Regulation (EC) No 216/2008 of the European Parliament and of the Council (repealed)Dangos y teitl llawn

Article 5 U.K. Airworthiness

1. Aircraft referred to in Article 4(1)(a), (b) and (c) shall comply with the essential requirements for airworthiness laid down in Annex I.

2. Compliance of aircraft referred to in Article 4(1)(b), and of products, parts and appliances mounted thereon shall be established in accordance with the following:

(a) products shall have a type-certificate. The type-certificate, and certification of changes to that type-certificate, including supplemental type-certificates, shall be issued when the applicant has shown that the product complies with a type-certification basis as specified in Article 20, established to ensure compliance with the essential requirements referred to in paragraph 1, and when it has no feature or characteristic making it unsafe for operation. The type-certificate shall cover the product, including all parts and appliances fitted thereon;

(b) parts and appliances may be issued with specific certificates when they are shown to comply with detailed airworthiness specifications established to ensure compliance with the essential requirements referred to in paragraph 1;

(c) each aircraft shall be issued with an individual certificate of airworthiness when it is shown that it conforms with the type design approved in its type-certificate and that relevant documentation, inspections and tests demonstrate that the aircraft is in condition for safe operation. This certificate of airworthiness shall remain valid as long as it is not suspended, revoked or terminated and as long as the aircraft is maintained in accordance with the essential requirements related to continuing airworthiness set out in point 1.d of Annex I and the measures referred to in paragraph 5;

(d) organisations responsible for the maintenance of products, parts and appliances shall demonstrate their capability and means to discharge the responsibilities associated with their privileges. Unless otherwise accepted these capabilities and means shall be recognised through the issuance of an organisation approval. The privileges granted to the approved organisation and the scope of the approval shall be specified in the terms of approval;

(e) organisations responsible for the design and manufacture of products, parts and appliances shall demonstrate their capability and means to discharge the responsibilities associated with their privileges. Unless otherwise accepted these capabilities and means shall be recognised through the issuance of an organisation approval. The privileges granted to the approved organisation and the scope of the approval shall be specified in the terms of approval;

in addition:

(f) personnel responsible for the release of a product, part or appliance after maintenance may be required to hold an appropriate certificate (personnel certificate);

(g) the capability of maintenance training organisations to discharge the responsibilities associated with their privileges in relation to the issuance of the certificates referred to in point (f) may be recognised by the issuance of an approval.

3. Aircraft referred to in Article 4(1)(a) and products, parts and appliances mounted thereon shall comply with paragraph 2(a), (b) and (e) of this Article.

4. By way of derogation from paragraphs 1 and 2:

(a) a permit to fly may be issued when it is shown that the aircraft is capable of performing safely a basic flight. It shall be issued with appropriate limitations, in particular to protect third parties' safety;

(b) a restricted certificate of airworthiness may be issued to aircraft for which a type certificate has not been issued according to paragraph 2(a). In this case, the aircraft shall be shown to comply with specific airworthiness specifications and deviations from the essential requirements referred to in paragraph 1 shall nevertheless ensure adequate safety with regard to the purpose. Aircraft eligible for these restricted certificates, and limitations for use of these aircraft, shall be defined according to the measures referred to in paragraph 5;

(c) when the number of aircraft of the same type eligible for a restricted certificate of airworthiness so justifies, a restricted type certificate may be issued and an appropriate type certification basis shall be established.

5. The measures designed to amend non-essential elements of this Article, by supplementing it, shall be adopted in accordance with the regulatory procedure with scrutiny referred to in Article 65(4). Those measures shall specify in particular:

(a) conditions for establishing and notifying to an applicant the type-certification basis applicable to a product;

(b) conditions for establishing and notifying to an applicant the detailed airworthiness specifications applicable to parts and appliances;

(c) conditions for establishing and notifying to an applicant the specific airworthiness specifications applicable to aircraft eligible for a restricted certificate of airworthiness;

(d) conditions for issuing and disseminating mandatory information in order to ensure the continuing airworthiness of products;

(e) conditions for issuing, maintaining, amending, suspending or revoking type-certificates, restricted type-certificates, approval of changes to type-certificates, individual certificates of airworthiness, restricted certificates of airworthiness, permits to fly and certificates for products, parts or appliances, including:

(i)

conditions on the duration of these certificates, and conditions to renew certificates when a limited duration is fixed;

(ii)

restrictions applicable to the issue of permits to fly. These restrictions should in particular concern the following:

• purpose of the flight,

• airspace used for the flight,

• qualification of flight crew,

• carriage of persons other than flight crew;

(iii)

aircraft eligible for restricted certificates of airworthiness, and associated restrictions;

(iv)

the minimum syllabus of maintenance certifying staff type rating training to ensure compliance with paragraph (2)(f);

(v)

the minimum syllabus of pilot type rating and the qualification of associated simulators to ensure compliance with Article 7;

(vi)

the master minimum equipment list as appropriate and additional airworthiness specifications for a given type of operation to ensure compliance with Article 8;

(f) conditions to issue, maintain, amend, suspend or revoke organisation approvals required in accordance with paragraph 2(d), (e) and (g) and conditions under which such approvals need not be requested;

(g) conditions to issue, maintain, amend, suspend or revoke personnel certificates required in accordance with paragraph 2(f);

(h) responsibilities of the holders of certificates;

(i) how aircraft referred to in paragraph 1 which are not covered by paragraphs 2 or 4 are to show compliance with the essential requirements;

(j) how aircraft referred to in Article 4(1)(c) are to show compliance with the essential requirements.

6. When adopting the measures referred to in paragraph 5, the Commission shall take specific care that they:

(a) reflect the state of the art and the best practices in the field of airworthiness;

(b) take into account worldwide aircraft experience in service, and scientific and technical progress;

(c) allow for immediate reaction to established causes of accidents and serious incidents;

(d) do not impose on aircraft referred to in Article 4(1)(c) requirements which would be incompatible with the International Civil Aviation Organization (ICAO) obligations of Member States.