeter systems
Five monitored dual navigation systems has a discrepancy
Seven monitored dual navigation systems has a discrepancy.
Five monitored dual navigation systems is operating correctly
Seven monitored dual navigation systems is operating correctly.
3
4
5
6
Two degrees pitch exists for more than three seconds between the RGA computers
Three degrees pitch exists for more than two seconds between the RGA computers.
Two degrees pitch exists for more than three seconds between the steering computers
Three degrees pitch exists for more than two seconds between the steering computers.