1/18/2022 | 8412904008 | PISTON (174 PCS) FROM CORROSION-RESISTANT STEEL FOR USE IN HYDRAULIC CYLINDERS OF STEERING UNITS ON CIVIL HELICOPTERS H135 WITH A MAXIMUM TAKE-OFF WEIGHT OF 3000 KG: : | 21.96 | 42387.2 | Germany | LINDENBERG IM ALLGOY | GIDROAGREGAT JSC |
1/18/2022 | 8412904008 | ROD (74 PCS) OF CORROSION-RESISTANT STEEL FOR USE IN HYDRAULIC CYLINDERS OF STEERING ASSEMBLY ON CIVIL HELICOPTERS EC-135 WITH A MAXIMUM TAKE-OFF WEIGHT OF 2950 KG AND ON CIVIL SUPERJET AIRCRAFT: : | 22.73 | 21969.9 | Germany | LINDENBERG IM ALLGOY | GIDROAGREGAT JSC |
1/15/2022 | 8412218008 | HYDRAULIC BOOSTER H/N SC5072 S/N 3216 (MY 2013) OF LINEAR ACTION, SERVES TO REMOVE LOADS FROM TAIL AND MAINTENANCE ROTOR COMMAND LEVER, FOR AS-350?3 RA-04054 CIVIL HELICOPTER | 2.21 | 1202.7 | United States of America | MERIDIAN ROAD HOP | UTair ENGINEERING JSC |
1/15/2022 | 8412218008 | HYDRAULIC BOOSTER H/N SC5083-1 S/N 4820 (MY 2011) OF LINEAR ACTION, SERVES TO REMOVE LOADS FROM TAIL AND MAINTENANCE ROTOR COMMAND LEVER, AFTER REPAIR, FOR CIVIL HELICOPTER AS350?3 RA-07208 | 2.24 | 1227.7 | United States of America | MERIDIAN ROAD HOP | UTair ENGINEERING JSC |
1/15/2022 | 8412218008 | LINEAR ACTING HYDRAULIC CYLINDER H/N SC8042 S/N 2919 (MY 2012) IS A LINEAR ACTING HYDRO CYLINDER WITH A DUAL HYDRAULIC SYSTEM DESIGNED TO TRANSFER FORCES FROM THE HELICOPTER CONTROLS TO THE ROTOR BLADE AND SERVES FOR | 4.24 | 3102.7 | United States of America | MERIDIAN ROAD HOP | UTair ENGINEERING JSC |
1/15/2022 | 8412218008 | HYDRAULIC BOOSTER H/N SC8043 C/N 1747 (MY 2014) OF LINEAR ACTION, DESIGNED FOR RELIEF OF LOADS FROM HELICOPTER CARRYING SYSTEM COMMAND LEVER IN CHANNELS OF LONGITUDINAL, TRANSVERSAL, TRAIL CONTROL WITH A COMMON PITCH, FOR MAINTENANCE MAINTENANCE | 4.8 | 1981.7 | United States of America | MERIDIAN ROAD HOP | UTair ENGINEERING JSC |
1/15/2022 | 8412218008 | HYDRAULIC BOOSTER H/N SC8043 C/N 1540 (MY 2012) OF LINEAR ACTION, DESIGNED FOR RELIEF OF LOADS FROM HELICOPTER CARRYING SYSTEM COMMAND LEVER IN CHANNELS OF LONGITUDINAL, TRANSVERSAL, TRAIL CONTROL WITH A COMMON PITCH, FOR MAINTENANCE MAINTENANCE | 4.74 | 1981.7 | United States of America | MERIDIAN ROAD HOP | UTair ENGINEERING JSC |
1/18/2022 | 8412218008 | ARTICLE 109-0112-05-107 DAMPER (US) FOR CIVIL HELICOPTER AW119MKII. PURPOSE OF EXPORT: RETURN OF A DEFECTIVE UNIT IN REPLACEMENT OF THE RECEIVED GOOD UNIT. INTENDED FOR DAMPING HELICOPTER HULL VIBRATIONS WHEN LANDING. | 7.2 | 17137.8 | Italy | VERGIATE VA ITALY | ALLIANCE AVIATEKHNOSERVICE LLC |
1/25/2022 | 8412904008 | ARTICLE 109-0110-42-136 HYDRAULIC POWER (US) FOR CIVIL HELICOPTER AW109SP. PURPOSE OF EXPORT: RETURN OF A DEFECTIVE UNIT IN REPLACEMENT OF THE RECEIVED GOOD UNIT. INTENDED TO REDUCE THE EFFORT FROM THE HELICOPTER CONTROLS. IS A METALLIC | 5.1 | 5663.7 | Italy | VERGIATE VA ITALY | ALLIANCE AVIATEKHNOSERVICE LLC |
1/25/2022 | 8412904008 | PART NUMBER 109-0110-42-134 HYDRAULIC POWER (USED) FOR CIVIL HELICOPTER AW109SP. PURPOSE OF EXPORT: RETURN OF A DEFECTIVE UNIT IN REPLACEMENT OF THE RECEIVED GOOD UNIT. INTENDED TO REDUCE THE EFFORT FROM THE HELICOPTER CONTROLS. IS A METALLIC | 5.1 | 5663.7 | Italy | VERGIATE VA ITALY | ALLIANCE AVIATEKHNOSERVICE LLC |