Customs Search

NOSE WHEEL STEERING HANDWHEEL TRANSMITTER UNIT, FOR AN AIRCRAFT. THE UNIT IS USED TO CONTROL THE DIRECTION OF THE AIRCRAFT WHEN ON THE GROUND. THE UNIT IS INSTALLED IN THE COCKPIT OF THE AIRCRAFT, A LEFT HAND VERSION FOR THE CAPTAIN, A RIGHT HAND VERSION FOR THE FIRST OFFICER. THE UNIT CHANGES THE POSITION OF THE STEERING HANDLE INTO A VOLTAGE. THIS VOLTAGE IS TRANSMITTED TO THE BRAKE STEERING CONTROL UNIT (BSCU), WHICH CONTROLS THE STEERING ANGLE OF THE NOSE WHEEL OF THE AIRCRAFT. AVAILABLE IN STANDARD, ILLUMINATED AND DAMPED VERSIONS LEFT AND RIGHT.

THE ECAM CONTROL PANEL IS A SUBASSEMBLY OF THE ELECTRONIC CENTRALIIZED AIRCRAFT MONITORING SYSTEM, WHICH IS USED TO PROVIDE THE CREW IN ENERGISZING AND ADJUSTING THE BRIGHTNESS OF THE DISPLAY UNIT, MANUAL PRESENTATION OF PAGES FOR DEALING WITH WARNING OR DISPLAY SYSTEMS, REACTIVATION OF CERTAIN CLEARED WARNINGS, TESTING OF TAKING-OFF CONFIGERATION.

A CABIN INTERCOMMUNICATION DATA SYSTEM (CIDS) DIRECTOR, AN INTERFACE BETWEEN THE COCKPIT AND THE SYSTEMS OF THE ELECTRONIC DEPARTMENT, THE CIDS DATA BUS WITH THE CONNECTED DECODER ENCODER UNITS (DEU) TO THE CABIN SYSTEM, THE FORWARD ATTENDANT PANEL (FAP) AND THE PROGRAMMING AND TEST PANEL (PTP). THE DIRECTOR CONTROLS MANY FUNCTIONS OF THE CONNECTED CABIN SYSTEMS, SUCH AS LOGIC, CHIMES, SWITCHING AND DISTRIBUTION. IT HAS AN ALUMINIUM CHASSIS AND ELECTRICAL SUBASSEMBLIES. INPUT VOLTAGE 18 VDC TO 31.5 VDC (NORM. 28 VDC). DIMENSIONS: 194 H X 90.4 W X 324 L MM. WEIGHT: 4.8 KG MAX.

A SMOKE DETECTOR CONTROL UNIT - SDCU FOR AIRBUS A340 ALSO COMMON TO AIRBUS A330 CIVIL AIRCRAFT. THE SDCU HAS THE FOLLOWING FUNCTIONS - TO MONITOR AND PROCESS THE SIGNALS OF THE SMOKE DETECTORS FOR THE AVIONICS SMOKE DETECTION SYSTEM, LDCC SMOKE-DETECTION SYSTEM, LAVATORY SMOKE-DETECTION SYSTEM. TO MONITOR THE FIRE EXTINGUISHING SYSTEM. TO SUPPLY THE DETECTORS WITH A CONTROLLED VOLTAGE THROUGH A TWO WIRE SAFETY BUS SYSTEM. IT IS PROTECTED AGAINST ONE SHORT CIRCUIT OR ONE OPEN CIRCUIT BETWEEN TWO SMOKE DETECTORS ON EACH BUS LOOP, WITHOUT THE LOSS OF THE DETECTOR FUNCTION. THIS UNIT HAS NO SOUND OR VISUAL SIGNAL, THE UNIT JUST PASSES THE ELECTRICAL SIGNAL TO OTHER APPARATUS WITHIN THE SYSTEM TO PROVIDE THE WARNING. THE SYSTEM DOES NOT CONTAIN ANY RADIOACTIVE SUBSTANCE.

A SMOKE DETECTOR CONTROL UNIT - SDCU FOR AIRBUS A340 ALSO COMMON TO AIRBUS A330 CIVIL AIRCRAFT. THE SDCU HAS THE FOLLOWING FUNCTIONS - TO MONITOR AND PROCESS THE SIGNALS OF THE SMOKE DETECTORS FOR THE AVIONICS SMOKE DETECTION SYSTEM, LDCC SMOKE-DETECTION SYSTEM, LAVATORY SMOKE-DETECTION SYSTEM. TO MONITOR THE FIRE EXTINGUISHING SYSTEM. TO SUPPLY THE DETECTORS WITH A CONTROLLED VOLTAGE THROUGH A TWO WIRE SAFETY BUS SYSTEM. IT IS PROTECTED AGAINST ONE SHORT CIRCUIT OR ONE OPEN CIRCUIT BETWEEN TWO SMOKE DETECTORS ON EACH BUS LOOP, WITHOUT THE LOSS OF THE DETECTOR FUNCTION. THIS UNIT HAS NO SOUND OR VISUAL SIGNAL, THE UNIT JUST PASSES THE ELECTRICAL SIGNAL TO OTHER APPARATUS WITHIN THE SYSTEM TO PROVIDE THE WARNING. THE SYSTEM DOES NOT CONTAIN ANY RADIOACTIVE SUBSTANCE.