1/18/2022 | 8412904008 | CYLINDER ASSEMBLY (14 PCS) FOR USE IN THE HYDRAULIC SYSTEM OF INTERCEPTOR DRIVE, AILERON DRIVE ON CIVIL SUPERJET AIRCRAFT: : | 45.44 | 33792.2 | Germany | LINDENBERG IM ALLGOY | GIDROAGREGAT JSC |
1/19/2022 | 8412212009 | RUDDER SERVO. ARTICLE NO. 11043071. 33 PCS. PART NO. 810D0000-01. OVERALL DIMENSIONS: 570 X 260 MM. MECHANICAL-HYDRAULIC. INSTALLED IN THE TAIL ON AIRBUS A319, 320, 321 CIVIL AIRCRAFT. USED FOR THE SYSTEM | 189.75 | 171825.1 | Germany | Ummendorf Germany | LIBHERR AEROSPACE NIZHNY NOVGOROD LAN LLC |
1/26/2022 | 7307298009 | JOINT FROM STEEL 15-5??, SERVES TO CONNECT TWO PARTS, PART OF CONTROL SYSTEM FOR CIVIL PASSENGER AIRCRAFT BD 100 , 1751-0002/079332350-48PCS. | 3 | 1059.04 | Germany | LINDENBERG IM ALLGOY | GIDRAVLIKA ENGINEERING SERVICE LLC |
1/17/2022 | 8481401000 | STEEL BLEED (SAFETY) VALVE FOR THE AIR BLEEDING SYSTEM FROM THE ENGINE OF APU A321 OF CIVIL AVIATION IS REMOVED FROM THE AIRCRAFT B/N VQ-BQH : | 2.58 | 18518.2 | Germany | RAUNHEIM GERMANY | PJSC AIRLINE SIBERIA |
1/26/2022 | 8481201009 | THE SERVO VALVE IS THE FLOW CONTROL DEVICE OF THE ELECTRO-HYDRAULIC SERVO VALVE THAT SUPPLYS THE REQUIRED HYDRAULIC FLOW TO THE SPOILER SYSTEM. IS A COMPONENT OF CIVIL PASSENGER AIRCRAFT RRJ-95 | 0.5 | 26046.8 | Germany | LINDENBERG IM ALLGOY | PJSC CORPORATION IRKUT |
1/27/2022 | 8807100000 | PROPELLER SPEED REGULATORS. TYPE P-883-82X SER. ?16G229HG/9/16-1PC. ARE A MECHANISM FOR ADJUSTING THE PITCH OF THE PROPELLER BLADE. INTENDED TO CONTROL THE TURN OF THE BLADES THROUGH THE HYDRO SYSTEM OF THE DIAM CIVIL AIRCRAFT | 1.5 | 143.06 | Germany | ATTING | SP PROPELLER SERVICE LLC |
1/26/2022 | 8412212009 | RUDDER SERVO. ARTICLE NO. 11043071. 30 PCS. PART NO. 810D0000-01. OVERALL DIMENSIONS: 570 X 260 MM. MECHANICAL-HYDRAULIC. INSTALLED IN THE TAIL ON AIRBUS A319, 320, 321 CIVIL AIRCRAFT. USED FOR THE SYSTEM | 172.5 | 154944.8 | Germany | Ummendorf Germany | LIBHERR AEROSPACE NIZHNY NOVGOROD LAN LLC |
1/12/2022 | 9025900008 | THE TEMPERATURE SENSOR (FAULT, REMOVED FROM THE ACFT) OF THE AIRPLANE TURBOJET ENGINE FIRE-FIGHTING SYSTEM. CONSISTS OF TWO HEAT-SENSITIVE ELEMENTS ASSEMBLY WITH ELECTRIC CABLE. INTENDED FOR MEASURING THE TEMPERATURE OF WORKING GASES AFTER | 1.34 | 13140.2 | Germany | DOMODEDOVO AIRPORT MOSCOW | AIRLINE ROYAL FLIGHT JSC |
1/13/2022 | 8421398006 | OZONE CONVERTER (FAIL, REMOVED FROM THE ACFT) - EQUIPMENT FOR FILTERING AND CLEANING THE AIR EXHAUSTED FROM THE TURBOJET ENGINE INTO THE AIRCRAFT CONDITIONING SYSTEM. IS A CATALYTIC TYPE FILTER STRUCTURALLY PERFORMED IN | 5.12 | 58116.8 | Germany | DOMODEDOVO AIRPORT MOSCOW | AIRLINE ROYAL FLIGHT JSC |
1/13/2022 | 9032200000 | HIGH PRESSURE CONTROLLER (FAULT, REMOVED FROM ACFT) OF AIRCRAFT PNEUMATIC SYSTEM. IS A MANOSTAT, MEMBRANE, ELECTROMECHANICAL. CONSISTS OF STEEL BODY, PNEUMATIC SWITCH, SHUT-OFF SOLENOID VALVE WITH | 1.9 | 31199.4 | Germany | DOMODEDOVO AIRPORT MOSCOW | AIRLINE ROYAL FLIGHT JSC |