8411228000 Hs Code: TRAE DATA ANALYSIS
Discover HS Code 8411228000 and identify key markets, dependable suppliers, and active buyers using Eximpedia’s advanced data analysis. Gain access to global trade data from over 130+ countries with a single subscription, without the hustle and bustle.
8411228000 – HS Code Overview
Eximpedia analyzes HS Code 8411228000 export and import records, including data from 0 buyers and 1 suppliers. We provide an intelligence report of HS Codes 8411228000 that covers product descriptions, customs tariffs, trade statistics and several subsections that enable shippers to provide detailed product information based solely on numerical data.
8411228000 Buyers, Suppliers & Shipments
HS code 8411228000 import markets
Gain insights into HS Code 8411228000 with data on monthly import values, major importing countries, key ports, leading competitors, and active suppliers.
TOP IMPORT HS CODE
| HS CODE | USD VALUE | SHIPMENTS | % |
|---|---|---|---|
| 8411228000 | 2.52 | 2 | 100.00 |
| TURBO-JETS, TURBO-PROPELLERS AND OTHER GAS TURBINES | |||
TOP IMPORT COUNTRY
| COUNTRY | USD VALUE | SHIPMENTS | % |
|---|---|---|---|
| UKRAINE | 2.52 | 2 | 100.00 |
TOP IMPORT PORTS
| PORT NAME | USD VALUE | SHIPMENTS | % |
|---|---|---|---|
| UA112030 | 2.52 | 2 | 100.00 |
TOP IMPORT COMPETITORS
| COMPANY | USD VALUE | SHIPMENTS |
|---|---|---|
| STATE ENTERPRISE ZAPORIZ MACHINE BUILDING DESIGN BUREAU PROGRESS NAMED AFTER ACADEMICIAN O H IVCHENKA | 2.52 | 28 |
TOP IMPORT SUPPLIERS
| COMPANY | USD VALUE | SHIPMENTS |
|---|---|---|
| ZIONMET GROUP LIMITED | 2.52 | 38 |
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8411228000 Import Market
Explore HSN Code 8411228000 with product description, import values, quantities, exporter name, country of origin and key destinations.
| HSN Code | Product Description | Imports | Exporter | Origin | Destination | Qty. |
|---|---|---|---|---|---|---|
| 8411228000 | 1. AVIATION GAS TURBINE (TURBO) ENGINES D-136 SERIES 1: #2251363101042-1 PC, #2251363101043 -1 PC. WITH A CAPACITY OF 8382 KW, WHICH WERE IN USE AND DEVELOPING THEIR RESOURCE. (MODULES FOR USE AS REPAIR FUND IN THE VIEW OF ENGINES). YEAR OF RELEASE - 1991. CIVIL PURPOSE. DEVELOPMENT FROM THE BEGINNING OF OPERATION -382 HOURS. 45 MINUTES. THE ENGINES WERE REMOVED FROM SERVICE DUE TO DEVELOPMENT OF THE LIMIT VALUE OF THE RESOURCE, WHICH IS SET BY THE REGULATORY TECHNICAL DOCUMENTATION. EXTREME FLIGHT OF THE HELICOPTER WITH ENGINES - 17.08.2008. EXTREME MAINTENANCE DURING STORAGE AT THE OB""""EKTA - 01.11.2010. EXTERNAL INSPECTION OF THE ENGINE MODULES SHOWED THE PRESENCE OF FOREIGN ORGANIC DEPOSITS, LEADS OF CORROSION AND OXIDATION ON METAL SURFACES OF NON-METALLIC PARTS THE DETAILS INCLUDE AREAS WITH CRACKED SURFACES AND LOST STRUCTURAL PROPERTIES, NUMEROUS DAMAGE TO PAINT COATINGS, CRACKS AND POTS WITH MATERIAL REAR, THERMAL DAMAGE. WILL BE USED AS A REPAIR FUND OF GAS TURBINE DRIVES AI-336-2-8 FOR CIVIL PURPOSE. NOT FOR SALE, FOR OWN USE |  |
|
UKRAINE | UKRAINE | 2 |
| 8411228000 | 1. AVIATION GAS TURBINE (TURBO) ENGINES D-136 SERIES 1: #2251362101053-1 PC, #2251362101066 -1 PC. WITH A CAPACITY OF 8382 KW, WHICH WERE IN USE AND DEVELOPING THEIR RESOURCE. (MODULES FOR USE AS REPAIR FUND IN THE VIEW OF ENGINES). YEAR OF RELEASE - 1991. CIVIL PURPOSE. DEVELOPMENT FROM THE BEGINNING OF OPERATION -229 HOURS. 22 MIN. THE ENGINES WERE REMOVED FROM SERVICE DUE TO DEVELOPMENT OF THE LIMIT VALUE OF THE RESOURCE, WHICH IS SET BY THE REGULATORY TECHNICAL DOCUMENTATION. EXTERNAL START OF THE ENGINES - 18/08/2008 EXTERNAL INSPECTION OF THE ENGINE MODULES SHOWED THE PRESENCE OF FOREIGN ORGANIC DEPOSITS, TRACE OF CORROSION AND OXIDATION ON THE METAL SURFACES OF THE PARTS, ON THE NON-METALLIC PARTS THERE ARE AREAS OF CRASH WANTED SURFACES AND LOST STRUCTURAL PROPERTIES, NUMEROUS DAMAGE TO PAINT COATINGS, VM""""YATINY AND DUMPS WITH MATERIAL REAR, THERMAL DAMAGE. WILL BE USED AS A REPAIR FUND OF GAS TURBINE DRIVES AI-336-2-8 FOR CIVIL PURPOSE. NOT FOR SALE, FOR YOUR OWN USE | |
|
UKRAINE | UKRAINE | 2 |
| 8411228000 | 1. AVIATION GAS TURBINE (TURBO) ENGINES D-136 SERIES 1: #2251363101042-1 PC, #2251363101043 -1 PC. WITH A CAPACITY OF 8382 KW, WHICH WERE IN USE AND DEVELOPING THEIR RESOURCE. (MODULES FOR USE AS REPAIR FUND IN THE VIEW OF ENGINES). YEAR OF RELEASE - 1991. CIVIL PURPOSE. DEVELOPMENT FROM THE BEGINNING OF OPERATION -382 HOURS. 45 MINUTES. THE ENGINES WERE REMOVED FROM SERVICE DUE TO DEVELOPMENT OF THE LIMIT VALUE OF THE RESOURCE, WHICH IS SET BY THE REGULATORY TECHNICAL DOCUMENTATION. EXTREME FLIGHT OF THE HELICOPTER WITH ENGINES - 17.08.2008. EXTREME MAINTENANCE DURING STORAGE AT THE OB""""EKTA - 01.11.2010. EXTERNAL INSPECTION OF THE ENGINE MODULES SHOWED THE PRESENCE OF FOREIGN ORGANIC DEPOSITS, LEADS OF CORROSION AND OXIDATION ON METAL SURFACES OF NON-METALLIC PARTS THE DETAILS INCLUDE AREAS WITH CRACKED SURFACES AND LOST STRUCTURAL PROPERTIES, NUMEROUS DAMAGE TO PAINT COATINGS, CRACKS AND POTS WITH MATERIAL REAR, THERMAL DAMAGE. WILL BE USED AS A REPAIR FUND OF GAS TURBINE DRIVES AI-336-2-8 FOR CIVIL PURPOSE. NOT FOR SALE, FOR OWN USE | |
|
UKRAINE | UKRAINE | 2 |
| 8411228000 | 1. AVIATION GAS TURBINE (TURBO) ENGINES D-136 SERIES 1: #2251362101053-1 PC, #2251362101066 -1 PC. WITH A CAPACITY OF 8382 KW, WHICH WERE IN USE AND DEVELOPING THEIR RESOURCE. (MODULES FOR USE AS REPAIR FUND IN THE VIEW OF ENGINES). YEAR OF RELEASE - 1991. CIVIL PURPOSE. DEVELOPMENT FROM THE BEGINNING OF OPERATION -229 HOURS. 22 MIN. THE ENGINES WERE REMOVED FROM SERVICE DUE TO DEVELOPMENT OF THE LIMIT VALUE OF THE RESOURCE, WHICH IS SET BY THE REGULATORY TECHNICAL DOCUMENTATION. EXTERNAL START OF THE ENGINES - 18/08/2008 EXTERNAL INSPECTION OF THE ENGINE MODULES SHOWED THE PRESENCE OF FOREIGN ORGANIC DEPOSITS, TRACE OF CORROSION AND OXIDATION ON THE METAL SURFACES OF THE PARTS, ON THE NON-METALLIC PARTS THERE ARE AREAS OF CRASH WANTED SURFACES AND LOST STRUCTURAL PROPERTIES, NUMEROUS DAMAGE TO PAINT COATINGS, VM""""YATINY AND DUMPS WITH MATERIAL REAR, THERMAL DAMAGE. WILL BE USED AS A REPAIR FUND OF GAS TURBINE DRIVES AI-336-2-8 FOR CIVIL PURPOSE. NOT FOR SALE, FOR YOUR OWN USE | |
|
UKRAINE | UKRAINE | 2 |
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