+SECTION I Airworthiness and environmental protection
---+Article 9 Essential requirements
------+Article 9 1.
------+Article 9 2.
---+Article 10 Compliance
------+Article 10 1.
------+Article 10 2.
---+Article 11 Design of products
---+Article 12 Design of parts
---+Article 13 Design of non-installed equipment
---+Article 14 Individual aircraft
------+Article 14 1.
------+Article 14 2.
---+Article 15 Organisations
------+Article 15 1.
------+Article 15 2.
------+Article 15 3.
------+Article 15 4.
------+Article 15 5.
---+Article 16 Personnel
------+Article 16 1.
------+Article 16 2.
------+Article 16 3.
---+Article 17 Implementing acts as regards airworthiness
------+Article 17 1.
------+Article 17 2.
------+Article 17 3.
---+Article 18 Derogations
------+Article 18 1.
------+Article 18 2.
---+Article 19 Delegated powers
------+Article 19 1.
------+Article 19 2.
------+Article 19 3.
------+Article 19 4.

SECTION I Airworthiness and environmental protection

SECTION I Airworthiness and environmental protection

1. Ülevaade

,
Pealkiri Regulatsioon
Article 9 Essential requirements
Article 10 Compliance
Article 11 Design of products

Article 11

Design of products

The design of a product shall be subject to certification and shall be issued with a type certificate. Changes to that design shall also be subject to certification and shall result in the issuance of a certificate of changes, including of supplemental type certificates. Repair designs shall be subject to certification and shall be issued with an approval.

An approval shall be issued in respect of the operational suitability data associated with a type design. That approval shall be included in the type certificate or the restricted type certificate referred to in point (b) of Article 18(1), as applicable.

That type certificate, that certificate of changes, that approval of repair designs and that approval of the operational suitability data shall be issued upon application when the applicant has demonstrated that the design of the product complies with the certification basis established in accordance with the delegated acts referred to in point (b)(i) and (ii) of Article 19(1), as applicable, and that the design of the product has no feature or characteristic making it environmentally incompatible or unsafe for operation.

That type certificate, that certificate of changes, that approval of repair design and that approval of the operational suitability data may also be issued without such application, by an organisation approved in accordance with Article 15 which has been granted the privilege to issue those certificates or approvals in accordance with the delegated act referred to in point (k) of Article 19(1), when that organisation has determined that the design of the product complies with the conditions established in the third subparagraph of this paragraph.

No separate type certificate shall be required for the design of engines and propellers that have been certified as part of the design of an aircraft in accordance with this Article.

Article 12 Design of parts

Article 12

Design of parts

Unless otherwise established by delegated acts referred to in Article 19, the design of parts shall be subject to certification and shall be issued with a certificate.

That certificate shall be issued upon application, when the applicant has demonstrated that the design of the part complies with the certification basis established in accordance with the delegated acts referred to in point (b)(iii) of Article 19(1).

That certificate may also be issued without such application, by an organisation approved in accordance with Article 15 which has been granted a privilege to issue those certificates in accordance with the delegated act referred to in point (k) of Article 19(1), when that organisation has determined that the design of the part complies with the certification basis established in accordance with the delegated acts referred to in point (b)(iii) of Article 19(1).

No separate certificate shall be required for the design of parts that have been certified as part of the design of a product in accordance with Article 11.

Article 13 Design of non-installed equipment

Article 13

Design of non-installed equipment

Where the delegated acts referred to in Article 19 so provide, the design of non-installed equipment shall be subject to certification and shall be issued with a certificate.

That certificate shall be issued upon application, when the applicant has demonstrated that the design of non-installed equipment complies with the certification basis established in accordance with the delegated acts referred to in point (b)(iii) of Article 19(1).

That certificate may also be issued without such application, by an organisation approved in accordance with Article 15 which has been granted a privilege to issue those certificates in accordance with the delegated act referred to in point (k) of Article 19(1), when that organisation has determined that the design of the non-installed equipment complies with the certification basis established in accordance with the delegated acts referred to in point (b)(iii) of Article 19(1).

Article 14 Individual aircraft
Article 15 Organisations
Article 16 Personnel
Article 17 Implementing acts as regards airworthiness
Article 18 Derogations
Article 19 Delegated powers

1.1 Viited

1.2 Tuvastatud nõuded

1.3 Seotud standardid

2. Tuvastatud nõuded

Nõuded
Allikas Nõue

3. Seotud standardid

Standardid
Allikas Nõue