The SDAC (System Data Acquisition Concentrator) is a subassembly of the ECAM (Electronic Centralized Aircraft Monitoring) system. This system provides the crew with operational assistance for both the normal and abnormal aircraft system configurations. This operational assistance is given through visual and aural attention getters devices and through the two ECAM Display Units by means of messages and system synoptic diagrams.

The Slat/Flap Control Computer (SFCC) provide one half of the control and monitoring electronics for the A320, A321 or A319 slat and flap hydromechanical drive system. There are two SFCC units fitted in the aircraft, each of which contains two identical independent channels, one dedicated to slat control and one dedicated to flap control. Each channel consists of two lanes, which drive the solenoid valves of one of the two hydraulic motors in the Power Control Unit (PCU) which, via the differential gear, transverse torque shafts and rotary actuators, operate the slat or flap surfaces.

An underwater locator beacon (ULB) is a specialized device designed to aid in locating and recovering aircraft or maritime assets that have submerged or crashed into water. It is commonly used in aviation and maritime industries to enhance search and rescue operations. The ULB is typically attached to the aircraft’s or vessel’s flight data recorder (FDR) or cockpit voice recorder (CVR) to facilitate their retrieval in case of an accident.

The Integrated Standby Flight Display (ISFD) receives the data from the Air Data and Inertial Reference Unit (ADIRU), the Multi-Mode Receiver (MMR), and the Instrument Landing System (ILS) through the ARINC 429 busses to calculate and show the air data that follows..

The MCDU helps the flight crew to operate the aircraft by supplying the data entry and display functions necessary for interactive control of the FMCS, ADAS, and CFDs systems. September 2022 triple release (FAA, EASA, and CAAC) in stock and ready to ship!

The CG1093AD Inertial Reference Mode Panel (IRMP) provides mode control, status indication, initialization data input, and information display for up to three Inertial Reference Units (IRUs) or three Air Data Inertial Reference Units (ADIRUs). Together, the IRMP and the IRUs make up the Inertial Reference System (IRS). Together, the IRMP and the ADIRUs make up the Air Data Inertial Reference System (ADIRS).

The EPS will supply four fused controlled outputs or uncontrolled outputs. The EPS battery pack will supply either controlled outputs or, if a link is connected across pins 18 and 24 of connector J1, uncontrolled outputs.

Audio Control Panel is standard equipment aboard the 777 and 767-400 aircraft. The panel features a full liquid seal which eliminates the harmful effects of coffee spills. The panel communicates to AvtechTyee’s 5700 series of Audio Management Unit via an ARINC 429 data bus. All lighting is accomplished via LEDs.

The Cabin Pressure Controller is the essential part of the cabin pressure control system. It automatically controls in combination with associated aircraft systems the cabin pressure and the rate of pressure change.

The Cabin Pressure Controller is the essential part of the cabin pressure control system. It automatically controls in combination with associated aircraft systems the cabin pressure and the rate of