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SILK WAY AIRLINES TRADE DATA ANALYSIS

Access comprehensive trade data for Silk Way Airlines with ease. Explore trade shipments, top suppliers & buyers, and values without the hassle.

Silk Way Airlines – Overview

Eximpedia analyzes Silk Way Airlines export and import records, including data from 1 buyers and 1 suppliers. We provide an intelligence report of Silk Way Airlines that covers trade statistics, shipment values, quantities, exporters & importers and trade destinations

Silk Way Airlines Buyers, Suppliers & Shipments

Silk Way Airlines import markets

Explore the Silk Way Airlines import market with monthly import values, major importers, HS Codes, key ports, top suppliers, and competitors

TOP IMPORT HS CODE

HS CODE USD VALUE SHIPMENTS %
8411128009 0.68 2 11.76
TURBO-JETS, TURBO-PROPELLERS AND OTHER GAS TURBINES
8413302008 0.10 1 5.88
PUMPS FOR LIQUIDS, WHETHER OR NOT FITTED WITH A MEASURING DEVICE; LIQUID ELEVATORS
9032890000 0.06 2 11.76
AUTOMATIC REGULATING OR CONTROLLING INSTRUMENTS AND APPARATUS
8413506900 0.02 1 5.88
PUMPS FOR LIQUIDS, WHETHER OR NOT FITTED WITH A MEASURING DEVICE; LIQUID ELEVATORS
8411910008 0.01 1 5.88
TURBO-JETS, TURBO-PROPELLERS AND OTHER GAS TURBINES

TOP IMPORT COUNTRY

COUNTRY USD VALUE SHIPMENTS %
RUSSIAN FEDERATION 0.89 17 100.00

TOP IMPORT PORTS

PORT NAME USD VALUE SHIPMENTS %
PERMIAN 0.89 17 100.00

TOP IMPORT COMPETITORS

COMPANY USD VALUE SHIPMENTS
VOLGA DNEPR AIRLINE LLC 10.84 41
LLC PROTEKTOR 23.98 10
PJSC UEC UMPO 30.15 3
INFORM SERVICE LLC 43.19 2
LLC ASSOCIATION OF SUPPLIERS 57.63 3901

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Silk Way Airlines Import Shipments

Discover the Silk Way Airlines with product description, import values, quantities, exporter name, country of origin and key destinations.

HSN Code Product Description Imports Exporter Origin Destination Qty.
8481101908 THERMAL VALVE GA133-100-6K, NO. 0900104. 0270086, 0130137 - 3 PCS. PREDN lock lock RUSSIAN FEDERATION RUSSIA 0
8481101908 THERMAL VALVE GA133-100-6K, NO. 0900104. 0270086, 0130137 - 3 PCS. DESIGNED TO PROTECT THE HYDRAULIC SYSTEM OF CIVIL AVIATION ENGINE PS-90A-76 FROM UNACCEPTABLE PRESSURE INCREASE (OVER 260+15 KGS/CM2) DUE TO THERMAL EXPANSION OF WORKING FLUID BY BYPASS OF WORKING FLUID INTO THE DRAIN LINE, IS INSTALLED INTO THE PIPE CONNECTOR ON THE LEFT SIDE OF THE ENGINE. NOMINAL PRESSURE IN THE DISCHARGE LINE MPA (KGS/SM2) - 21 (210), NOMINAL PRESSURE IN THE DRAIN LINE MPA (KGS/SM2) - 2(10). WORKING LIQUID - AMG10. USED IN THE PS-90A-76 CIVIL AVIATION ENGINE OF IL-76 TYPE AIRCRAFT. IMPORTED FOR RESEARCH AND REPAIR AT THE MANUFACTURING FACTORY. USED. IN OUT OF WORKING CONDITION. ARE IMPORTED COMPLETELY ACCORDING TO THE PRODUCT DATA SHEET. IS NOT A SPECIALLY DESIGNED OR PREPARED BELLOWS VALVE, MANUAL OR AUTOMATIC, STOP OR CONTROL, MADE OF UF6 RESISTANT MATERIALS, FOR INSTALLATION IN lock lock RUSSIAN FEDERATION RUSSIA 0
8483405109 BOX OF DRIVES MODULE 94-06-8015-01 NO. KP27507630500026 (ASSEMBLY WITH BMF-94 UNITS NO. BMF27530500036 WITH SP-0.6E NO. 4406736, BCA-94 NO. BCA27530500063)-1PC. SERVES FOR INSTALLATION AND FASTENING lock lock RUSSIAN FEDERATION RUSSIA 1
8413302008 PUMP-REGULATOR NR-90 - 1 PCS. IND NO. 10102919026. DESIGNED FOR SUPPLYING FUEL TO THE COMBUSTION CHAMBER OF CIVIL AVIATION ENGINE PS-90A OF IL-76 TYPE AIRCRAFT; SUPPLY OF HIGH PRESSURE FUEL TO THE HYDRAULIC CYLINDERS OF COMPRESSOR MECHANIZATION AND AIR BLEED CONTROL SYSTEMS ACCORDING TO SIGNALS GENERATED BY RED-90 AND HYDROMECHANICAL REGULATORS INCLUDED IN NR-90; ABOVE-SYSTEM LIMITATION OF HPC ROTOR ROTATION FREQUENCY AND AIR PRESSURE BEYOND HPC. CONSTRUCTIVELY CONSISTS OF THE FOLLOWING UNITS: - A SELECTION MECHANISM DESIGNED FOR SWITCHING THE MAIN AUTOMATION (OA) TO THE RESERVE AUTOMATION (RA) AND BACK, - A PLUNGER TYPE PUMP UNIT DESIGNED FOR CHI FUEL HIGH PRESSURE IN THE AUTOMATIC FUEL DISTRIBUTION ART-90 AND POWER HYDRAULIC CYLINDERS, - ENGINE OPERATING MODES SETTING UNIT, - FUEL CONSUMPTION CONTROL UNIT INTO THE COMBUSTION CHAMBER, - VNA CONTROL UNIT, - ALL-MODE ROTOR SPEED REGULATOR, - PHYSICAL SENSOR lock lock RUSSIAN FEDERATION RUSSIA 0
8413506900 PLUNGER PUMP NP89D-3 - 1 PC, IND, NO. N905B1. DESIGNED FOR INJURING AND MAINTAINING OPERATING PRESSURE OF HYDRAULIC FLUID IN THE HYDRAULIC SYSTEM FOR CONTROL SYSTEM OF THE REVERSING DEVICE OF AIRCRAFT ENGINE PS-90A-7 lock lock RUSSIAN FEDERATION RUSSIA 1
7326909807 PIPELINE 94-13-9407 - 1 PCS, ID NO. 7492036, DESIGNED FOR FUEL SUPPLY lock lock RUSSIAN FEDERATION RUSSIA 0
8481309108 94-10-994 AIR BYPASS VALVE IND NO. 706145-5Р2 - 1 PC. DESIGNED FOR D lock lock RUSSIAN FEDERATION RUSSIA 0
9032890000 ELECTRONIC ENGINE REGULATOR RED-90M - 1 PCS (IND. NO. 54308161239). IT IS PART OF THE ELECTRONIC PART OF THE PS-90A-76 ENGINE CONTROL SYSTEM FOR CIVIL AVIATION. DESIGNED TO DEVELOP CONTROL INFLUENCES ON ACTUATOR MECHANISMS. CONTROL THE POSITION OF THE FUEL DOSING NEEDLE OF THE PUMP-REGULATOR NR-90 AND THE PRESSURE IN THE DRIVE CYLINDERS OF THE INPUT GUIDING DEVICE BLADES, AND ALSO FOR FORMING DISCRETE ENGINE SYSTEMS CONTROL SIGNALS AT STARTING, LICE AND TRANSITIONAL MODES. CONSTRUCTIONALLY, THE REGULATOR IS MADE IN THE FORM OF A RECTANGULAR SECTION MONOBLOCK WITH OVERALL DIMENSIONS 200X200X515 MM WITH FOUR BRACKETS WITH SHOCK ABSORBERS FIXED ON THE SIDE WALLS FOR INSTALLATION ON THE ENGINE. POWER SUPPLY - FROM AN AUTONOMOUS GENERATOR AND TWO INDEPENDENT ONBOARD DC POWER SUPPLY SYSTEMS, VOLTAGE 27 V, POWER CONSUMPTION - NO MORE THAN 150VA. IMPORTED FOR INVESTIGATION AND REPAIR AT THE MANUFACTURING FACTORY. FORMER IN lock lock RUSSIAN FEDERATION RUSSIA 1
8481309108 94-10-994 AIR BYPASS VALVE IND NO. 706145-5Р2 - 1 PC. DESIGNED FOR BYPASSING AIR FROM THE HPC OF THE PS-90A-76 CIVIL AVIATION AIRCRAFT ENGINE. IT CONSISTS OF A CASE WITH A FLANGE AND A COVER, INSIDE THE CASE IS A DOUBLE-ACTING HYDRAULIC CYLINDER AND A PISTON WHICH IS CONNECTED TO A PLATE. CONDITIONAL DIAMETER OF THE VALVE FLOW SECTION IS 76 MM. OPERATING PRINCIPLE: TO OPEN THE VALVE, HIGH PRESSURE FUEL IS SENT INTO THE FITTING, AND THE FITTING IS CONNECTED WITH THE DRAIN. IN THIS WAY, THE PLATE MOVES DOWN FROM THE SEAT ON THE FLANGE AND OPENS THE PASSAGE FOR BYPASSED AIR FROM THE COMPRESSOR TO THE EXTERNAL CIRCUIT. TO CLOSE THE VALVE, HIGH PRESSURE FUEL IS SUPPLIED TO THE FITTING, AND THE FITTING IS CONNECTED WITH THE DRAIN. AT THIS TIME, THE PLATE MOVES UP TO THE END OF THE SEAT ON THE FLANGE AND CLOSURES THE PASSAGE FOR BYPASSED AIR. MANUFACTURING METHOD - CASTING. MATERIAL - STEEL. IMPORTED FOR INVESTIGATION AND REPAIR AT THE MANUFACTURING FACTORY. SECOND-HAND. IN OUT OF WORKING CONDITION. IS NOT SPECIFICALLY lock lock RUSSIAN FEDERATION RUSSIA 0
9032890000 ELECTRONIC ENGINE REGULATOR RED-90M - 1 PCS (IND. NO. 54308161239). INCLUDED lock lock RUSSIAN FEDERATION RUSSIA 1
8411128009 TURBOJET, DOUBLE-CIRCUIT, TWO-ROTOR ENGINE PS-90A-76, WITH SUPPORT lock lock RUSSIAN FEDERATION RUSSIA 1
8411128009 TURBOJET, DOUBLE-CIRCUIT, TWO-ROTOR ENGINE PS-90A-76, WITH SUPPORTED LPC STEPS, WITH FLOW MIXING AND A REVERSING DEVICE IN THE EXTERNAL CIRCUIT CHANNEL FOR THE IL-76 CIVIL AVIATION AIRCRAFT, SERIAL NO lock lock RUSSIAN FEDERATION RUSSIA 1
8536908500 SWITCHING UNIT BK-90 - 1 PCS. IND NO. 763319153, DESIGNED FOR FORMATION AND PRODUCTION OF DISCRETE ELECTRICAL SIGNALS FOR THE CONTROL OF STARTING ELECTRICAL AUTOMATICS lock lock RUSSIAN FEDERATION RUSSIA 0
8108909008 GRID SECTION RU 94-20-8160-01 - 1 PC. INSTALLED ON THE PS-90A-76 CIVIL AVIATION ENGINE. SON MET lock lock RUSSIAN FEDERATION RUSSIA 0
8481309108 94-10-994 AIR BYPASS VALVE (IN CASE 94-10-565R) IND NO. 792436-2 - 1 PCS, DESIGNED FOR BYPASSING AIR FROM THE HPC OF THE PS-90A-76 CIVIL AVIATION AIRCRAFT ENGINE. CONSISTS OF HOUSING WITH FLANGE AND COVER. INSIDE THE CASE IS A DOUBLE-ACTING HYDRAULIC CYLINDER, A PISTON, WHICH IS CONNECTED TO A PLATE. CONDITIONAL DIAMETER OF THE VALVE FLOW SECTION IS 76 MM. OPERATING PRINCIPLE: TO OPEN THE VALVE, HIGH PRESSURE FUEL IS SENT INTO THE FITTING, AND THE FITTING IS CONNECTED WITH THE DRAIN. IN THIS WAY, THE PLATE MOVES DOWN FROM THE SEAT ON THE FLANGE AND OPENS THE PASSAGE FOR BYPASSED AIR FROM THE COMPRESSOR TO THE EXTERNAL CIRCUIT. TO CLOSE THE VALVE, HIGH PRESSURE FUEL IS SUPPLIED TO THE FITTING, AND THE FITTING IS CONNECTED WITH THE DRAIN. AT THIS TIME, THE PLATE MOVES UP TO THE END OF THE SEAT ON THE FLANGE AND CLOSURES THE PASSAGE FOR BYPASSED AIR. MANUFACTURING METHOD - CASTING. MATERIAL - STEEL. IMPORTED FOR INVESTIGATION AND REPAIR AT THE MANUFACTURING FACTORY. SECOND-HAND. IN OUT OF WORKING CONDITION lock lock RUSSIAN FEDERATION RUSSIA 0
7326909807 PRODUCTS FROM FERROUS METAL: N08-087-8-13-8-TSVSP-3S SPHERE - 18 PCS, 94-03-8640 BRACKET - 18 PCS, 94-03-1085 BLOCK - 18 PCS. THEY ARE METAL PRODUCTS OF COMPLEX SHAPE WITH DIFFERENT SIZES lock lock RUSSIAN FEDERATION RUSSIA 0
8411910008 94-03-8535 INJECTOR SET FRD-94DS - 1 SET, IND. SET NO. 050702 (CONSISTS OF 12 INJECTORS INDICATOR NO. 010726, 010723. 010752, 010706, 071237, 010747, 010745, 010702, 071245, 071204 lock lock RUSSIAN FEDERATION RUSSIA 0

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Silk Way Airlines export markets

Explore the RUSSIA export market with monthly export values, major importers, HS Codes, key ports, top suppliers, and competitors

TOP EXPORT HS CODE

HS CODE USD VALUE SHIPMENTS %
8411128009 3.90 2 4.08
TURBO-JETS, TURBO-PROPELLERS AND OTHER GAS TURBINES
9032890000 0.34 5 10.20
AUTOMATIC REGULATING OR CONTROLLING INSTRUMENTS AND APPARATUS
8413302008 0.16 1 2.04
PUMPS FOR LIQUIDS, WHETHER OR NOT FITTED WITH A MEASURING DEVICE; LIQUID ELEVATORS
7326909807 0.07 4 8.16
OTHER ARTICLES OF IRON OR STEEL
8479899707 0.04 2 4.08
MACHINES AND MECHANICAL APPLIANCES HAVING INDIVIDUAL FUNCTIONS, NOT SPECIFIED OR INCLUDED ELSEWHERE IN THIS CHAPTER

TOP EXPORT COUNTRY

COUNTRY USD VALUE SHIPMENTS %
AZERBAIJAN 4.59 49 100.00

TOP EXPORT PORTS

PORTS USD VALUE SHIPMENTS %
BAKU 4.59 49 100.00

TOP EXPORT BUYERS

COMPANY USD VALUE SHIPMENTS
OMNIPOL A S 0.10 1
SILK WAY AIRLINES 7.81 49
VOLGA DNEPR AIRLINE LLC 16.00 4

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Silk Way Airlines Export Shipments

Discover the Silk Way Airlines with product description, import values, quantities, exporter name, country of origin and key destinations.

HSN Code Product Description Imports Exporter Origin Destination Qty.
8479899707 AIR STARTER STV5-40-800R. INDIVIDUAL NO. D9112057. AIR STARTER STV-5 - 1 PCS. IS AN AIR TURBINE STARTER, WITH AN AXIAL TWO-STAGE TURBINE AND A SINGLE-STAGE PLANETARY GEARBOX WITH A SAFETY FRICTION CLUTCH. THE STARTER IS INSTALLED ON THE DRIVE BOX OF THE PS-90A-76 AIRCRAFT ENGINE FOR CIVIL AVIATION. THE STARTER OPERATES ON COMPRESSED AIR SUPPLIED FROM AN EXTERNAL SOURCE. COMPRESSED AIR IS SUPPLIED FROM ONE OF THREE SOURCES: FROM THE ONBOARD AUXILIARY POWER UNIT, FROM THE AERODROME AIR STARTING UNIT, FROM THE OPERATING ENGINE. THE STARTER IS DESIGNED TO SPIN THE ROTOR OF THE ENGINE'S HIGH PRESSURE COMPRESSOR DURING COLD CROPPING, FALSE STARTING AND STARTING THE ENGINE ON THE GROUND, AND ALSO, IF NECESSARY, WHEN STARTING THE ENGINE IN FLIGHT. IT IS EXPORTED COMPLETELY ACCORDING TO THE PRODUCT DATA SHEET lock lock RUSSIA AZERBAIJAN 0
8479899707 AIR STARTER STV5-40-800R. INDIVIDUAL NO. D9112057. AIR STARTER STV-5 - 1 PCS. IS AN AIR TURBINE STARTER, WITH AN AXIAL TWO-STAGE TURBINE AND A SINGLE-STAGE PLANETARY GEARBOX WITH A SAFETY FRICTION CLUTCH. START lock lock RUSSIA AZERBAIJAN 0
8481805990 85-07-806 K/T NO. 072301 (KE72-4 NO. 220023) HYDRAULIC DISTRIBUTOR KE72-4 - 1 PIECE, INSTALLED IN THE HYDRAULIC SYSTEM FOR CONTROL OF THE REVERSING DEVICE OF ENGINE PS-90A-76 CIVIL AVIATION. DESIGNED FOR SUPPLYING WORKING FLUID TO THE HYDRAULIC SYSTEM OF THE REVERSING DEVICE CONTROL OF THE PS-90A-76 ENGINE IN REVERSE THRUST MODES AND CUT OFF THE HYDRAULIC SYSTEM OF THE REVERSING DEVICE FROM THE AIRCRAFT HYDRAULIC SYSTEM IN DIRECT THRUST MODES I. PRESSURE IN THE DISCHARGE LINE - 0-21.57 MPA, PRESSURE IN THE DRAIN LINE - 0-2.94 MPA. IT IS EXPORTED COMPLETELY ACCORDING TO THE PRODUCT DATA SHEET. IS NOT A PIPELINE FITTING WITH A NOMINAL SIZE MORE THAN 0.01 M (3/8 INCH), OR A FITTING BODY WITH A REPLACEABLE SHUT-OFF ELEMENT AND A MOLDED INSERT INTENDED FOR USE IN SUCH FITTINGS IN WHICH ALL SURFACES LOCATED IN IN CONTACT WITH CHEMICALS, MADE FROM ONE OR MORE OF THE FOLLOWING MATERIALS: NICKEL OR ALLOYS WITH MORE THAN lock lock RUSSIA AZERBAIJAN 0
8481309908 AUTOMATIC FUEL DISTRIBUTOR ART-90R - 1 PCS INDICATOR NO. 10107202002. USED IN AIRCRAFT ENGINES PS-90A-76 FOR CIVIL AVIATION, DESIGNED FOR DISTRIBUTION OF DOSED FUEL OF HIGH PRESSURE UNIT NR-90 ON COMBUSTION CHAMBER MANIFOLDS lock lock RUSSIA AZERBAIJAN 0
7326909807 PRODUCTS FROM FERROUS METAL: 94-03-893 GASKET - 60 PCS, N08-087-8-13-8-TSVSP-3S SPHERE - 60 PCS, 94-03-1085R BLOCK - 60 PCS, N08-8035-8 BUSHING WITH WITH GASKET - 10 PCS, Н08-8035-12 BUSH WITH GASKET - 10 PCS, 94-03-8640 BRACKET - 60 PCS lock lock RUSSIA AZERBAIJAN 0
7318157008 CORROSION-RESISTANT STEEL HEX BOLTS WITHOUT NUTS AND WASHERS IN DIFFERENT SIZES WITH METRIC THREAD. N08-055-6-16-SR BOLT -120 PCS. DESIGNED FOR USE IN VARIOUS COMPONENTS OF CIVIL AVIATION AIRCRAFT PS-90A ENGINE lock lock RUSSIA AZERBAIJAN 0
7318240008 UNTHREADED CLIPS IN DIFFERENT SIZES. 2X16.2.11 GOST 397-79 SPIN - 60 PCS. DESIGNED FOR USE IN VARIOUS COMPONENTS OF CIVIL AVIATION AIRCRAFT PS-90A-76 ENGINE. MATERIAL OF MANUFACTURE - CORROSION-RESISTANT STEEL lock lock RUSSIA AZERBAIJAN 0
7318210009 SPRING AND LOCKING WASHERS, PRODUCTS WITHOUT THREAD IN DIFFERENT SIZES. N08-440-01-6 LOCK WASHER - 60 PCS, N08-265-6-26 DOUBLE LOCK WASHER - 60 PCS. DESIGNED FOR USE IN VARIOUS CIVIL AIRCRAFT ENGINE COMPONENTS lock lock RUSSIA AZERBAIJAN 0
8481101908 THERMAL VALVE GA133-100-6K, NO. 0130140 - 1 PCS. DESIGNED TO PROTECT THE HYDRAULIC SYSTEM OF CIVIL AVIATION ENGINE PS-90A-76 FROM UNACCEPTABLE PRESSURE INCREASE (OVER 260+15 KGS/CM2) DUE TO THERMAL EXPANSION OF WORKING FLUID P lock lock RUSSIA AZERBAIJAN 0
8481805990 85-07-810 SHUTTER VALVE UG97-7- 2 PCS, INDIVIDUAL NO. 0631158, 0631159, INSTALLED ON CIVIL AVIATION AIRCRAFT ENGINE PS-90A-76. DESIGNED FOR BYPASSING WORKING FLUID FROM THE ROD CAVITY OF HYDRAULIC CYLINDERS TO THE PISTON CHAMBER, FOR COMPUTER lock lock RUSSIA AZERBAIJAN 0
9032890000 ELECTRONIC ENGINE REGULATOR RED-90M - 1 PCS (IND. NO. 54312361577). IT IS PART OF THE ELECTRONIC PART OF THE PS-90A-76 ENGINE CONTROL SYSTEM FOR CIVIL AVIATION. DESIGNED FOR DEVELOPING CONTROL INFLUENCES ON ACTUATORS, CONTROL MECHANISMS lock lock RUSSIA AZERBAIJAN 1
3926909200 OTHER PLASTIC PRODUCTS MADE FROM SHEET MATERIAL: 620-676 GOST 23825-79 PROTECTIVE RING lock lock RUSSIA AZERBAIJAN 0
4016930005 GASKETS AND OTHER SEALINGS FROM VULCANIZED NON-POROUS RUBBER IN DIFFERENT SIZES: 017-020-19-2-061 OST1 lock lock RUSSIA AZERBAIJAN 0
7318210009 SPRING AND LOCKING WASHERS, PRODUCTS WITHOUT THREAD IN DIFFERENT SIZES. N08-440-01-8 LOCK WASHER - 36 PCS, N08-265-8-42.4 WASHER lock lock RUSSIA AZERBAIJAN 0
7318210009 SPRING AND LOCKING WASHERS, PRODUCTS WITHOUT THREAD IN DIFFERENT SIZES. N08-036 lock lock RUSSIA AZERBAIJAN 0
7326909807 PRODUCTS FROM FERROUS METAL: 94-13-9407 FUEL SUPPLY PIPELINE TO THE UNIT DTSN-94 - 1 PCS, Н08-8035-8 BUSH WITH GASKET - 10 PCS lock lock RUSSIA AZERBAIJAN 0
8481808199 94-07-829-01Р NO. 4200720250462-76 REVERSE CONTROL VALVE KR-85 - 1 PCS, INSTALLED IN THE HYDRAULIC SYSTEM FOR CONTROL OF THE REVERSE DEVICE OF THE CIVIL AVIATION ENGINE PS-90A-76. DESIGNED FOR MECHANICAL CONTROL OF THE SUPPLY OF WORKING FLUID TO THE HYDRAULIC CYLINDERS OF THE REVERSING DEVICE FOR SHIFTING THE REVERSING DEVICE TO THE DIRECT AND REVERSE DRAW POSITION. IT IS A SWITCH TYPE WORKING FLUID DISTRIBUTOR WITH A BALL VALVE AND A LEVER CONTROL MECHANISM MOUNTED IN ONE CASE. THE SUPPLY OF WORKING FLUID TO THE HYDRAULIC SYSTEM IS CONTROLLED BY THE CRANE CONTROL LEVER. WORKING PRESSURE, MPA, (KGS/CM2) - 8.0...22.0 (80...220), MAXIMUM ALLOWABLE PRESSURE, MPA, (KGS/CM2) - 28.0 (280). IT IS EXPORTED COMPLETELY ACCORDING TO THE PRODUCT DATA SHEET. IT IS NOT A PIPELINE FITTING WITH A NOMINAL ORIGINAL DIAMETER MORE THAN 0.01 M (3/8 INCH), OR A FITTING BODY WITH A REPLACEABLE (REPLACEABLE) SHUTOFF ELEMENT lock lock RUSSIA AZERBAIJAN 0
8481809907 85-07-806R K/T NO. 705336 (KE72-4 NO. 140010), K/T NO. 706140 (KE72-4 NO. 150006) HYDRAULIC DISTRIBUTOR KE72-4 - 2 PIECES. INSTALLED IN THE HYDRAULIC SYSTEM OF THE CONTROL SYSTEM OF THE REVERSING DEVICE OF THE PS-90A-76 CIVIL AVIATION ENGINE, DESIGNED TO SUPPLY WORKING FLUID TO THE HYDRAULIC SYSTEM OF THE CONTROL SYSTEM OF THE REVERSING DEVICE OF THE PS-90A-76 ENGINE IN REVERSE MODES THRUST AND CUTS OF THE HYDRAULIC SYSTEM OF THE REVERSING DEVICE FROM THE AIRCRAFT HYDRAULIC SYSTEM IN DIRECT THRUST MODES. PRESSURE IN THE DISCHARGE LINE - 0-21.57 MPA, PRESSURE IN THE DRAIN LINE - 0-2.94 MPA. IT IS EXPORTED COMPLETELY ACCORDING TO THE PRODUCT DATA SHEET. IS NOT A PIPELINE FITTING WITH A NOMINAL SIZE MORE THAN 0.01 M (3/8 INCH), OR A FITTING BODY WITH A REPLACEABLE SHUT-OFF ELEMENT AND A MOLDED INSERT INTENDED FOR USE IN SUCH FITTINGS IN WHICH ALL SURFACES LOCATED IN IN CONTACT WITH CHEMICALS, MADE FROM ONE OR MORE OF THE FOLLOWING MATERIALS lock lock RUSSIA AZERBAIJAN 0
8544300007 OTHER WIRE SETS FOR SPARK PLUGS USED FOR CIVIL AVIATION: 94-09-8093 NO. 062306 WIRING HARNESS - 1 PCS, INCLUDED IN THE IGNITION SYSTEM OF AIRCRAFT ENGINE PS-90A-76 CIVIL AVIATION. LOW-VOLTAGE, CAPACITIVE IGNITION SYSTEM IS DESIGNED FOR IGNITION OF THE FUEL-AIR MIXTURE IN THE COMBUSTION CHAMBER WHEN STARTING THE ENGINE ON THE GROUND AND IN FLIGHT CONDITIONS. DESIGNED TO TRANSFER ENERGY FROM THE IGNITION UNIT PVF-22-20 TO THE SPARK PLUGS. SUPPLY VOLTAGE - CONSTANT, 27+1V. NOT HAZARDOUS WASTE. IS NOT A CONDUCTOR FROM SUPERCONDUCTING COMPOSITE MATERIALS, CONTAINING ONE OR MORE NIOBIUM TITANIUM FILAMENTS, HAVING ALL OF THE FOLLOWING: A) PLACED IN A MATRIX NOT FROM COPPER OR NOT BASED ON COPPER; AND B) HAVING A CROSS SECTIONAL AREA OF LESS THAN 0.28 X 10-4 MM2 (6 µM IN DIAMETER FOR ROUND SECTION THREADS); A CONDUCTOR FROM SUPERCONDUCTING COMPOSITE MATERIALS, CONTAINING ONE OR MORE SUPERCONDUCTING FILAMENTS lock lock RUSSIA AZERBAIJAN 0
9013800000 INTEK PRO SMD46-200 VIDEO ENDOSCOPIC SYSTEM (D = 6 MM, L = 2000 MM) - 1 PCS. IT IS A VIDEO ENDOSCOPE WITH A PROBE WITH AN OUTER DIAMETER OF 6 MM, A LENGTH OF 2 M WITH A NON-REPLACEABLE OPTICAL ADAPTER BASED ON THE VISI-PRO 7 VIDEO RECORDER. DESIGNED FOR HV lock lock RUSSIA AZERBAIJAN 1

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Silk Way Airlines frequently asked questions

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