Document from CIS Legislation database © 2003-2024 SojuzPravoInform LLC

The document ceased to be valid since  January 17, 2018 according to Item 2 of the Order of the Minister of investments and development of the Republic of Kazakhstan of July 19, 2017 No. 483

I.O.'S ORDER OF THE MINISTER OF INVESTMENTS AND DEVELOPMENT OF THE REPUBLIC OF KAZAKHSTAN

of February 24, 2015 No. 193

About approval of Rules of certification and certification of compliance of copy of the civil aircraft to airworthiness standards

According to subitem 41-21) of Item 1 of article 14 of the Law of the Republic of Kazakhstan of July 15, 2010 "About use of airspace of the Republic of Kazakhstan and activities of aircraft" PRIKAZYVAYU:

1. Approve the enclosed Rules of certification and certification of compliance of copy of the civil aircraft to airworthiness standards.

2. To committee of civil aviation of the Ministry for Investments and Development of the Republic of Kazakhstan (Seydakhmetov B. K.) provide:

1) in the procedure established by the legislation state registration of this order in the Ministry of Justice of the Republic of Kazakhstan;

2) within ten calendar days after state registration of this order in the Ministry of Justice of the Republic of Kazakhstan the direction it the copy on official publication in periodic printing editions and information system of law of Ad_let of the republican state company on the right of economic maintaining "The republican center of legal information of the Ministry of Justice of the Republic of Kazakhstan";

3) placement of this order on Internet resource of the Ministry for Investments and Development of the Republic of Kazakhstan and on the intranet portal of state bodies;

4) within ten working days after state registration of this order in the Ministry of Justice of the Republic of Kazakhstan submission to Legal department of the Ministry for Investments and Development of the Republic of Kazakhstan of data on execution of the actions provided by subitems 1), 2) and 3) of Item 2 of this order.

3. I reserve control of execution of this order.

4. This order becomes effective after twenty one calendar days after day of its first official publication.

Acting Minister

Zh. Kasymbek

It is approved

Minister of national economy of the Republic of Kazakhstan

June 18, 2015

 

E.Dosayev

Approved by the Order of the Acting Minister of investments and development of the Republic of Kazakhstan of February 24, 2015 No. 193

Rules of certification and certification of compliance of copy of the civil aircraft to airworthiness standards

1. General provisions

1. These rules of certification and certification of compliance of copy of the civil aircraft to airworthiness standards (further - Rules) are developed according to subitem 41-21) of article 14 of the Law of the Republic of Kazakhstan of July 15, 2010 "About use of airspace of the Republic of Kazakhstan and activities of aircraft".

2. These rules determine procedure for certification and certification of compliance of copy of the civil aircraft to airworthiness standards (further - the certificate of compliance).

3. In these rules the following terms and determinations are used:

1) authorized body in the sphere of civil aviation (further - authorized body) - the central executive body performing management in the field of use of airspace of the Republic of Kazakhstan and activities of civil and experimental aviation;

2) operational documentation of EGVS - the set of documents regulating flight and technical operation of EGVS, including its maintenance and repair of specific EGVS and its components, and also containing operating conditions and operational restrictions;

3) the certificate of compliance of EGVS NLG - the document issued by authorized body in the sphere of civil aviation, certifying compliance of design of EGVS, characteristics and operational technical documentation to airworthiness standards;

4) developer the physical person or legal entity performing development of the aircraft equipment;

5) modification of VS - any change of the accepted design of VS and (or) its components which significantly influences their flight validity or affects their characteristics influencing the environment;

6) the aircraft (further - VS) - the device supported in the atmosphere due to its interaction with air excepting interaction with the air reflected from land (water) surface;

7) manufacturer - the physical person or legal entity performing production of VS;

8) evidential documentation - documentation containing results of checks, testing, researches and estimates of technical condition of the aircraft equipment;

9) the applicant - the physical person or legal entity which addressed with the request to authorized body in the sphere of civil aviation for certification of copy of the civil aircraft (further - EGVS);

10) the operator - the physical person or legal entity which is engaged in operation of civil aircrafts or offering the services in this area;

11) the expert organization - the non-profit organization uniting operators of aircrafts;

12) technical commission of experts - permanent working body of the expert organization authorized for implementation of expert evaluation of design, flight characteristics of the aircraft and determination of its technical condition and the validity to flights;

13) airworthiness standards (further - NLG) - requirements to design, parameters and flight qualities of the aircrafts and their components aimed at safety of flights;

14) the certificate of type - the document confirming compliance with airworthiness standards of design like civil VS.

4. Each copy of the civil aircraft which does not have the approved standard design shall be certified and have the certificate of compliance of its design, characteristics issued by authorized body in the sphere of civil aviation and operational technical documentation to airworthiness standards.

VS on which the certificate of compliance is issued is not allowed to implementation of commercial air transportations.

5. The procedures and general technical requirements containing in these rules are applied to EGVS of easy and extralight aircraft (planes, helicopters, gliders with the motor, autogyros, aero static aircrafts) with the maximum take-off weight no more than 2250 kg.

6. In case of modification of EGVS it is subject to repeated certification.

2. Procedure for certification of EGVS

7. The applicant submits the certification application to authorized body to EGVS in form according to appendix 1 to these rules.

Are applied to the request:

1) set of operational documentation of copy of VS;

Warning!!!

This is not a full text of document! Document shown in Demo mode!

If you have active License, please Login, or get License for Full Access.

With Full access you can get: full text of document, original text of document in Russian, attachments (if exist) and see History and Statistics of your work.

Get License for Full Access Now

Disclaimer! This text was translated by AI translator and is not a valid juridical document. No warranty. No claim. More info

Effectively work with search system

Database include more 50000 documents. You can find needed documents using search system. For effective work you can mix any on documents parameters: country, documents type, date range, teams or tags.
More about search system

Get help

If you cannot find the required document, or you do not know where to begin, go to Help section.

In this section, we’ve tried to describe in detail the features and capabilities of the system, as well as the most effective techniques for working with the database.

You also may open the section Frequently asked questions. This section provides answers to questions set by users.

Search engine created by SoyuzPravoInform LLC.