1/29/2022 | 8482200009 | BEARINGS WITH TAPERED ROLLERS INTENDED FOR COMPLETING AND REPAIRING HELICOPTERS SERIES MI OF MOTOR SICH AIRLINES, NOT FOR MILITARY PURPOSE, SHKH15-SH STEEL | 5.11 | 2083.54 | Ukraine | G SARATOV MARX | TD EPK LLC |
1/27/2022 | 8481808199 | TWO-POSITION CRANE WITH ELECTROMAGNETIC CONTROL FOR POWER ON OF HYDRAULIC BOOSTER, FOR CIVIL HELICOPTERS MI-8/17/171 | 1.38 | 3920.84 | China | BEIJING AIRPORT BEIJING PRCHINA | AVIAHELP LLC |
1/27/2022 | 8414592000 | AXIAL FANS FOR CIVIL HELICOPTERS MI-8/17/171 | 0.64 | 2967.24 | China | BEIJING AIRPORT BEIJING PRCHINA | AVIAHELP LLC |
1/13/2022 | 8483105000 | THE CARDAN SHAFT OF THE FAN DRIVE IS INTENDED TO TRANSMISSION OF TORQUE FROM THE MAIN REDUCER DRIVE OF THE MI-171 CIVIL AVIATION HELICOPTER. SECOND-HAND. SUPPLIED AFTER REPAIRED. | 3.4 | 5503.5 | Uzbekistan | ST PETERSBURG RUSSIA | VERTO LLC |
1/13/2022 | 8413603100 | ROTARY GEAR PUMPS ARE DESIGNED FOR INJECTION OF LIQUID INTO THE CIVIL AVIATION HELICOPTER HYDRAULIC SYSTEM. USED. SUPPLIED AFTER REPAIRED. | 8.4 | 5403.5 | Uzbekistan | ST PETERSBURG RUSSIA | VERTO LLC |
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 |
1/26/2022 | 8483902009 | FLANGE IN STEEL 3.4364 FOR CONNECTING TWO STRUCTURAL ELEMENTS. DETAIL OF THE CONTROL SYSTEM OF THE CIVIL PASSENGER HELICOPTER AGUSTAVESTLAND AW139 . 1653-0030/10228238-15pcs. | 3 | 1769.32 | Germany | LINDENBERG IM ALLGOY | GIDRAVLIKA ENGINEERING SERVICE LLC |
1/17/2022 | 8481101908 | STEEL REDUCER VALVES NOT CONTAINING RADIOACTIVE SOURCES OF IONIZING RADIATION INTENDED TO REGULATE AIR PRESSURE IN THE BRAKING SYSTEM OF CIVIL AVIATION HELICOPTER MI-171E: ACCELERATOR REDUCTION UP03/2M (FORMER V | 1.56 | 4824.38 | United States of America | POOLVILLE TEXAS USA | AVIA SYSTEMS LLC |
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 |