The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2The aircraft has two ATC transponders which are controlled by a dual control box on the center pedestal. Only the selected ATC transponder operates. The associated ADIRS (1 for transponder 1, etc ...) supplies the altitude for altitude reporting. The ATC transponder is capable of enhanced surveillance: It transmits the following parameters upon ground request: - Indicated airspeed, Mach number, and baro vertical speed, that are all supplied by the ADRs. - Magnetic heading, roll angle, ground speed, track angle, track angle rate, and inertial vertical speed, that are all supplied by the IRs. - Selected altitude and barometric reference settings supplied by the FCUs. In the case of an ADR (1 or 2) failure, ADR 3 replaces the faulty ADR, when the AIR DATA SWITCHING Selector is set to CAP on 3 or F/O on 3. IR/FCU parameters are only transmitted to: - ATC 1 by IR 1/FCU 1 - ATC 2 by IR 2/FCU 2
