The CAMO should establish a process to verify that the maintenance organisation complies with the applicable requirements of Subpart E. Essentially this means that the aircraft may be maintained by an organisation which is not compliant with the requirements of EASA Part 145.

(1) Components which are in a satisfactory condition, released on an EASA Form 1 or equivalent and marked in accordance with Subpart Q of Annex I (Part 21) to Regulation (EU) No 748/2012, unless otherwise specified in Annex I (Part 21) to Regulation (EU) No 748/2012 or in this Annex (Part-M).

PPL. Om man har ett Quickie Q-2. fartsmyndigheten i Sverige har kompletterat EASA:s regelverk. (subpart Q) så att de särskiljer sig i Sverige jämfört med andra länder i Europa. Små bolag har  Regulation (EU) No 1321/2014, Annex I, Part M, Section A, Subpart F, point vissa icke-säkerhetskritiska delar för installation utan en EASA-blankett 1. INBS on the ELA they receive (measures (p) and (q) referred to in recital 68) and to the  Material (GM) som r utfrdade av EASA r infrlivade genom hnvisning (t.ex.

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consistently deliver safe and cost effective products, parts or appliances is a . challenge for all organisations. This course provides in detail a full regulatory understanding of obligations related to EASA / GCAA in detail the requirements of (Part 21), Subpart G (Production Organisation Approval) and Subpart F(Production without Production Organisation Approval), Consideration is also provided related to the Acceptable Means of Compliance (AMC) and Guidance Material (GM). The information below is for approval holders and gives details of regulation, policy and guidance from the CAA and EASA. Guidance material provides interpretation or greater detail about aspects of regulation or policy so that approval holders can fully implement quality systems which remain compliant and perform well. Regulation (EU) No. 1321/2014 determines the rules for the continuing airworthiness and maintenance of aircraft subject to EASA regulation. Part M Subpart G of this regulation concerns the management of continuing airworthiness of EASA aircraft..

Part 21, Subpart D – Changes on Type Certificates and restricted Type Certificates. Part 21, Subpart Q – Identification of Products, Parts & Appliances. Part 21, Subpart P – Permit to Fly Procedures (incl.

EASA PART 21 SUBPART G PRODUCTION ORGANISATION CAPABILITY LIST General Quality Document GQD-1003 – Revision 48 EASA Part 21 Subpart G Approval Certificate No. CH.21G.0008 Meggitt SA Tel: +41 26 407 1111 Physical Location: Route de Moncor 4, CH-1752 Villars-sur-Glâne, Switzerland

Familiarisation with the EU Regulation s containing Part 21 and how to manage amendments. (1) Components which are in a satisfactory condition, released on an EASA Form 1 or equivalent and marked in accordance with Subpart Q of Annex I (Part 21) to Regulation (EU) No 748/2012, unless otherwise specified in Annex I (Part 21) to Regulation (EU) No 748/2012 or in this Annex (Part-M). - EASA Part-M Subpart E on Components - EASA Form 1 (Appendix II to EASA Part-M) - Class and Rating System (Appendix IV to EASA Part-M) - Acceptable Means of Compliance to EASA Part-M/D&E - Guidance Material to EASA Part-M/D&E - EASA Part-21 Subpart Q on Identification - Guidance Material to EASA Part-21/Q - Selected EASA Decisions (AD's, PMA Subpart E of Section B is replaced by the following: ‘In this Subpart, references to type-certificates include type-certificates and restricted type-certificates. 21.B.109 Type-certification basis, environmental protection requirements and operational suitability data certification basis for a supplemental type-certificate EASA Part M Subpart C, G & I Initial– 3 Days Introduction The primary purpose of this training is to provide a thorough understanding of the Role of Part M in all jurisdictions managed by an EASA Regulatory environment.

Regulation (EU) No. 1321/2014 determines the rules for the continuing airworthiness and maintenance of aircraft subject to EASA regulation. Part M Subpart G of this regulation concerns the management of continuing airworthiness of EASA aircraft.. Organisations approved to Part M Subpart G can additionally be approved to make recommendations to a competent authority that an Airworthiness Review

CS FTL.1.100 Applicability These Certification Specifications are applicable to commercial air transport by aeroplanes for scheduled and Council Regulation (EEC) No. 3922/91, excluding Subpart Q concerning flight and duty time limitations and rest requirements. (2) In accordance with Article 22(2) of Regulation (EC) No 216/2008, implementing rules related to flight and duty times and rest requirements should initially include all Subpart Q PERMIT TO FLY •Effective from 28 march 2007 •Permit to fly used where the C of A is temporarily invalid or cannot be issued but the aircraft is capable of performing a safe flight •EASA permit to fly may be issued by competent authority on application or by a production or design organisation with appropriate privileges SUBPART A CS-ETSO A-1 SUBPART A - GENERAL 1. APPLICABILITY 1.1 Requirements for the issue of European Technical Standard Order (ETSO) Authorisations are found in Part 21 Section A Subpart O. 1.2. Marking requirements for the issue of European Technical Standard Order Authorisations are found in Part 21 Section A Subpart Q. 2.

for passengers, EU citizens & general public SUBPART Q . FLIGHT AND DUTY TIME LIMITATIONS AND REST REQUIREMENTS . OPS 1.1090 . Objective and scope . 1. An operator shall establish a flight and duty time limitations and rest scheme (FTL) for crew members. 2.
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Subpart F. • Analogous to a DOA certification, there is transfer of AIRWORTHINESS. CERTIFICATES. Subpart Q. Subpart D. SUPPLEMENTAL.

1.3.3 . The FAA and EASA mutually recognize each other’s aircraft certification systems which includes EASA recognitio n of FAA’s designee system and . Technical Implementation Procedures Combined Revision 6 including Amendment 1 4 EASA Flight Time Limitations (FTL) From 18 February 2016 Commercial Air Transport operators of aeroplanes will need to have transitioned to EASA Subpart FTL. Operators can transition before this date and most major airlines plan to transition by October 2015 for the start of the winter season.
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EASA by Country; International cooperation. Cooperation with ICAO; Regional Safety Oversight Organisations (RSOOs) Technical cooperation. Technical Cooperation Projects; Worldwide initiatives; Safety Management & Promotion. Accident and incident investigation support. Legal and regulatory framework; Safety Recommendations; EASA Virtual Academy; Aviation Safety Reporting

Organisations will need to decide whether, in this scenario, they wish to retain both a national and an EASA approval. Further details regarding the EASA application process can be found on this link. A UK Part M Subpart F will Subpart E - Components Summarise -summarise the maintenance of the components Subpart E 1 Define -define components eligible to be fitted and a document equivalent to an EASA Form 1 M.A.501 Installation Part-M, Appendix II, EASA Form 1 -No component may be fitted The European Union Aviation Safety Agency (EASA) is an agency of the European Union (EU) with responsibility for civil aviation safety.It carries out certification, regulation and standardisation and also performs investigation and monitoring.: §4.3 It collects and analyses safety data, drafts and advises on safety legislation and co-ordinates with similar organisations in other parts of the EASA Part CAMO Implementation date - 24 March 2020. Following the implementation date In accordance with Article 4 of Regulation (EU) 1321/2014 as amended, after 24 September 2021, there should be no more Part-M Subpart F and Part-M Subpart G organisations. (Existing Part M Subpart G approvals will no longer be valid from 24 September 21). Subpart Q concerning flight and duty time limitations and rest requirements.

EASA Part M Subpart G and I approved CAMO organisation Subsidiary to Nordic MRO.

OPS 1.1090 . Objective and scope . 1. An operator shall establish a flight and duty time limitations and rest scheme (FTL) for crew members. 2. An operator shall ensure that for all its flights: 2.1. The flight and duty time limitations and rest scheme is in accordance with both: Subpart Q remains applicable until the full implementation of the new EU FTL rules in all member states (18 February 2016 at the latest).

Augmented flight crew: Subpart Q – Identification of Products, Parts & Appliances. Concerns the Marking and identification of Products, Parts & Appliances, Concerns European Part Approval (EPA) related to data not belonging to TC or ETSOA Holder. substantive provisions of Subpart Q of Annex III to Regulation (EEC) No. 3922/91, taking into account the latest scientific and technical evidence. (3) This Regulation constitutes an implementing measure referred to in Articles 8(5) and EU OPS SUB PART Q Flight and Duty Time Limitations and Rest Requirements for Flight Crew _____ SUB PART Q Flight and Duty Time Limitations and Rest Requirements for Flight Crew Feb 2002 2 4.1. A crew member shall not operate on aeroplane if he/she knows or suspects that he/she is suffering from or is likely to suffer from fatigue, Subpart Q PERMIT TO FLY •Effective from 28 march 2007 •Permit to fly used where the C of A is temporarily invalid or cannot be issued but the aircraft is capable of performing a safe flight •EASA permit to fly may be issued by competent authority on application or by a production or design organisation with appropriate privileges Flight Time Limitations Regulation (EC) No 1899/2006 (EU-OPS) established the first mandatory EU flight duty limitations and rest requirements (FTL) for aircrew under subpart Q of it's Annex III. The aim was to ensure that flight and cabin members perform safety functions on board of aircraft at a proper level of alertness.