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Commission Regulation (EC) No 375/2007 of 30 March 2007 amending Regulation (EC) No 1702/2003 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations (Text with EEA relevance) (repealed)
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This is the original version (as it was originally adopted).
In paragraph 21A.139 the following subparagraph (b)(1)(xvii) is added:
Issue of permit to fly and approval of associated flight conditions.’
In paragraph 21A.163 the following subparagraph (e) is added:
Under procedures agreed with its competent authority for production, for an aircraft it has produced and when the production organisation itself is controlling under its POA the configuration of the aircraft and is attesting conformity with the design conditions approved for the flight, to issue a permit to fly in accordance with 21A.711(c) including approval of the flight conditions in accordance with 21A.710(b).’
In paragraph 21A.165 the following subparagraphs (j) and (k) are added:
Where applicable, under the privilege of 21A.163(e), determine the conditions under which a permit to fly can be issued.
Where applicable, under the privilege of 21A.163(e), establish compliance with 21A.711(b) and (d) before issuing a permit to fly (EASA Form 20b, see Appendix) to an aircraft.’
The title of Subpart H of Section A is replaced by the following:
In paragraph 21A.173 (b) (2), the words ‘specific certification specifications’ are replaced by the words ‘specific airworthiness specifications’.
In paragraph 21A.173 subparagraph (c) is deleted.
In paragraph 21A.174 subparagraph (d) is deleted.
Subparagraph (b) of paragraph 21A.179 is replaced by the following:
Where ownership of an aircraft has changed, and the aircraft has a restricted certificate of airworthiness not conforming to a restricted type-certificate, the airworthiness certificates shall be transferred together with the aircraft provided the aircraft remains on the same register, or issued only with the formal agreement of the competent authority of the Member State of registry to which it is transferred.’
In paragraph 21A.184, the words ‘specific certification specifications’ are replaced by the words ‘specific airworthiness specifications’.
Paragraph 21A.185 is deleted.
In paragraph 21A.263, subparagraph (b) is replaced by the following:
Subject to 21A.257(b), the Agency shall accept without further verification the following compliance documents submitted by the applicant for the purpose of obtaining:
the approval of flight conditions required for a permit to fly; or
a type-certificate or approval of a major change to a type design; or
a supplemental type-certificate; or
an ETSO authorisation under 21A.602B(b)(1); or
a major repair design approval.’
In paragraph 21A.263 (c), the following subparagraphs (6) and (7) are added:
To approve the conditions under which a permit to fly can be issued in accordance with 21A.710(a)(2),
except for initial flights of:
a new type of aircraft, or
an aircraft modified by a change that is or would be classified as a significant major change or significant STC, or
an aircraft whose flight and/or piloting characteristics may have been significantly modified;
except for permits to fly to be issued for the purpose of 21A.701(a)(15).
To issue a permit to fly in accordance with 21A.711(b) for an aircraft it has designed or modified, and when the design organisation itself is controlling under its DOA the configuration of the aircraft and is attesting conformity with the design conditions approved for the flight.’
In paragraph 21A.265 the following subparagraphs (f) and (g) are added:
Where applicable, under the privilege of 21A.263(c)(6), determine the conditions under which a permit to fly can be issued.
Where applicable, under the privilege of 21A.263(c)(7), establish compliance with 21A.711(b) and (d) before issuing a permit to fly (EASA Form 20b, see Appendix) to an aircraft.’
Subpart P of Section A is replaced by the following:
Permits to fly shall be issued in accordance with this Subpart to aircraft that do not meet, or have not been shown to meet, applicable airworthiness requirements but are capable of safe flight under defined conditions and for the following purposes:
development;
showing compliance with regulations or certification specifications;
design organisations or production organisations crew training;
production flight testing of new production aircraft;
flying aircraft under production between production facilities;
flying the aircraft for customer acceptance;
delivering or exporting the aircraft;
flying the aircraft for Authority acceptance;
market survey, including customer’s crew training;
exhibition and air show;
flying the aircraft to a location where maintenance or airworthiness review are to be performed, or to a place of storage;
flying an aircraft at a weight in excess of its maximum certificated takeoff weight for flight beyond the normal range over water, or over land areas where adequate landing facilities or appropriate fuel is not available;
record breaking, air racing or similar competition;
flying aircraft meeting the applicable airworthiness requirements before conformity to the environmental requirements has been found;
for non-commercial flying activity on individual non-complex aircraft or types for which a certificate of airworthiness or restricted certificate of airworthiness is not appropriate.
Any natural or legal person shall be eligible as an applicant for a permit to fly except for a permit to fly requested for the purpose of 21A.701(a)(15) where the applicant shall be the owner. A person eligible for an application for permit to fly is also eligible for application for the approval of the flight conditions.
Notwithstanding 21.1, for the purpose of this Subpart, the “Competent Authority” shall be:
the authority designated by the Member State of registry; or
for unregistered aircraft, the authority designated by the Member State which prescribed the identification marks.
the purpose(s) of the flight(s), in accordance with 21A.701;
the ways in which the aircraft does not comply with the applicable airworthiness requirements;
the flight conditions approved in accordance with 21A.710.
Flight conditions include:
the configuration(s) for which the permit to fly is requested;
any condition or restriction necessary for safe operation of the aircraft, including:
the conditions or restrictions put on itineraries or airspace, or both, required for the flight(s);
the conditions and restrictions put on the flight crew to fly the aircraft;
the restrictions regarding carriage of persons other than flight crew;
the operating limitations, specific procedures or technical conditions to be met;
the specific flight test programme (if applicable);
the specific continuing airworthiness arrangements including maintenance instructions and regime under which they will be performed;
the substantiation that the aircraft is capable of safe flight under the conditions or restrictions of subparagraph (b);
the method used for the control of the aircraft configuration, in order to remain within the established conditions.
when approval of the flight conditions is related to the safety of the design, to the Agency in a form and manner established by the Agency; or
when approval of the flight conditions is not related to the safety of the design, to the Competent Authority in a form and manner established by that authority.
the proposed flight conditions;
the documentation supporting these conditions; and
a declaration that the aircraft is capable of safe flight under the conditions or restrictions of paragraph 21A.708(b).
the Agency; or
an appropriately approved design organisation, under the privilege of 21A.263(c)(6).
upon presentation of the data required by 21A.707; and
when the conditions of 21A.708 have been approved in accordance with 21A.710; and
when the Competent Authority, through its own investigations, which may include inspections, or through procedures agreed with the applicant, is satisfied that the aircraft conforms to the design defined under 21A.708 before flight.
The manuals, placards, listings, and instrument markings and other necessary information required by applicable certification specifications shall be presented in one or more of the official language(s) of the European Community acceptable to the Competent Authority.
The holder of, or the applicant for, a permit to fly shall provide access to the aircraft concerned at the request of the Competent Authority.
compliance with the conditions and restrictions of 21A.711(d) associated to the permit to fly;
the permit to fly not being surrendered or revoked under 21B.530;
the aircraft remaining on the same register.
Renewal of the permit to fly shall be processed as a change in accordance with 21A.713.
The holder of a permit to fly shall ensure that all the conditions and restrictions associated with the permit to fly are satisfied and maintained.
Paragraph 21B.20 is replaced by the following:
Each competent authority of the Member State is responsible for the implementation of Section A, Subparts F, G, H, I and P only for applicants, or holders, whose principal place of business is in its territory.’
In paragraph 21B.25 subparagraph (a) is replaced by the following:
The Member State shall designate a competent authority with allocated responsibilities for the implementation of Section A, Subparts F, G, H, I and P with documented procedures, organisation structure and staff.’
The title of Subpart H of Section B is replaced by the following:
In paragraph 21B.325 subparagraph (a) is replaced by the following:
Paragraph 21B.330 is replaced by the following:
Subpart P of Section B is replaced by the following:
evaluation of the eligibility of the applicant;
evaluation of the eligibility of the application;
evaluation of the documentation received with the application;
inspection of the aircraft;
approval of the flight conditions in accordance with 21A.710(b).
The Competent Authority shall issue a permit to fly (EASA Form 20a, see Appendix) when it is satisfied that the applicable requirements of Section A, Subpart P are met.
the documents provided by the applicant;
documents established during the investigation, in which the activities and the final results of the elements defined in 21B.520(b) are stated; and
a copy of the permit to fly.
The list of Appendices is replaced by the following:
‘Appendix I — EASA Form 1 Authorised release Certificate
Appendix II — EASA Form 15a Airworthiness Review Certificate
Appendix III — EASA Form 20a Permit to Fly
Appendix IV — EASA Form 20b Permit to Fly (issued by approved organisations)
Appendix V — EASA Form 24 Restricted Certificate of Airworthiness
Appendix VI — EASA Form 25 Certificate of Airworthiness
Appendix VII — EASA Form 45 Noise Certificate
Appendix VIII — EASA Form 52 Aircraft Statement of Conformity
Appendix IX — EASA Form 53 Certificate of Release to Service
Appendix X — EASA Form 55 Production Organisation Approval Certificate
Appendix XI — EASA Form 65 Letter of Agreement [Production without POA]’
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