1 . PROPELLER BRAKE. THE PROPELLER BRAKING SYSTEM ALLOWS THE RIGHT ENGINE TO BE SAFELY USED AS A DC GENERATOR AND GROUND AIR CONDITIONING. THE PROPELLER BRAKING SYSTEM IS A HYDROMECHANICAL SYSTEM INSTALLED ON THE RIGHT ENGINE GEARBOX ALLOWING TO STOP THE PROPELLER AND THE POWER TURBINE. HYDRAULIC POWER FOR THE PROPELLER BRAKE IS PROVIDED BY THE BLUE HYDRAULIC SYSTEM AT 3000 PSI (207 BAR). PRESSURE IS GENERATED BY EITHER THE BLUE HYDRAULIC PUMP POWERED BY AC MAINS OR THE AUXILIARY HYDRAULIC PUMP POWERED BY DC MAINS. FOR CIVIL AVIATION.
1 . PROPELLER BRAKE. THE PROPELLER BRAKING SYSTEM ALLOWS THE RIGHT ENGINE TO BE SAFELY USED AS A DC GENERATOR AND GROUND AIR CONDITIONING. THE PROPELLER BRAKING SYSTEM IS A HYDROMECHANICAL SYSTEM INSTALLED ON THE RIGHT ENGINE GEARBOX ALLOWING TO STOP THE PROPELLER AND THE POWER TURBINE. HYDRAULIC POWER FOR THE PROPELLER BRAKE IS PROVIDED BY THE BLUE HYDRAULIC SYSTEM AT 3000 PSI (207 BAR). PRESSURE IS GENERATED BY EITHER THE BLUE HYDRAULIC PUMP POWERED BY AC MAINS OR THE AUXILIARY HYDRAULIC PUMP POWERED BY DC MAINS. FOR CIVIL AVIATION.
10-June-2022
8411990091
1 . ENGINE EXHAUST DEVICE (SERVES TO DIRECTION OF AIR FLOW FROM ENGINE TURBINE AND SUPPRESSION OF EXHAUST JET NOISE) FOR CIVIL AVIATION ACFT
1 . ENGINE EXHAUST DEVICE (SERVES TO DIRECTION OF AIR FLOW FROM ENGINE TURBINE AND SUPPRESSION OF EXHAUST JET NOISE) FOR CIVIL AVIATION ACFT
14-September-2022
3403990000
1 . AVIATION TURBINE OIL
1 . AVIATION TURBINE OIL
26-September-2022
8411990098
1 . THE FUEL SUPPLY REGULATOR IS THE UNIT CONTROLLING THE SUPPLY OF FUEL TO THE ARMED FORCES OF UKRAINE (GAS TURBINE ENGINE POWER OF 1 47 KW) CONSISTS OF: FUEL PUMP LOW -PRESSURE FILTER LIMITER OF DYNAMIC OVERLOAD CENTRIFUGAL REGULATOR VACCINATE AND UNLOADING VALVES IS PART OF THE GAS TURBINE ENGINE AIRCRAFT INSTALLED ON THE AIRCRAFT APU DRIVE BOX FOR TECH. MAINTENANCE AND/OR REPAIR OF B737 CIVIL AVIATION AIRCRAFT. BOO. PART NUMBER 361 7750-1
1 . THE FUEL SUPPLY REGULATOR IS THE UNIT CONTROLLING THE SUPPLY OF FUEL TO THE ARMED FORCES OF UKRAINE (GAS TURBINE ENGINE POWER OF 1 47 KW) CONSISTS OF: FUEL PUMP LOW -PRESSURE FILTER LIMITER OF DYNAMIC OVERLOAD CENTRIFUGAL REGULATOR VACCINATE AND UNLOADING VALVES IS PART OF THE GAS TURBINE ENGINE AIRCRAFT INSTALLED ON THE AIRCRAFT APU DRIVE BOX FOR TECH. MAINTENANCE AND/OR REPAIR OF B737 CIVIL AVIATION AIRCRAFT. BOO. PART NUMBER 361 7750-1