1 . RETRACTABLE LANDING LIGHT (THE CYLINDRICAL SHAPE WITH A HEADLIGHT RELEASE/RETRACT MECHANISM AND ELECTRICAL CONNECTOR) SERVES TO LIGHT THE RUNWAY WHEN LANDING A CIVIL AVIATION AIRCRAFT
1 . RETRACTABLE LANDING LIGHT (THE CYLINDRICAL SHAPE WITH A HEADLIGHT RELEASE/RETRACT MECHANISM AND ELECTRICAL CONNECTOR) SERVES TO LIGHT THE RUNWAY WHEN LANDING A CIVIL AVIATION AIRCRAFT
1 . LANDING LIGHT (AIRWAY LIGHTING DURING APPROACH TAXIING AND TAKEOFF) FOR CIVIL AVIATION ACFT
1 . LANDING LIGHT (AIRWAY LIGHTING DURING APPROACH TAXIING AND TAKEOFF) FOR CIVIL AVIATION ACFT
05-April-2022
9405920008
1 . REAR COVER - LIGHTING LAMP FOR THE REAR LOBBY OF A PASSENGER AIRCRAFT FROM PLASTIC FOR TECH. MAINTENANCE AND/OR REPAIR OF B737 CIVIL AVIATION AIRCRAFT. PART NUMBER 239004-1 9
1 . REAR COVER - LIGHTING LAMP FOR THE REAR LOBBY OF A PASSENGER AIRCRAFT FROM PLASTIC FOR TECH. MAINTENANCE AND/OR REPAIR OF B737 CIVIL AVIATION AIRCRAFT. PART NUMBER 239004-1 9
05-April-2022
8536619000
1 . LAMP HOLDER (CARTRIDGE) - WITH ELECTRIC CONNECTING WIRES (COPPER STRANDED IN PLASTIC INSULATION WITH A SECTION OF 4 SQ. MM) FOR A TUBULAR DOUBLE-ENDED FLUORESCENT LIGHTING OF THE AIRCRAFT CABIN. SUPPLY VOLTAGE 1 1 5 VOLT / 400 HERTZ FOR TECH. MAINTENANCE AND/OR REPAIR OF B737 CIVIL AVIATION AIRCRAFT. PART NUMBER BV03031 D01 -24
1 . LAMP HOLDER (CARTRIDGE) - WITH ELECTRIC CONNECTING WIRES (COPPER STRANDED IN PLASTIC INSULATION WITH A SECTION OF 4 SQ. MM) FOR A TUBULAR DOUBLE-ENDED FLUORESCENT LIGHTING OF THE AIRCRAFT CABIN. SUPPLY VOLTAGE 1 1 5 VOLT / 400 HERTZ FOR TECH. MAINTENANCE AND/OR REPAIR OF B737 CIVIL AVIATION AIRCRAFT. PART NUMBER BV03031 D01 -24
29-April-2022
8407100003
1 . ENGINE FOR THE CORVETA-AT AND CORVETTE-B3 CIVILIAN LIGHT AIRCRAFT THE JABIRU-2200 AVIATION ENGINE-85 L. S. INTERNAL COMBUSTION FOUR-STROKE 4-CYLINDER HORIZONTAL-OPPOSITE 1 CENTRAL CAMSHAFT GAS DISTRIBUTION MECHANISM WITH PUSHING RODS AND NON-SURVEYOR . JABIRU AIRCRAFT ENGINES ARE DESIGNED FOR INSTALLATION ON LIGHT AND ULTRA LIGHT AIRCRAFT POWER – 63 KW NO MORE THAN THREE SEATS MAX. ENGINE SPEED 3300RPM
1 . ENGINE FOR THE CORVETA-AT AND CORVETTE-B3 CIVILIAN LIGHT AIRCRAFT THE JABIRU-2200 AVIATION ENGINE-85 L. S. INTERNAL COMBUSTION FOUR-STROKE 4-CYLINDER HORIZONTAL-OPPOSITE 1 CENTRAL CAMSHAFT GAS DISTRIBUTION MECHANISM WITH PUSHING RODS AND NON-SURVEYOR . JABIRU AIRCRAFT ENGINES ARE DESIGNED FOR INSTALLATION ON LIGHT AND ULTRA LIGHT AIRCRAFT POWER – 63 KW NO MORE THAN THREE SEATS MAX. ENGINE SPEED 3300RPM