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Commission Regulation (EC) No 1702/2003 of 24 September 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and appliances, as well as for the certification of design and production organisations (Text with EEA relevance) (repealed)
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Version Superseded: 10/09/2012
Point in time view as at 28/12/2009. This version of this provision has been superseded.
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1.An organisation responsible for the design of products, parts and appliances or for changes or repairs thereto shall demonstrate its capability in accordance with Part 21.
2.By way of derogation from paragraph 1, an organisation whose principal place of business is in a non-member State may demonstrate its capability by holding a certificate issued by that State for the product, part and appliance for which it applies, provided:
(a)that State is the State of design; and
(b)the Agency has determined that the system of that State includes the same independent level of checking of compliance as provided by this Regulation, either through an equivalent system of approvals of organisations or through direct involvement of the competent authority of that State.
3.Design organisation approvals issued or recognised by a Member State in accordance with the JAA requirements and procedures and valid before 28 September 2003 shall be deemed to comply with this Regulation. In such case, the period for closure of level two findings, referred to in Subpart J of Part 21, shall not exceed one year when those findings are associated with differences with previous applicable JAR.
4.A type-certificate holder who does not hold on 28 September 2003 an appropriate design organisation approval issued under applicable JAA procedures shall demonstrate its capability under the conditions laid down in 21A.14 of Part 21 before 28 September 2005.
5.An organisation, being the applicant for a supplemental type-certificate, a major repair design approval or an Auxiliary Power Unit design approval which does not hold on 28 September 2003 an appropriate design organisation approval issued by a Member State under applicable JAA procedures shall demonstrate its capability before 28 September 2005 in accordance with Part 21, [F121A.112A], 21A.432B, or in the case of an Auxiliary Power Unit, 21A.602B.
6.With regard to organisations for which a design organisation approval is proceeding through a Member State on 28 September 2003 under applicable JAA procedures:
21A.234 of Part 21 shall not apply;
compliance findings made under JAA procedures shall be deemed to have been made by the Agency for the purpose of complying with 21A.245 of Part 21.
Textual Amendments
F1 Substituted by Commission Regulation (EC) No 1194/2009 of 30 November 2009 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 certification of design and production organisations (Text with EEA relevance).
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