| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-21 | 8411210009 | PART TYPE sun Civil Aviation DHC6-400 SER.â„– 881: airplane turboprop, MODEL PT6A-34 SER.â„– PCE-RB0707, a power of 620 (462.5 KW) .On AIRCRAFT ENGINE INSTALLED 2 PT6A-34. The engine consists of PROPELLER WITH REDUCTION GEAR: M | *** | RUSSIA | 147 | 777707,97 | *** | ***** | ***** |
| 2017-09-27 | 9029100009 | CATEGORY 4.2. PROPERTY IN THE LIST â„–GP-13132051379-07515014-0058: Instruments for determining the magnitude of the step of the main rotor of a military helicopter Mi-35M, no electronic:: INDEX pitch propellers JSC "AVIAAVTOMATIKA" NO USHV-1K SERIES February 1 | *** | RUSSIA | 0.3 | 518,11 | *** | ***** | ***** |
| 2017-09-28 | 8411210009 | PART TYPE sun Civil Aviation DHC6-400 SER.â„– 881: airplane turboprop, MODEL PT6A-34 SER.â„– PCE-RB0708, a power of 620 (462.5 KW) .On AIRCRAFT ENGINE INSTALLED 2 PT6A-34. The engine consists of PROPELLER with gear: K | *** | RUSSIA | 147 | 779304,29 | *** | ***** | ***** |
| 2017-10-03 | 8413603900 | PUMP B / N 4122-006002, b / y, VOLUME ROTARY gear type, for voltage 28VDC, DUTY CYCLE: 30sec FOR 10min. (Are motorized) FOR SUBMISSION OF AVIATION OIL SYSTEM feathering propeller operating pressure | ABSENT | *** | 1.85 | 500 | MOSCOW | ***** | ***** |
| 2017-10-03 | 8413603900 | PUMP B / N 4122-006002, b / y, VOLUME ROTARY gear type, for voltage 28VDC, DUTY CYCLE: 30sec FOR 10min. (Are motorized) FOR SUBMISSION OF AVIATION OIL SYSTEM feathering propeller operating pressure | ABSENT | *** | 1.85 | 500 | MOSCOW | ***** | ***** |
| 2017-10-11 | 8411910008 | PART B / C TYPE DHC6-400 CIVIL AVIATION: LEVER REVERSE, CHERT.â„– 3,012,526, is an integral part of the mechanism to control the reversal of the propeller, is designed to manage name a mechanism. IMPACT ON THE LEVER REVERSE propeller is carried out from | Trademarks are not marked | *** | 0.2 | 1022,21 | TORONTO | ***** | ***** |
| 2017-10-11 | 8411910008 | PART B / C TYPE DHC6-400 CIVIL AVIATION: LEVER REVERSE, CHERT.â„– 3,012,526, is an integral part of the mechanism to control the reversal of the propeller, is designed to manage name a mechanism. IMPACT ON THE LEVER REVERSE propeller is carried out from | Trademarks are not marked | *** | 0.2 | 1022,21 | TORONTO | ***** | ***** |
| 2017-10-23 | 8412218008 | UNIT B / N 815585-7, D / I, provides a hydraulic cylinder linear action, is designed to control the propeller BC, REPAIR AND MAINTENANCE commercial aircraft ATR72. SCOPE-CIVIL AVIATION | OTCUTSTVUET | *** | 14.5 | 500 | MOSCOW | ***** | ***** |
| 2017-10-23 | 8412218008 | UNIT B / N 815585-7, D / I, provides a hydraulic cylinder linear action, is designed to control the propeller BC, REPAIR AND MAINTENANCE commercial aircraft ATR72. SCOPE-CIVIL AVIATION | OTCUTSTVUET | *** | 14.5 | 500 | MOSCOW | ***** | ***** |
| 2017-10-26 | 8412298909 | HYDROMECHANICAL MODULE (GEAR) propeller engine. Party. NUMBER S146440-2.PREDNAZNACHEN FOR REPAIR AND MAINTENANCE OF PASSENGER AIRCRAFT CIVIL AVIATION ATR 42-500 | *** | *** | 7 | 37844,78 | PARIS | ***** | ***** |