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 | 8412218008 | ARTICLE 109-0112-39-105 DAMPER (US) FOR CIVIL HELICOPTER AW109SP. INTENDED FOR DAMPING HELICOPTER HULL VIBRATIONS WHEN LANDING. IS AN EXTENDED CYLINDER. ON ONE SIDE FASTENING TO THE FUSELAGE, ON THE OTHER SIDE M | 10 | 22646.7 | Italy | VERGIATE VA ITALY | ALLIANCE AVIATEKHNOSERVICE LLC |
1/5/2022 | 8412218008 | SPARE PARTS OF CIVIL HELICOPTERS MI-171 AND MI-17-1V ARE EXPORTED AFTER REPAIR: | 0.96 | 243.7 | United Arab Emirates | DUBAI | AVIAENGINEERING LLC |
1/31/2022 | 8412218008 | NLG NOW CHASSIS RETRACTION ACTUATOR AS LINEAR ACTING HYDRAULIC CYLINDER IN BLACK METAL BODY FOR CIVIL HELICOPTER AGUSTA WESTLAND AW 189 OIL AND GAS PRODUCTION FACILITY - 1 PIECE | 8.77 | 41827.7 | Italy | UNKNOWN | EXXON NEFTEGAZ LIMITED |
1/13/2022 | 8412218008 | COMBINED HYDRAULIC STEERING GEAR, MOD. KAU-115AM - 2 pcs., SER. No. 1111549, 1111551, DESIGNED FOR REDUCING EFFORT ON CONTROLS, SECOND-HAND, EXPORTED AFTER REPAIR, FOR CIVIL AVIATION TO THE MI-17 (MI-171) HELICOPTER, NOT MILITARY | 20.52 | 2606.56 | Czechia | MOSCOW RUSSIA | AEROTECHSERVICE BRANCH LLC |