The ADF-700 AM receiver is a solid state digital airborne
automatic direction finder receiver that determines relative bearing to any
selected transmitter operating between 190 kHz and 1750 kHz. When a frequency
is selected in the cockpit by a control it converts the frequency selected to
ARINC 429 code to transmit through the aircraft data bus to the ADF-700 to
cause it to tune to the frequency selected. Bearing information of the
received signal is then sent to the bearing indicator for display while aural
intelligence is presented to the aircraft intercom system. The ADF-700
receives RF signals from three antennas and determines the relative bearing
between the center line of the aircraft and the selected station. The signals
received may include any in the normal broadcast band from commercial
broadcast ground transmitters. Ground transmitters are located at known
coordinates around the world which transmit AM modulated station
identification codes, weather and flight information. This information is
converted into ARINC 429 format for transmission to the aircraft-bearing
indicator.
The ADF-700 consists
of sub-assemblies and a chassis assembly housed in a 2-MCU-size case. The
equipment consists of an aluminum chassis to provide mounting and Collins
surfaces for the major sub-assemblies. Cooling air is circulated freely
throughout the unit through holes provided on the top and bottom of the
chassis. Three self-test indicators and a self-test button are located on the
front panel with a foldaway handle that facilitates removal from the rack and
carrying the ADF-700. A hold-down is supplied on the front to secure the LRU
to the aircraft equipment rack. Electrical connections are made through an
ARINC 600 connector on the rear of the chassis. The ADF-700 is directly
interchangeable with installations that have full ARINC 712 wiring. The
ADF-700 works in association with an indicator which displays aircraft
magnetic heading, course and relative bearing between aircraft heading and
the direction of the selected signal source. The ADF-700 also requires a
sense (omnidirectional) antenna that is vertically polarized in the
horizontal plane and 2 loop (directional) antennas that are
orthogonally-polarized with one antenna being longitudinal and one being
lateral. The ADF antennas must be able to receive signals in the 190 kHz to
1750 kHz range.
Part Number Differences: Part Number | Detects Audio | Detects Bearing Info | Maintenance Fault Memory | Sign Status Matrix Delay | Sense-To-Loop Ratio | SB 1 | SB 3 | SB 4 | SB 5 | SB 6 | SB 7 | SB 8 | SB 9 | SB 10 | SB 11 | SB 12 | SB 13 | SB 16 | SB 17 | SB 18 | SB 19 | SB 20 | SB 24 | SB 25 | SB 26 | SB 29 | SB 30 | SB C | SB D | SB E | SB F |
622-5222-001 | Yes | Yes | No | No | Standard | Yes | Yes | Yes | Yes | Yes | Yes | No | No | No | Yes | Yes | Yes | No | No | No | Yes | No | No | No | No | Yes | Yes | No | No | No | No |
622-5222-002 | Yes | Yes | Yes | Yes | Standard | No | No | Yes | No | Yes | Yes | No | No | Yes | Yes | Yes | Yes | Yes | Yes | Yes | Yes | Yes | No | No | Yes | Yes | Yes | No | Yes | No | No |
622-5222-020 | Yes | Yes | Yes | Yes | Standard | No | No | Yes | No | Yes | Yes | No | No | Yes | Yes | Yes | Yes | Yes | Yes | Yes | Yes | Yes | No | No | Yes | Yes | Yes | No | No | No | No |
622-5222-102 | Yes | Yes | Yes | Yes | Standard | No | No | No | No | No | No | Yes | Yes | No | Yes | Yes | Yes | Yes | Yes | Yes | Yes | Yes | Yes | Yes | Yes | Yes | Yes | No | No | No | No |
622-5222-120 | Yes | Yes | No | No | Standard | Yes | Yes | Yes | Yes | Yes | Yes | No | No | No | Yes | Yes | Yes | No | No | No | Yes | No | No | No | No | Yes | Yes | Yes | No | Yes | No |
622-5222-420 | Yes | Yes | Yes | Yes | Use With Bae 146/RJ Aircraft | No | No | Yes | No | Yes | Yes | No | No | Yes | Yes | Yes | Yes | Yes | Yes | Yes | Yes | Yes | No | No | Yes | Yes | Yes | No | No | No | Yes |