In accordance with M.A.302 and in particular M.A.302(h)(3), the AMP, declared or approved, shall in all cases include all the mandatory maintenance/continuing airworthiness requirements, such as repetitive Airworthiness Directives or the Airworthiness Limitation Section (ALS). The previously published EASA SIB 2011-01 has been withdrawn after publication of CS-STAN “Standard Changes and Standard Repairs”. This only applies for aircraft (including rotorcraft and lighter-than-air) but not to propulsion. STCs approved on US-built Cessnas and their applicability to Reims-Cessna models. However, it does not mean that existing technology being applied for the first time to a particular product line is automatically novel. 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. 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. need to reduce number and increase efficiencies)}Imminent changes in the Basic Regulation (which will impact industry too). A light propeller driven aircraft's certificated noise level is dependant on two factors, the aircraft's noise at source and the aircraft's take-off performance as defined the AFM. The ToRs, which shall be published on the Agency’s website, shall … An application from a non-EU organization for the EASA validation of a non-EU STC. CA stands for Certificating Authority, i.e. Regarding the applicability of the change, each application need to include a reference to the TC and the eligible A/C type/model to be changed. 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. Where the Flight Conditions are not related to safety of the design, they may be approved by the competent authority. Please refer to Article 2 (point k) of Regulation (EU) 1321/2014 for the definition of ELA1. An application from an EU organization for the EASA approval of a new STC. September 2003: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxemburg, Portugal, Spain, Sweden, The Netherlands, United Kingdom. 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. Only individual aircraft that were registered in one of the Member states before the date of applicability of the Basic regulation to that State were covered by the transitional arrangements described above. This means that the conditions that make the classification minor are valid for all the models (and categories) and no limitation is invalidated (example: installation of transponder on A/C with cruise TAS greater than 250 kts, is major); The mass of the new equipment is not significantly higher; Cables and Antennas have not changed (change of the mating electrical connector on the aircraft is accepted); The equipment does not add any new functionality. May 2004: Czech Republic, Cyprus, Estonia, Hungary, Latvia, Lithuania, Malta, Poland, Slovak Republic, Slovenia. In this respect, the owner may decide to deviate from the applicable scheduled maintenance recommendations (see also remark below) without the need to justify such deviation(s), but under his/her full responsibility. transponder) represent one of such exceptions. However, there is no restriction on the usage of an ADS-B IN only portable unit (reception of ADS-B transmissions). 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. 21.A.710c), hence need to provide the Agency with a comprehensive certification plan for each application/aircraft. MMEL, CDL etc.. Tap sets which is restricted to find requirements in air traffic control of. 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. The principles for the issuance were based on the rulemaking task MDM.032. In many cases the ground tests are “post-installation tests” to check functionality and conformity for the release of the installation. The process for applying for the PtF from your Competent Authority is detailed on their website or in their publications. Any other design change designated as Non-Basic by the CA. The GNSS receiver is not approved or its installation is not certified. June 2005: Iceland, Norway, Liechtenstein. 323 1 1 … 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. EASA does not automatically accept alterations that affect type design. 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 FAA in this case, VA stands for Validating Authority, i.e. Follow asked Mar 23 '16 at 14:42. Master Drawing List, Installation Instructions, Aircraft Flight Manual (AFM), Master Minimum Equipment List (MMEL), Instructions for Continued Airworthiness (ICA) including the published safety documents as Service Bulletins, Safety Information Letters, Airworthiness Directives, etc.). As an EASA certification following ELA processes will be appropriate in future the PtF has to be replaced. As there are still some open issues left e.g. 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. The rules for the classification are identified in paragraph 21.A.91 and the guidance in the GM 21.A.91. Even minor modifications for example seat covers, replacement of stickers, or the installation of a magazine holder requires appropriate approved … the legal person holding the Type Certificate (TC) has ceased to exist. In accordance with Part21A.711, the competent authority of the member state of registry is normally responsible for the issue of a Permit to Fly. 2.1 Base Maintenance & Line Maintenance The Isle of Man Aircraft Registry identifies a generic “Class Validation” status to enable all approved A maintenance regime has to be defined following basic principles of "new" Part-M. During this transition period all the LSA aircraft flying under PtF will need to obtain a normal or restricted Certificate of Airworthiness, after inspection and, if necessary, modification. The EASA aircraft lists can be found in the Product List page. This covers all previous approvals from minor changes to major changes, STCs and complete aircraft, both certifications and validations with the exception of products of the former Soviet Union. Substantiation by test does not automatically mean that the change is major. An "acoustical change" is defined as a change that increases the noise certification level by more than 0.1 dBA. In such cases the instructions below are not needed since the test would be done based on already approved data. Where there is a need, Generic Flight Conditions (GFC), if not yet existing, will be developed by EASA in cooperation with the National Aviation Authority (NAA) of the State of Design and added to the SAS. the installation of external cargo pods, external fuel tanks, larger tyres to a fixed undercarriage, floats etc.). A Data Sheet (DS) should be understood as an aircraft design definition document and is an essential part of the FC. Fax: + 49 (0)221-89990 4455 EASA Design Organisation Approval (DOA) is based on the principle of delegation whereby the various organisations are issued with an approval that allows them certain privileges Organisation approval – The Authority employs a number of experts to audit the organisations (manufacturers, operators, maintenance centres, training centres) and to sample by audit & Inspection the … The certification plan should consider the relevant Certification Specification (CS) for the aircraft (e.g. In legal terms, Airworthiness Directives (AD’s) do not automatically apply to EASA permitted aircraft. Prasanth. 1. The mechanism that is used is the minor change, even if the modification would normally be classified as STC (ie, a major change). Annex II types are, by definition, not EASA aircraft and are therefore handled under national rules. 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