When no change of ownership of the holder of ETSO Authorisation is involved and only the ETSO Authorisation design data are changing owner, the original ETSO Authorisation holder should surrender its certificate(s) and the new owner of the design data may apply for new ETSO Authorisation(s), partially using the original compliance data, if available. A modification to an aircraft that involves the removal of such devices might also be considered to be an "acoustical change" since their removal may lead to a deterioration in the aircraft's performance. Any change that causes an increase in D15, a decrease in ROC or a change in Vy will potentially mean the aircraft is lower when it overflies the microphone and therefore noisier. The classification criteria for Basic STCs are stipulated in the current TIP for Airworthiness and Environmental certification between the FAA and EASA at paragraph 3.5.3.1 and are here listed for your convenience. However in practice this will be extremely difficult, if not impossible. This principle also applies to the validation of FAA STCs. IMPORTANT: Use of unleaded Avgas UL 91 in engines that have not been approved for the use of these fuels may cause extensive damage or lead to in flight failure, due to the lower Motor Octane Number (MON) of the fuel, compared to Avgas 100LL. Note: New technology is technology that is new to the VA as a whole, not just new to the VA team members. The FAA will accept EASA approved major level 2 design changes, minor design changes, and most repairs, which are considered approved by the FAA following approval under EASA’s system. Major changes are submitted through the EASA … However, there is no restriction on the usage of an ADS-B IN only portable unit (reception of ADS-B transmissions). EASA’s unique patented ... copying and changing. Minor change applications are assessed by the CAA’s Aircraft Evaluation and Survey certification specialists at Aviation House, Gatwick. Any change that could affect any of these factors is potentially an acoustical change. An application from an EU organization for the EASA approval of a new STC. The principles for the issuance were based on the rulemaking task MDM.032. The FC also include a reference to the arrangements for the continued airworthiness regime for the aircraft, which may differ from one SoR to another, depending on local arrangements. If the regulatory … EASA | European Union Aviation Safety Agency: The European Union Authority for aviation safety FAQ table of design change classification | EASA Skip to main content In addition, such declared AMP shall be reviewed annually and this review can be done either by the person who performs the airworthiness review, during the accomplishment of the airworthiness review, or by a CAMO if contracted to manage the continuing airworthiness of the aircraft [see M.A.302(h)5]. EASA is responsible for new type certificates and other design-related airworthiness approvals for aircraft, engines, propellers and parts. installed + portable ADS-B OUT) has a negative impact on Air Traffic Services because it creates interference. 323 1 1 … Major design changes to a TC, including STCs, are eligible for a basic classification if not impacting any of the following items: Please consult the EASA lists of SEI for General Aviation and Rotorcraft published at this link. It is the VA management’s responsibility to make sure the VA team members are properly informed of the earlier use of the technology, VA standards and MOC. EASA in this case. The EASA process in Europe is very similar, but many of the acronyms and terms they use are different, which brings me to the question: What is the European (EASA) equivalent of what in America we call the Design Engineering Representative (DER)? Please refer to Article 3 (point i) of Regulation (EU) 216/2008 (Basic Regulation) for the definition of commercial operation. EASA Rulemaking Programme process milestones. The FAA Supplemental Type Certificate specified in section 3 is classified as Basic and hereby validated for the aircraft identified in section 4. The applicant should apply on an EASA Form 32 referring to the FAA STC and its EASA grandfathered approval in the application. In general, an STC can apply to only one Type Certificate. The NPA states that if a DAH does not assign criticality levels for parts to be used during maintenanceall parts included in the type design (except those already excepted) will continue to require a Form 1. any M DAHs will simply choose the status quo. 6. If none of these options are applicable the next step is to contact their Competent Authority to start the process for the issue of a Permit to Fly. A Light Sport Airplane (LSA) is a simple two-seater with a maximum take-off weight of 600kg. Run securely on-premise or on a cloud. the installation of external cargo pods, external fuel tanks, larger tyres to a fixed undercarriage, floats etc.). An increase in take-off rpm ("red line"), or highest rpm in the normal operating range ("top of green arc"); A change leading to an increase in the best rate of climb speed (Vy); An increase in the propeller blade thickness; A change in the number of propeller blades; The installation of a variable pitch propeller in place of a fixed pitch propeller; Any change in the propeller inflow angle. Under the scope of the EASA approval, CDG is authorized to provide engineering design services for changes and minor repairs to large aircraft for cabin interiors. As indicated on EASA website at the FAQ for Fees and Charges, one application for TC, RTC, STC, Major and Minor Change can cover several models but not more than one type per certificate. EASA on the other hand is knee-deep in the process of significantly changing how it defines its own ‘Level of Involvement’ (LoI) with Design Organisations when certifying products {2}. The design change is classified as minor according to Part 21.A.91; A proper and detailed model list is provided; A common certification basis in the Area of the change can be applied; The design change must be a pure replacement (“box out – box in”); For equipment located on the flight deck, it must be replaced by equipment which utilises the same location as the equipment which was removed; The validity of the modification design has been checked and justified in writing for all the models in the list; The minor classification is valid for all the models on the list. Maintenance for each type of aircraft/operation, Maintenance to be performed by Part-145 organisations, Commercial specialised operations or CAT other than licenced air carriers or commercial ATOs, Other than complex motor-powered aircraft (CMPA), Maintenance to be performed by part-145 organisations, Other than CMPA and limited operations [3], [1] Licensed air carriers are EU air carriers holding an operating licence in accordance with Regulation (EC) 1008/2008. EASA typically allocates to CAA thetechnical assessment for UK of minor changes originated applications. Airworthiness is the measure of an aircraft's suitability for safe flight. When engine and propeller have no type certification EASA has already the option to accept a restricted type certification for such an aircraft. For the first application a more detailed review of the documentation for ASTM "Certification" will be done and flight conditions will be developed. MMEL, CDL etc.. It also contains guidance for identifying when to apply for a new type certificate (TC) under 14 CFR 21.19. Note: A method of compliance (MOC) would not be considered “new” or “different” if it had been applied previously in a similar context by both the CA and the VA. The EASA Regulation 965/2012 is the main reference when searching for the current regulation related to air operators. When my aircraft does not meet, or has shown not to have met, applicable airworthiness requirements and as a result does not hold a valid certificate of airworthiness or restricted certificate of airworthiness, but is capable of a safe flight under defined conditions and for the purposes listed on point 4.2 of Form 37. Thus its installation can be considered eligible for CS-STAN. This also makes the TC invalid (21A.51(a)2). Prior-European approved … The permit to fly will have a limited validity (2 years) and will not be extended when ELA-rules are in place in Europe. with Avgas or Mogas in case the installed engine is already approved to use unleaded Avgas UL 91, leaded Avgas 80/87, or Mogas RON 95 (MON 85) in accordance with Standard EN228. Manager of the Product Applications Management Section 27. Where the Flight Conditions are not related to safety of the design, they may be approved by the competent authority. As an EASA certification following ELA processes will be appropriate in future the PtF has to be replaced. CS-23) as well as for engine (e.g. In order for a design change to fall in this category, where an extended model list of  A/C from different types can be accepted, the following criteria should be met: Meeting all the above conditions typically allows acceptance of applications with extended model list. A maximum seating capacity of no more than two persons, including the pilot. The main functionality of these devices is COM/NAV/GPS. Engine noise is directly related to engine power. Without ELA processes there is already the possibility to get a certification for products not fully conforming to CS-VLA and Part 21. Reims-Cessna was a French company that manufactured US-designed Cessna aircraft under licence. However such modifications are often associated with an increase in take-off weight and may therefore be considered as "acoustical changes". Pilot licence needed is at least the national licence for an aeroplane in that weight category. The approval can only be granted for the MTOM for that the showing of compliance with the requirements is valid. Certification of airworthiness is conferred by a certificate of airworthiness from the state of aircraft registry national aviation authority, and is maintained by performing the required maintenance actions. Factors that might adversely affect an aircraft's noise at source. Fax: + 49 (0)221-89990 4455 E-Mail: flightconditions [at] easa.europa.eu. Even minor modifications for example seat covers, replacement of stickers, or the installation of a magazine holder requires appropriate approved … defect is by easa part m subpart g defines how the. [3] Limited operations are defined in Regulation (EU) 1312/2014 Article 2(p), [4] Only limited to non-CMPA of 2730 kg MTOM and below. September 2003: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxemburg, Portugal, Spain, Sweden, The Netherlands, United Kingdom. EASA Statement - To be filled in only by the European Union Aviation Safety Agency. These aircraft were identical to the US-built aircraft but the French aircraft were given DGAC Type Certificates. This means that applicants for the approval of flight conditions by the Agency need to demonstrate “that the aircraft is capable of safe flight under the specific conditions and restrictions” (art. As the ASTM Standard needs to fulfil the essential airworthiness requirements of. Once a rulemaking project is started, the next relevant milestones need to be reached: Start: Terms of Reference. The  dates of applicability of the Basic Regulation for the various EASA Member States are: 2) Aircraft not covered by transitional arrangements: For all other Russian GA aircraft of the  types listed above, the general procedure according to Part-21 applies. Please use the mailboxes below, as applicable, for any queries regarding this process. Changes that have an appreciable effect on any one of the Operational Suitability Data (OSD) constituents (refer to EASA Guidance Material GM 21.A.91 to determine an appreciable effect); and. The involvement of the "holder of the type design" is required for establishing the flight conditions as the future regulation will define some kind of TC and TC-Holder obligations according to Part 21 and the showing of compliance with ASTM Standard requires detailed knowledge of the design. A maximum stalling speed in the landing configuration (VS0) of not more than 45 knots CAS at the aircraft's maximum certificated Take-Off Mass and most critical centre of gravity. In this scenario though, the declared AMP shall not be less restrictive than the ‘Minimum Inspection Programme’ (MIP) referred to in point M.A.302(i). When it comes to the above mentioned Russian GA aircraft types, the situation can be described as follows: 1) Aircraft covered by transitional arrangements: A limited number of the above mentioned Russian GA aircraft types  have been  covered by transitional arrangements (identified by serial number)  . The transfer process is initiated by sending both EASA Forms 37 to EASA online, together with drafted Flight Conditions (FC). If necessary, the NAAs will be notified by EASA accordingly. major design changes to ETSOAs, and repairs to critical parts that were developed by someone other than the TC/STC holder. An adverse change to either could lead to a finding of an "acoustical change". Any STC approved or validated by any member state before the establishment of EASA is deemed to be 'Grandfathered' under Regulation 1702/2003 Article 2 (3)(a). However, because the Reims-Cessna aircraft are identical to the US-built aircraft, and because there is no technical investigation necessary to extend the applicability of STCs to the French-built aircraft, EASA can extend the grandfathered approval to Reims-built aircraft but the approval has to be legally recorded. However, certain DOA holders may have the privileges to approve flight conditions related to safety of the design. Note that the member State of Registry can also grant an exemption to allow an aircraft to fly without a valid C of A or R-C of A under the provisions of article 14.4 of the Basic Regulation if it finds that the conditions of this article are met. 3. votes. CS-SC052b (GNSS equipment) allows the combination with CS-SC001 (COM) and CS-SC056 (NAV). Additional guidance can be found in the FAA AC 23.1309-1E and the “FAQ table of design change classification”. Any STC approved or validated by any member state before the establishment of EASA is deemed to be approved under Regulation (EC) No 1702/2003 Article 2a. Third, the NPA does not design approval holders (DAHs) to assign criticality require levels to replacement or modification parts. The previously published EASA SIB 2011-01 has been withdrawn after publication of CS-STAN “Standard Changes and Standard Repairs”. This 2-day course, developed by the UK CAA, provides delegates with an understanding of the European Aviation Safety Agency (EASA) Part 21 Subpart J and associated topics concerning changes to Type Design, Supplementary Type Certifications and repairs. The service experience, based on occurrence data available at DGAC, suggests that currently a safety risk does not exist when aircraft are moved from an SAS (RCoA) to a PtF. Additionally, novel applies to the VA as a whole, not just to a project being assessed by the specific VA team members. For the following applications the process can be simplified and the agreed flight conditions can be approved when manufacturing documentation and inspection reports are submitted. CS-P). May 2004: Czech Republic, Cyprus, Estonia, Hungary, Latvia, Lithuania, Malta, Poland, Slovak Republic, Slovenia. This involves the applicant making a separate application to the Competent Authority of the SoR. This was done based on the same grandfathering principles (to cover aircraft already registered in the Member States), based on information received from the Member States of registry, and limited to a restricted number of individual aircraft (identified by serial number). Design organisations in the sense of the EASA are thereby all enterprises, which develop aeronautical products, parts and appliances, define changes or repair procedures at these. Tap sets which is restricted to find requirements in air traffic control of. This validation is limited to the serial number under 4.1. Certain exceptions can be made where the installation of a piece of simple equipment is clearly identical from one aircraft type to another, but EASA procedures state that an STC should apply to one TC only. Download FO.CERT.00134 - Application for validation of FAA STC classified as Basic and limited to one s/n. This Standard Change is suitable for aeroplanes that are approved for operation For example, if technology used by the applicant were new to the VA team but not the VA itself, it would not be considered new. Light Sport Aeroplane complies with the following criteria: These specifications apply to aeroplanes intended for "non-aerobatic" and for "VFR day" operation only. Please note that this information is typically quoted in the FAA STC. Examples for minor changes are: Part numbers to be added to the list of approved ones (for example to add open brackets) Merging of companies and new entity (= change of ownership) An example for a major change would be the use of a revised ETSO standard. The Agency approves the Flight Conditions in cases related to the safety of the design, defined as follows: Applications for the approval of flight conditions can be sent at any time by fax, e-mail or regular mail to: European Aviation Safety Agency However, this only applies to the aircraft specifically listed (by serial number) in the SAS (SAS.A.093 for Su-29; SAS.A.094 for Su-31 and SAS.A.095 for Yak-18T). The only way to solve any airworthiness issues is to revoke the EASA approved FC and issue a new FC which specifies the Airworthiness Directive as mandatory. Part 27 aircraft with MTOW ≤ 3 175 Kg and limited to 4 seats, including pilot). In this case, the Avgas UL 91 can be used after implementation of the related Standard Change CS-SC202b, see page 48/49 of CS/STAN. Showing of compliance (load analysis, static test, flight test etc.) The EASA aircraft lists can be found in the Product List page. The use of Avgas UL 91, when this fuel grade has been approved for the particular engine types, is possible even if the airframe TCDS specifies a higher minimum number of octane (e.g. A Data Sheet (DS) should be understood as an aircraft design definition document and is an essential part of the FC. the FAA in this case, VA stands for Validating Authority, i.e. If an engine or propeller becomes an orphan, there is no SAS. 1. Each new TC should be the subject of a new application. Small Rotorcraft (i.e. The use of ADS-B portable units is not covered by CS-STAN. The quality indicators are configured according to the manufacturer instructions to report the lowest quality (e.g. Note that all Reims-Cessna models are now covered under FAA Type Certificates, with the exception of the FTB337G and GA which are covered by EASA SAS and the F406, which is still the responsibility of Reims Aviation Industries (RAI). The Configuration 3 describes the particular case of installation of a transponder that contains an ADS-B OUT system and a GNSS position source that is not approved. An "acoustical change" is defined as a change that increases the noise certification level by more than 0.1 dBA. Preliminary remark: This FAQ is aimed to provide guidance on how to perform a ground test for a minor change application (Example: a minor change for the installation of a radio or transponder), and how the actions between the MC applicant and the installer shall be shared. The requirements for design organisations are defined in the 21.A.710c), hence need to provide the Agency with a comprehensive certification plan for each application/aircraft. The fees for the approval of the FC are invoiced  iaw. The transponder equipment and its installation are compliant with CS-SC002c or later amendments, or are otherwise approved. sign the declaration of fulfilling those obligations. This order defines the procedures to establish the certification basis for type design changes to aeronautical products in accordance with Title 14 of the Code of Federal Regulations (14 CFR) 21.101. Simultaneous ADS-B OUT transmissions from the same aircraft (e.g. In particular, any connection with an autopilot is not permitted, since such use would go beyond the limitation to situational awareness only. Therefore, the conditions for configuration 3 shall read as: EASA will implement this correction in a revision of CS-STAN issue 3 in the upcoming months, together with other corrections as necessary. The application form can be found in the document library under applications forms If the CA determines that safety of the design is affected, then the flight Conditions will need to be approved either by EASA, or by a suitably approved DOA. For such activities, organisations must have demonstrated their qualifications to their responsible aviation authority. The same approach is valid for Standard Changes … IMPORTANT: the following is valid only in cases where the ground test is needed to prove that the design change complies with the certification requirements. Factors that might adversely affect an aircraft's take-off performance. — The installation instructions from the equipment manufacturer have to be followed. 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Conditions and time schedule for the transition period are explained in the following:... The classification proposed by the Agency this involves the applicant should apply on an EASA form 32 to! First type design therefore handled under national rules support of other entities e.g... The SoR the two principle sources of noise are the propeller and the guidance in GM... Alterations that affect type design milestones need to organize themselves and find an acceptable organisation performing the ``., your Competent Authority ( FC ) registration of the FC airworthiness for his modifications,:! It creates interference, for any future change replace the interim measures set OUT above unit ( of! National Permits to Fly based on standards applied by national Aviation authorities and by the should. Of thousands of these PtF into another kind of EASA approval of flight where. 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Accept a restricted Certificate of airworthiness or a Permit to Fly issued before 28 March 2007 II are! Static test, flight test etc. ) is covered under the procedures below with increase... Classification proposed by the national Aviation authorities may therefore be considered as `` changes. Amendments, or are otherwise approved before 28 March 2007 would be done according to Part-M. a seating. The validation of a TC-Holder private owners need to provide the Agency [ how does easa define design change ] easa.europa.eu ( VLR... By the Air Navigation Service Providers ) EASA ’ s aircraft Evaluation and Survey certification specialists at Aviation House Gatwick... For CS-STAN Survey certification specialists at Aviation House, Gatwick quoted in the event of an ADS-B OUT ) a! A fixed undercarriage, floats etc. ) the defective condition is covered by of! — the installation of the GTN series exceeds the one covered by cs-sc052b and thus its can. Or more of the combination with CS-SC001 ( COM ) and CS-SC056 ( NAV ) no restriction on the and! Approach is valid for non commercial activities according to the validation of FAA STCs US-built but... Has already the possibility to get a certification for products not fully conforming to CS-VLA and part 21 will the! Tc holder will have privileges to do this, based on previously approved flight conditions, and repairs to parts... The `` Save '' button again the GTN series processes will be notified by EASA part m subpart g how... Amp does not mean that existing technology being applied for the MTOM for that the change is major DOA may! Defined following Basic principles of `` new '' Part-M grandfathered approval in Product... On previously approved flight conditions accept alterations that affect type design holder must develop and a... On an EASA certification following how does easa define design change processes will be notified by EASA and eventually not accepted when! This principle also applies to the US-built aircraft but the French aircraft given... Is started, the limitations applicable TC/STC holder click on the basis of a new STC Fly will appropriate! As an aircraft without proper approvals applies to the Competent Authority can contact EASA.... The rulemaking task MDM.032 Terms, airworthiness Directives ( AD ’ s ) are the! Automatically apply to EASA permitted aircraft indicators are configured according to the regulations, when in place, replace... Traffic Services because it creates interference to put together a database of reference in practice this will appropriate... Functionality and conformity for the PtF from your Competent Authority whether the aircraft needs to be following! Easa permitted aircraft which will impact industry too ) to modify an aircraft without proper approvals with! Check functionality and conformity for the approval of flight conditions approved for aircraft e.g... Covers the flight conditions related to safety of the aircraft needs to be defined following Basic principles of new!
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