Law 48/1960 of 21 July on Air Navigation sets out in Article 36 the requirement that all aircraft be fitted with an airworthiness certificate.

This article establishes the competence of the Ministry of Public Works for the issue of this certificate to civil aircraft, so it must be understood, that this competence has the Ministry of Defense for the aircraft that are considered to be military or belong to the Armies, institutes, agencies or services that are dependent on or linked to the Ministry of Defense.

With the publication of Royal Decree 2218/2004 of 26 November, approving the Regulations on Air Navigation of Defense, the mandate of the Law 48/1960, of July 21, was fulfilled. by regulatory means the requirements and tests necessary for the issue and renewal of the certificates relating to the airworthiness of the aircraft, as well as their period of validity.

The experience gained since the entry into force of Royal Decree 2218/2004 of 26 November, the appearance of the air systems piloted by remote control in the fleets of the Armies and the importance they have in the Spain's major international aviation programmes with the participation of Spain, make it necessary to deal with the approval of a new Defence Aircraft Regulation to adapt it to current circumstances.

In addition, it is necessary to include in the scope of the regulation to the Civil Guard, since this armed institute uses aircraft that have the consideration of military aircraft, in accordance with Article 14.1 of the Law 48/1960 of 21 July.

In the process of processing, in order to comply with the provisions of article 24.1.c) of Law 50/1997, of 27 November, of the Government, and to evacuate the process of hearing to the citizens or associations or bodies that represent them, this royal decree has been submitted to consultation of professional associations and business associations whose purposes are directly related to the object of the provision.

The objective of this royal decree is to establish the process by which an aircraft obtains the certificate of airworthiness, for which it is established as a prerequisite that the design of the aircraft has one of Type Certificates that are described in the same.

The application for the issuance of any Type Certificate, as well as the requirements to be met and the documentation to be delivered, are defined in Chapters III, IV, V, VI and VII of this royal decree.

In its virtue, on the proposal of the Minister of Defense, with the prior approval of the Minister of Finance and Public Administrations, according to the State Council and after deliberation by the Council of Ministers at its meeting of the October 2, 2015,

DISPONGO:

Single item. Adoption of the Regulation.

The Defense Airworthiness Regulation is approved, which is inserted below.

Single repeal provision. Regulatory repeal.

The Royal Decree 2218/2004 of 26 November, for which the Air Navigation Regulations of the Defense is approved, is hereby repealed, and the provisions of equal or lower rank that oppose the provisions of this real decree.

Final disposition first. Competence title.

This royal decree is issued in accordance with the provisions of Article 149.1.4. of the Constitution, which attributes to the State exclusive competence in the field of Defense and Armed Forces.

Final disposition second. Faculty of development.

The Minister of Defense is empowered to dictate in the field of his powers how many provisions are necessary for the development and implementation of the provisions of this royal decree.

The Minister of Defense and the Minister of the Interior are empowered to jointly dictate how many provisions are necessary for the development and implementation of the provisions of this royal decree in cases where the rules that are dictate affect the Civil Guard Corps.

Final disposition third. Entry into force.

This royal decree will enter into force on the day following its publication in the "Official State Gazette".

Given in Madrid, on October 2, 2015.

FELIPE R.

The Minister of Defense,

PEDRO MORENES EULATE

AIRWORTHINESS REGULATION OF THE DEFENCE

CHAPTER I

General provisions

Article 1. Object and scope of application.

1.This Regulation defines and regulates the various certificates guaranteeing the flight safety of military aircraft and air systems piloted by remote control, and establishes the procedures for their dispatch, the requirements to be met by the applicants for the certificates, and the rules to be followed by their holders and depositors in order to maintain their validity and to achieve their renewal.

2. This regulation applies to:

(a) All aircraft, military air systems piloted by remote control, engines and propellers, hereinafter referred to as "products", used by the Armies, institutes, agencies or services dependent or linked to the Ministry of Defense or the Civil Guard, or that may be of interest to them or to the Spanish defense industry.

(b) Military aircraft or air systems piloted by remote control of foreign ownership only in the specific case of restricted airworthiness certificates or for experimentation, with limitations that are indicate in the relevant paragraphs of this Regulation, provided that there is the delegation of the Air-Navigation Authority of the aircraft that owns the aircraft to the Defence Aircraft Authority, hereinafter AAD, and accepted by is, when they are in the Spanish defense industry for:

1. Performing maintenance or modification jobs,

2. or conducting trials under the supervision or direction of the National Aerospace Technical Institute "Esteban Terradas", hereinafter INTA, or any other accredited testing centre.

3. This Regulation does not apply to aircraft with a registration of civil registration.

4. No aircraft or military air system flown by remote control of those covered by this Regulation shall be authorised for flight if it does not have the certificate of airworthiness applicable to it.

5. Any aircraft covered by this Regulation shall carry on board the certificate of airworthiness applicable to it during its shipments. For military air systems piloted by remote control, this document should always be available at the control station.

6. The provisions of this Regulation shall be without prejudice to the rules applicable in the case of a request for a certificate from the remote control aircraft or military aircraft operated by remote control in question. civil aviation authority.

Article 2. Certificate classes.

The certificates regulated in this regulation are as follows:

(a) Certificate of Type: document by which the AAD states that a product type has been designed and tested in accordance with the approved rules and procedures and is therefore considered safe for flight.

(b) Provisional Type Certificate: document by which the AAD states that for a product type, a degree of knowledge of its technical and technical characteristics has been achieved throughout the certification process. (a) a deep enough operation to enable the establishment of airworthiness limitations within which such a type is considered safe for flight.

(c) Supplementary Type Certificate: document by which the AAD states that a major modification to a design of a type that has been designed and tested by an organisation other than the holder of the type certificate, has demonstrated compliance with the applicable applicable requirements and procedures.

d) Certificate of Conformity: a document by which the signatory of a contract ensures that the product, component, equipment or service meets the contractual technical requirements.

(e) Certificate of Aptitude: a document by which the company or organization responsible for the production or maintenance of products, components or equipment ensures that the work carried out on them complies with the regulations of airworthiness applicable.

f) Certificate of Airworthiness: a document that is used to technically identify a military aircraft or air system piloted by remote control, define its characteristics and express the qualification it deserves for its use, deduced from the ground inspection and the relevant ground and flight tests.

g) Certificate of Airworthiness for Experimentation: document issued for that aircraft or military air system piloted by remote control that is in the prototype phase or used specifically for flights testing, in experimental or demonstration phase.

(h) Restricted Airworthiness Certificate: document issued for that aircraft or military air system flown by remote control which is covered by a type-certificate or a provisional type-certificate, but whose airworthiness is not fully demonstrated, although it is capable of safely performing some air operations.

i) Provisional airworthiness certificate: document issued for that aircraft or military air system flown by remote control which is covered by a provisional type-certificate, but which, independently of this, it meets all other requirements to obtain an airworthiness certificate.

j) Certificate of Airworthiness for Export: document issued for an aircraft or military air system flown by remote control for export or sale purposes.

k) Technical Certificate: a document that ensures that the tests, analyses and all types of tests and experimental work are carried out, necessary to demonstrate that they comply with the certification bases established for each product type or those modifications to the product type that require it.

The issue of certificates of type as defined in paragraphs (a), (b) and (c) above corresponds to the AAD. They must be signed by the aeronautical engineer, or personnel with equivalent qualifications in accordance with the current legislation, of the Industrial Inspection Area of the General Administration of Inspection, Regulation and Industrial Strategy of Defense, and shall be endorsed by the Defence Aircraft Authority.

The certificate of conformity shall comply with the provisions of Article 35 (2) and Article 36 of this royal decree.

The certificate of fitness shall be in accordance with Article 38 of this royal decree.

The issuance and renewal of the airworthiness certificates as defined in paragraphs (f), (g), (h), (i) and (j) above shall be subject to the provisions of Article 40 of this royal decree.

The technical certificate shall be issued by an aeronautical engineer, or personnel with equivalent qualifications in accordance with the legislation in force, recognised by the competent technical body issuing the certificate.

Article 3. Inventory of military aircraft and air systems piloted by remote defense control.

1.It will be carried out in the Directorate General of Armament and Material, hereinafter DGAM, of the Ministry of Defense, for the purpose of controlling the application of this regulation, the inventory of military aircraft and air systems piloted by remote control of the defence, in which all aircraft and military air systems piloted by remote control which fall within the scope of this Regulation shall be registered. The Board of Airworthiness shall determine the contents of this inventory.

2. The different Armies, institutes, agencies or services which are dependent or linked to the Ministry of Defence, which have aircraft or military air systems piloted by remote control, may constitute for the same purposes other inventories, in which, at least, the same data as those included in the inventory referred to in the preceding subparagraph shall be included. These inventories do not supply the inventory of military aircraft and air systems piloted by remote control of the Defense constituted in the DGAM.

3. Military aircraft and air systems piloted by remote control that may be of interest to the Ministry of Defense, the Civil Guard or to the Spanish defense industry must be included in the DGAM inventory. from the moment its owner requests the Ministry of Defense to apply this regulation.

CHAPTER II

Competent authorities and bodies

Article 4. The Air Navigation Authority of Defense.

1.The Director-General of Armament and Material is the Defense Airworthiness Authority and the senior executive authority resides in the application of this regulation.

2. For the exercise of its authority it shall be advised by the Board of Airworthiness.

Article 5. Board of Airworthiness.

1.The Airworthiness Board is the AAD's body of work and will be staffed with the personal, technical and budgetary means assigned to the DGAM.

2. It shall consist of the following members:

a) President: the AAD.

b) Vice-President: The Deputy Director-General for Inspection, Regulation and Industrial Strategy of Defence of DGAM.

(c) Vocals: The airworthiness representatives of the Army of the Earth, the Navy and the Air Force, the airworthiness representative of the Civil Guard, a representative of the General Inspection Subdirectorate, Regulation and Industrial Strategy of Defense of the DGAM, appointed by the AAD, a representative of the General Subdirectorate of Experimentation and Certification of the INTA appointed by the Director General of the INTA and the airworthiness representatives of all institutes, agencies or services which are dependent or linked to the Ministry of Defence or the Civil Guard with aircraft or military air systems piloted by remote control.

(d) Secretary: a representative of the Directorate-General for Inspection, Regulation and Industrial Strategy of Defence of the DGAM appointed by the AAD. For the purposes of Council meetings, the Secretary shall have a voice but not a vote.

3. The members of the Board of Airworthiness shall be aeronautical engineers.

4. The duties of permanent secretariat of the Board of Airworthiness shall be taken up by the Directorate-General for Inspection, Regulation and Industrial Strategy of Defence of DGAM.

5. A Competent Technical Body is an organisation recognised by the AAD with sufficient capacity, guarantees and procedures to be able to carry out directly or through other recognised bodies, the supervision of inspections, testing and On-shore and in-flight tests necessary for, after completion of the process, issue of a Technical Certificate and the corresponding data sheets of a product or may carry out certification tasks of design, production, training or maintenance of products and issuance of personnel licenses maintenance. The competent technical bodies to which the Board of Airworthiness will be of priority shall be the General Subdirectorate for Experimentation and Certification of the INTA and the Subdirectorate for Inspection, Regulation and Industrial Strategy of Defense of the DGAM.

6. The President of the Board of Airworthiness may convene experts when he considers it appropriate, to speak with a voice but without a vote.

7. The functions of the Airworthiness Board are as follows:

a) Approve the certification bases for obtaining the Type, Provisional Type and Supplemental Type Certificate.

(b) To report in advance on the issue of type, provisional and supplementary type certificates as well as their revisions.

c) Propose to the AAD the airworthiness directives deemed necessary, as well as establish the procedure for their preparation.

d) To inform in advance of the AAD rating of aeronautical engineers who issue and renew the airworthiness certificates referred to in this Regulation.

e) Establish the procedures for the approval of foreign documents relating to the maintenance of airworthiness of domestic and imported products.

(f) Develop in relation to airworthiness, general guidelines and procedures to be issued by the AAD for the development and interpretation of this Regulation and to harmonise its implementation in the field of each Army, institute, agency or service dependent or linked to the Ministry of Defence or the Civil Guard.

g) Support the AAD in relations with international civil and military airworthiness organizations and agencies, to know and propose the application of international standards and practices that are considered to be of interest and, in The European Defence Agency, in particular, from the scope of the European Defence Agency.

h) Promote training on issues of airworthiness of personnel who may be considered affected by the application of this regulation.

8. The actions of the Board of Airworthiness shall be in accordance with the provisions of Title II, Chapter II of Law 30/1992 of 26 November of the Legal Regime of Public Administrations and of the Common Administrative Procedure.

Article 6. Airworthiness representatives.

1.Each Army, institute, agency or service dependent or linked to the Ministry of Defense or the Civil Guard shall appoint from its aeronautical engineer personnel to the airworthiness representative. If you do not have such technical staff, you may delegate these functions to another Army, body, institute or service. If any of the above options are not possible, exceptionally, they may specifically designate appropriate technical personnel from another source with the express approval of the Airworthiness Board.

2. In the Logistics Command of each Army, and in each institute, agency or service dependent or linked to the Ministry of Defense or the Civil Guard, there will be a technical body responsible for managing the entire airworthiness process within the its own organisation, which shall have the approval of the AAD, which shall define in advance the requirements to be met by that body.

3. The functions of the airworthiness representatives shall be as follows:

a) Represent in the Board of Airworthiness to each Army, agency, institute or service or to the Civil Guard.

b) Coordinate all actions on airworthiness within your organization for the purposes of the particular application in each case of the provisions of this regulation.

c) Exercise the initiative for the issuance of airworthiness directives.

d) Propose to the AAD the aeronautical engineers who must be enabled to issue and renew the certificates of airworthiness regulated in this regulation and the aeronautical personnel empowered to issue and endorse the fitness certificates to be obtained.

CHAPTER III

Type certificate

Article 7. Type certificate.

1.The type certificate consists of:

a) The certificate itself.

b) The review sheet for the same.

c) The data sheet with the definition of the associated type design, reference to the flight manual, weights and centered manual and maintenance plan for aircraft, military air systems piloted by remote control and the documentation with equivalent information needed for other products.

2. In the case of military air systems piloted by remote control, the type-certificate refers to the complete system, i.e. the aircraft or set of aircraft, station or control stations, the data link and the elements of the launch and recovery, if available and any other elements of the system required for safe flight.

Article 8. Type layout.

1. A type layout consists of:

(a) The product plans and specifications, and a list of the drawings and specifications of the configuration elements, which make it possible to identify the configuration and aspects of the product, to demonstrate compliance with the requirements requirements of this Regulation applicable to the product.

b) Information about dimensions, materials, and processes required to define product characteristics.

(c) The section of the airworthiness limitations contained in the instructions for the maintenance of airworthiness.

(d) Any other data necessary to enable the determination of the airworthiness characteristics of subsequent products of the same type.

2. Each type design will be uniquely identified.

Article 9. Application for the issue of the type-certificate.

1.It may request a certificate of type from any public or private body or entity with a capacity to assume the responsibilities and obligations arising from its concession.

2. The application for the issue of the type-certificate shall be addressed to the AAD and may be submitted in the register of the DGAM or the Secretariat of the Board of Airworthiness in the Subdirectorate-General for Inspection, Regulation and Industrial Strategy In accordance with Law 11/2007 of 22 June 2007 on electronic access for citizens, the Defense Department of Defense or any of the places established in Article 38.4 of Law 30/1992 of 26 November, and the use of electronic means, in accordance with Law 11/2007, of 22 June to Public Services.

3. Such application shall be accompanied by:

a) The type layout.

(b) Calculations and analyses necessary to demonstrate or help demonstrate that the product to be certified complies with the certification basis.

(c) Reporting and test results (bank, land and flight) that demonstrate or help demonstrate that the product to be certified complies with the certification basis.

(d) The Technical Certificate of the Competent Technical Authority, if the applicant has, or its corresponding application.

4. For products covered by a valid civil type certificate in Spain, the Airworthiness Board shall determine the requirements for its validation.

5. The maximum time limit for resolving and reporting shall be six months from the day following the submission of the relevant application, understanding that the absence of a resolution, after that time limit, shall have an adverse effect. Against this resolution which puts an end to the administrative procedure, it is possible to bring the replacement of a replacement or be challenged directly before the judicial-administrative court order. In the allocation of jurisdiction to appeal, the organs of the State Administration and the public bodies created under their dependency are expressly excluded.

Article 10. Technical certificate.

1.This certificate will include, in addition to your review sheet:

a) The data sheet with the express mention of the definition of the type design.

b) Any other condition or limitation prescribed for the product to be determined by the Board of Airworthiness.

2. The Board of Airworthiness, through its Permanent Secretariat, shall be informed of the certification activities developed in the field of application of this Regulation.

3. All specifications of the elements, materials, equipment and accessories included in the design of the type and which shall be used in the manufacture of the products shall be previously documented and aero-qualified, and in their integration will not present any features or features that make your operation insecure.

4. For the purposes of Article 83.3 of Law No 30/1992 of 26 November 1992, this certificate shall be of a mandatory and decisive nature for the completion of the process of resolution and notification of the Type Certificate.

Article 11. Determination of the certification bases.

1.The certification bases are the rules, requirements and requirements of the applicable regulations for obtaining the type certificate, which will be established by agreement between the applicant and the Technical Authority Competent and presented to the Council of Airworthiness for approval.

2. To be determined, it shall be taken into account:

a) The rules of enforced compliance.

b) The regulations proposed by the applicant.

c) The rules applied in such products for domestic use.

(d) The rules applied by the national authority of the country of origin of the product, if this is of import.

e) The rules that have been agreed between the applicant and the contracting entity.

(f) The airworthiness requirements that the Competent Technical Authority or the applicant considers appropriate to the product to be certified.

g) The proposed compliance means.

h) The regulations established in international organizations in which Spain participates.

i) Any other requirement that the Board of Airworthiness considers appropriate.

3. If the Airworthiness Board does not manifest otherwise within two months of the day following the date of submission for approval, the initial certification basis shall be deemed to have been approved.

4. If no agreement is reached between the applicant and the Competent Technical Authority on the basis of certification, it shall be the Airworthiness Board that decides in that case.

Article 12. Demonstration of compliance with certification bases.

1.Once the certification bases have been approved, the applicant shall be notified for their knowledge and effects in carrying out the tests and tests that are necessary for their compliance.

2. The applicant shall allow the Competent Technical Authority, directly or through other bodies, to monitor the ground and flight inspections and tests necessary to demonstrate compliance with the certification bases.

3. For all types of aircraft or military air systems piloted by remote control, prior to the completion of the initial engine bearings in the prototypes and the first flight, the applicant shall carry out the studies, analyses and tests. Land tests necessary to ensure acceptable safety conditions for such operations. This shall be in accordance with Article 46.

4. The applicant, with the supervision of the Competent Technical Authority and in accordance with the certification plan agreed between them, shall make all inspections and tests on both ground and flight necessary to determine:

a) Compliance with certification bases and airworthiness requirements.

b) That the materials and products conform to the specifications of the type design.

c) That the parts of the products are in accordance with the design plans of type.

d) That the manufacturing, construction, and assembly processes conform to what is specified in the type design.

e) The limitations of Airworthiness.

5. Once the process of demonstrating compliance with the certification bases has been completed, the Competent Technical Authority shall issue a technical certificate.

Article 13. Issue of the type certificate.

Once the technical certificate has been issued, the AAD shall issue the type certificate, which shall be signed by an aeronautical engineer of the General Subdirectorate for Inspection, Regulation and Industrial Strategy of Defence favourable to the Council on Airworthiness.

Article 14. Type-certificate for imported products or resulting from international collaboration with the participation of the Ministry of Defense.

1.For the issue of the type-certificate of an import product, the Airworthiness Board may, if necessary, rely on the results of tests obtained at an official technical centre in the country of origin. In these cases, the issue of the technical certificate shall also be the responsibility of the Competent Technical Authority, subject to verification of compliance with the applicable rules of the procedures and methods of that centre.

2. The certificate of type can also be obtained by validation with that of the country of origin, provided that the Competent Technical Authority verifies the certification bases, for which the existence of reciprocal agreements will be taken into account. The documentation submitted shall be sufficient to enable the Competent Technical Authority to issue the relevant technical certificate.

3. For products resulting from an international collaboration program with the participation of the Ministry of Defense, the Board of Airworthiness will adapt the compliance of this regulation to the specific characteristics of this program.

Article 15. The validity of the type certificate.

The validity of the type certificate will be indefinite. However, the AAD may leave the type-certificate without validity if any of the conditions required for its granting are not met. To this end, the appropriate file shall be opened in which the holder shall be heard.

Article 16. Modifications that require a new type certificate.

1.A new type certificate must be requested from the AAD when the modifications proposed by the holder of the type certificate for a given product include:

a) For aircraft:

1. A change in the number of engines or rotors.

2. ° Changes in the propulsion principles of engines or rotors, or the latter using different operating principles.

b) For remotely piloted systems: In addition to the specific aircraft mentioned above:

1. º Change in the number or type of aircraft that make up the system.

2. º Change in the number or type of control stations that make up the system.

3. º Change in the principles of data control and transmission.

c) For aircraft engines, changes affecting the operating principle.

d) For propellers, a change in the number of blades or in the principle of operation of the step change mechanism.

2. A new type certificate must also be requested when the modification or set of proposed modifications in configuration, power, power constraints (engines), speed limitations (engines) or weight are such an extension. they assume, in the judgment of the Board of Airworthiness and prior report of the Competent Technical Authority, a substantial change in the type design, requiring a full investigation to demonstrate compliance with the applicable requirements.

CHAPTER IV

Provisional Type Certificate

Article 17. Provisional type certificate.

1.The provisional type-certificate fulfils the same characteristics as those expressed for the type-certificate of Chapter III, and shall only be issued when the requirements referred to in Article 21 are met.

2. The provisional type-certificate may be issued for products which are in a process of certification for the validation of a certificate of type issued by a certifying authority of a foreign country, provided that it is provide evidence to enable the requirements of this Chapter to be met by the Board of Airworthiness.

Article 18. Application for the issue of the provisional type certificate.

The application for the issue of the provisional type-certificate shall comply with the conditions set out in Article 9.

Article 19. Issue of the provisional type certificate.

Once the provisional technical certificate has been issued, the AAD shall issue the provisional type certificate, which shall be signed by an aeronautical engineer from the General Subdirectorate for Inspection, Regulation and Industrial Strategy of Defense of the Board of Defense of the Board of Airworthiness.

Article 20. Validity of the interim type certificate.

The interim type certificate will be valid for one year and can be renewed for equal periods of time.

Article 21. Requirements for the issue of the provisional type certificate.

1.The applicant for the provisional type certificate shall:

a) Haber requested type certificate.

b) Having secured approval by the Board of Airworthiness of the corresponding certification bases of the proposed type design and by the Competent Technical Authority of the certification plan.

c) Declare that:

1. The design complies substantially with the applicable airworthiness requirements for the issue of the requested type certificate.

2. The design is secure under the appropriate operating limitations and specified in paragraph e) of this article.

d) Submit a report demonstrating that the aircraft or military air system piloted by prototype remote control has been flown by performing all necessary manoeuvres to substantially test compliance with the requirements for the issue of the requested technical certificate, and to establish that the aircraft or military air system piloted by remote control can be operated safely, in accordance with the limitations contained in this article.

e) Demonstrate all the limitations required for the issue of the requested technical certificate, including the limitations of weights, centering, speeds, loading, flight manoeuvres, operation of the controls and systems, less than, for each limitation not established, the appropriate operating restrictions of the military aircraft or military air system are imposed by remote control.

f) Credit that a prototype of the aircraft or military air system piloted by remote control has made at least 50 hours of flight time.

g) Submit a flight manual and a manual of weights and focus that contains the limitations set forth in this article.

h) Submit the airworthiness maintenance instructions through an inspection and maintenance plan to ensure the airworthiness of the aircraft or military air system piloted by remote control.

2. In addition, it shall be determined that there is no indication, feature or condition that makes the aircraft or military air system remotely piloted by remote control when operated in accordance with the limitations set out in paragraph 1.e) of this Article.

CHAPTER V

Type design modifications and requirements for approval

Article 22. Classification of modifications to the type design.

Type design modifications are classified as major and minor. A major change is that which, without falling within the meaning of Article 16, has an appreciable effect on the weight, balance, structural resistance, reliability, operating characteristics or other characteristics affecting the airworthiness of the product. They shall also have this consideration for software modifications that may contribute to a failure in a system function which result in a failure to safely continue the flight or landing of the unmanned aircraft or aerial vehicle; or The armed, loose or blocking of the arms, or those resulting from an engineering process associated with a change of processor, shall be carried out in an inadvertent manner. All other modifications are minor.

Article 23. Approval of major modifications to the type design.

1.The major modifications will be approved by the Competent Technical Authority. If the applicant is not the holder of the type-certificate, it shall apply as set out in Chapter VII.

2. The applicant should submit substantial and descriptive data to the Technical Authority (plans, technical design documents, tests, calculations, airworthiness maintenance instructions, etc.). Once approved, if the Competent Technical Authority considers a new type-certificate or a revision of the certificate to be necessary, it shall forward the relevant proposal to the Airworthiness Board, in order for it to take its decision.

3. For products manufactured by the domestic industry for export purposes, the Board of Airworthiness may delegate to the Competent Technical Authority the determination of the requirement for a new type certificate or a revision of the existing.

4. For import products, the Airworthiness Board shall establish special approval procedures duly sanctioned by the AAD.

5. Prior to the installation of the modification it must be demonstrated that the relationship between it and any other previously installed modification or major repair does not introduce any adverse effect on the airworthiness of the product.

Article 24. Approval of minor modifications to the type design.

1.Minor modifications to the type design shall be approved by the Competent Technical Authority, to which the applicant shall provide the information necessary for its assessment, which must include at least plans and descriptions of the type of design. modifications.

2. The Competent Technical Body may delegate to the applicant, after recognition of its technical training, such approval. The procedures for the delegation shall be drawn up by the Board of Airworthiness and duly sanctioned by the AAD.

3. The Armies, institutes, agencies or services that are dependent on or linked to the Ministry of Defense or the Civil Guard may approve minor modifications to the design of the type that correspond to their respective areas, in accordance with the the procedure to be established by the AAD on a proposal from the Board of Airworthiness.

4. Modifications approved by a Foreign Aeronautical Authority applicable to military aircraft or air systems piloted by remote control in service may be approved by the Armies, Institutes, Agencies or Dependent Services or linked to the Ministry of Defence in accordance with the procedure established by the Board of Airworthiness duly sanctioned by the AAD.

Article 25. Airworthiness Directives.

1.The Airworthiness Directive is a change in the type design to restore safety levels as a result of a failure, defective operation or defect in that design affecting flight safety.

2. Where the AAD issues an airworthiness directive, the holder of the certificate of type:

a) Facilitate the modifications made to the type design to all operators of the products covered by this type certificate.

b) You will enter the required modification in the new products.

Article 26. Determination of the certification bases for modifications of the type design.

1.Any modification of the type design must comply with the same certification bases used in obtaining the type certificate.

2. If the Competent Technical Authority considers that a proposed modification results in a new design, or a complete redesign of system or equipment elements or installations, a new determination of the certification bases shall be made.

Article 27. Reports of failures, defective functions, and defects.

The holder of a type, provisional or additional type certificate and airworthiness representatives shall inform the AAD and the Board of Airworthiness through its Permanent Secretariat, within the time limit. as short as possible and with the inclusion of all information available and applicable to the case, of any accident, incident, failure, defect or malfunction in any system, subsystem, equipment or element which, by its nature, generality or persistence, directly or indirectly, affects security in flight of the aircraft or military air system flown by remote control.

Article 28. Maintenance of airworthiness and documentary reflection of modifications.

1.It is the set of actions conducive to maintaining the initial airworthiness conditions by means of established procedures and covered by the type certificate. These actions, as well as the technical and human resources necessary for them, will be in accordance with the regulations established by the AAD.

2. Modifications made to a product in service, covered by a type certificate, or on its documentation, shall be reflected in an approved service bulletin or technical order, prior to its referral to the user.

3. Those documents shall be approved in accordance with the provisions of Articles 23, 24 or 25 as applicable.

CHAPTER VI

Revisions of the type certificate

Article 29. Request to review the type certificate.

In order to modify a product covered by a type certificate with the introduction of a major modification generated by the holder of the type-certificate not provided for in Article 16, the AAD must be requested to issue a revision of the original type certificate. This request shall be made in accordance with Article 9.

Article 30. Determination of the certification bases in the revisions of the type certificate.

To determine the certification bases will proceed as indicated in Article 26 for modifications of the type design.

Article 31. Issue of the review of the type certificate.

The revision of the type certificate will include the annotation in the revision sheet of the original product type certificate, the revision of the data sheet, which collects the approval of the proposed major modification with the conditions specified in Article 23 and the revision of the technical certificate.

CHAPTER VII

Supplemental type certificates

Article 32. Request for a supplemental type certificate.

The application for the supplementary type certificate must be addressed to the AAD, which is the responsibility of the AAD, and shall include proof that the necessary information is available for the design of the type to which it is applicable, either with the own resources of the applicant, or by means of agreements with the holder of the type-certificate.

Article 33. Identification of the certification bases for a supplementary type certificate.

The certification bases applicable to a major modification which is intended to be covered by a supplementary type certificate shall be established by agreement between the Competent Technical Authority and the applicant, approved by the Airworthiness board and must be based on the originals that were used to certify the design of the type to be modified.

Article 34. Requirements for the issue of a supplementary type certificate.

1. The holder of a supplementary type certificate shall draw up, maintain and update the manuals required by the applicable type certification criteria, by means of the necessary amendments covering the changes introduced by virtue of the of the major modification covered by the supplementary type certificate, and to provide copies of these manuals to the Competent Technical Authority when requested.

2. The Airworthiness Board shall impose additional requirements on the applicant for a supplementary type certificate to ensure the continued airworthiness and safety levels of aircraft as well as compliance with the requirements of this Regulation. of their obligations.

3. The organisation which would have designed and tested the major modification should be recognised as a Design Organisation with sufficient scope for the design of complete aeronautical products. This recognition should include in particular the following procedures to be regularly audited:

(a) Those that ensure continued airworthiness of the certified design and of the military aircraft or air systems piloted by remote control covered by such supplementary type certificate.

(b) Those defining a structure capable of carrying out the analysis of data after the notification of accidents, incidents, failures, defects or defective functions which may result in airworthiness directives, and define the appropriate corrective actions.

c) Those defining the generation and distribution to operators of service bulletins, modifications and maintenance information necessary to ensure compliance with the airworthiness directives applicable to the product.

CHAPTER VIII

Compliance and fitness certificates

Article 35. Issue of the certificate of compliance.

1.The manufacturer shall issue a certificate of conformity for each product serial number. You may also issue such a certificate for principal sets when required and for all items that are contractually requested.

2. The procedure for issuing the certificate of conformity shall be as follows:

(a) In the case of products of national manufacture, the certificate must be signed by the recognized representative of the manufacturer's quality organization, in accordance with its own rules accepted by the Ministry of Defense, and must be endorsed by the representative of the official Quality Assurance, hereinafter RAC, corresponding, named to the effect.

b) In the case of foreign-made products:

1. If this is a country that has a Mutual Support Agreement with Spain with Spain, it will apply the provisions of national manufacturing, with the exception that the endorsement will have to do so. the relevant official body of the manufacturer country or, where appropriate, the relevant RAC, appointed for that purpose.

2. In the case of a country not included in the previous point, the provisions for domestic products shall apply, except that the endorsement shall be made by an official organisation outside the country of origin. manufacturer or, where appropriate, the relevant RAC, appointed for that purpose.

Article 36. Endorsement of the certificate of compliance.

1.This certificate must always be endorsed by a representative of the Industrial Inspections Area of the Directorate-General for Inspection, Regulation and Industrial Strategy of Defense of the DGAM. For products of non-Spanish origin, this endorsement shall be obtained by delegation or directly.

2. The endorsement shall ensure that the manufacture of the product has been carried out in compliance with the quality publications corresponding to those included in the STANAG 4107 "Mutual Acceptance of Government Quality Assurance" (Mutual Acceptance of the Product). Official Quality Assurance) and must always ensure that the products that have been manufactured according to the applicable specifications and drawings that define the type design.

Article 37. Documentation required for the endorsement of the certificate of compliance.

1.The following documentation shall be required for the endorsement of the certificate of conformity:

(a) In the case of domestically made products covered by a type certificate:

1. Type Certificate.

2. º Definition of the design standard for the manufacture of the aircraft endorsed by the Competent Technical Authority.

3. The ratio of deviations and derogations accepted by the contracting authority or the corresponding RAC, if this is established.

4. ° Relationship of functional tests signed according to the manufacturer's quality organisation representative with the appropriate RAC visa when applicable.

5. The manufacturer's test flight acceptance document, if applicable.

6. The Customer Test Flight Acceptance Document, if applicable.

7. Data sheet of engines and propellers installed with their operating time, in the case of aircraft and military air systems piloted by remote control.

b) In the case of foreign-made products, the documentation to be provided shall be defined by the National Quality Assurance Authority, hereinafter the ANAC, for each particular case and shall be equivalent to that required for domestic manufacturing products.

2. The ANAC shall also determine the documents that require official endorsement.

Article 38. Certificate of aptitude.

1.This certificate shall be signed by the staff with the appropriate qualifications, training and experience in the product concerned, as defined by the Board of Airworthiness and designated by the responsible organisation carrying out the work of production or maintenance on the products or elements. This certificate ensures that the actions referred to in Article 43 (2) (b), (c), (d) and (e) have been carried out correctly. If they have been carried out in different establishments, the above staff, designated by each of them, shall issue their own certificate.

2. In the case of work in the industry, these certificates must be endorsed by the staff with the appropriate qualifications, training and experience, as defined by the Board of Airworthiness, designated for the purpose by the Ministry of Defence, Army, body or institute or service which has contracted the work.

3. In the case of work carried out by the foreign industry or maintenance centres, the holder of the aircraft or military air system piloted by remote control may adapt the compliance of this requirement to the characteristics of the aircraft. same.

CHAPTER IX

Airworthiness Certificates

Article 39. Certificate of airworthiness.

1.This certificate shall include an express reference to the type certificate for the aircraft or military air system flown by remote control and its data sheet.

2. The possession of this certificate in force indicates that the aircraft or military air system piloted by remote control:

a) It is an approved design and is therefore covered by a type certificate.

b) It has been manufactured according to the type design by approved procedures.

c) Since the beginning of its life cycle, it has been constructed, inspected and maintained according to approved plans and procedures, which have been designed to maintain airworthiness.

Article 40. Issue and renewal of certificates of airworthiness.

1.The issue and renewal of the airworthiness certificates covered by this Chapter is the responsibility of the AAD. They must be signed by an aeronautical engineer, or personnel with equivalent qualifications in accordance with the legislation in force, enabled by the AAD and designated for the purpose under procedure established by the Board of Airworthiness and approved by the AAD, provided that the documentation provided and the result of the ground and flight inspections clearly demonstrate the safety of the aircraft or the military air system by remote control for the flight, except for the certificates of restricted and experimental airworthiness, for which they are not necessary in-flight tests.

2. The maximum time limit for resolving and reporting shall be six months from the day following the submission of the relevant application, understanding that the absence of a resolution, after that time limit, shall have an adverse effect. Against this resolution which puts an end to the administrative procedure, it is possible to bring the replacement of a replacement or be challenged directly before the judicial-administrative court order. In the allocation of jurisdiction to appeal, the organs of the State Administration and the public bodies created under their dependency are expressly excluded.

Article 41. Documentation necessary for the issue of the certificate of airworthiness.

1.The following documents shall be required for the issue of the airworthiness certificate:

a) For new remote control aircraft or military aircraft systems:

1. º Copy of the type certificate that protects the military aircraft or military air system by remote control.

2. Certificate of Conformity.

3. º Documentation identifying the aircraft or military air system piloted by remote control.

4. º Accreditation of the ownership of the military aircraft or military air system by remote control.

5. º Photography in accordance with the regulatory model provided for in Annex III.

6. The applicant's declaration to be in possession of the flight manual, the manual of weights and centering, the maintenance manual, the maintenance plan, and the illustrated catalogue of parts, approved and updated according to the documentation.

7. The relationship of applicable applicable airworthiness directives applied and pending to be incorporated.

b) For used military aircraft or military air systems used by remote control:

1. The same documentation as for new remote control aircraft or military air systems, except for the manufacturer's certificate of conformity.

2. The last airworthiness certificate.

3. The Relationship of Service Bulletins and Embedded Technical Orders.

4. Documentation that clearly reflects the previous life of the aircraft or military air system piloted by remote control so that it can technically assess its status.

2. In the event that any of these documents cannot be obtained, the Airworthiness Board shall determine the equivalent test to be provided.

Article 42. Validity of the certificate of airworthiness.

1.The validity of the certificate of airworthiness shall be one year and shall be renewed in accordance with the provisions of Article 43.

2. The maintenance of airworthiness during the period of validity is the responsibility of the Army, agency, institute or service owner or user of the aircraft or military air system piloted by remote control, according to its internal organisation and procedures. The AAD shall verify compliance with the applicable regulations through the corresponding joint audits between DGAM personnel and the corresponding Army, body, institute or service, the result of which will be reduced of the relevant organisation to exercise responsibility for the maintenance of airworthiness.

3. The certificate of airworthiness shall lose its validity, in addition to the completion of its validity period, in the following cases:

(a) By accident or breakdown involving a major repair according to the classification of Article 49.

(b) For failure to meet in-time required compliance modifications or inspections ordered in airworthiness directives.

c) By entry into general review of the aircraft or military air system piloted by remote control.

(d) By specific provision of the AAD when, on a reasoned proposal from the Aeronautical Representative of the organisation responsible for the maintenance of the aircraft or military air system flown by remote control, it is observed a safety degradation for the flight, even if none of the above mentioned assumptions are made.

Article 43. Documentation necessary for the renewal of the airworthiness certificate.

1.The renewal of the certificate of airworthiness shall be requested when any of the loss of life scenarios described in Article 42 occur.

2. The aeronautical engineer responsible for the renewal shall at least require the following documentation:

a) Last certificate of airworthiness issued.

b) Approved maintenance plan and work done and pending, according to the plan, since the last renovation.

(c) A documented relationship of repairs, breakdowns and corrective actions carried out since the last renewal or issue.

(d) List of airworthiness directives distributed by the Council of Airworthiness in force for the products concerned incorporated since the last renewal or issue and the pending of incorporation.

e) Relationship of service bulletins and technical orders incorporated since the last renewal or issue.

f) Certificates of aptitude to proceed.

3. Verified documentation and carried out on ground and in-flight tests and tests on the aircraft or military air system flown by remote control by the competent technical staff, in accordance with the approved procedure and with satisfactory result, the designated aeronautical engineer shall renew the certificate of airworthiness.

Article 44. Cancellation of the certificate of airworthiness.

1.The certificate of airworthiness shall be cancelled where it is any of the documents which have been used as a basis for their issue or where one of them has been altered or distorted.

2. It shall also be nullified in the light of any change in the design or approved operation of the military aircraft or military air system by remote control that creates a new model.

Article 45. Certificate of provisional airworthiness.

The provisional airworthiness certificate shall be issued for remote control aircraft or military air systems that are covered by a provisional type certificate and their use shall be compliant. with the limitations specified in Article 21. Its validity shall be six months and shall never exceed that of the provisional type-certificate itself. The conditions for their emission shall be the same as those specified for the normal airworthiness certificate.

Article 46. Certificate of limited airworthiness.

1.For dispatch the aircraft or military air system piloted by remote control must have a valid type or provisional type certificate and be able to safely perform any of the operations listed:

a) Aircraft or military air systems piloted by new remote control: Verification and production acceptance flights.

b) Aircraft or military air systems piloted by used remote control:

1. Verification and acceptance flights after factory or maintenance maintenance work, for which the certificate of airworthiness has lost its validity.

2. No flights to the industry or maintenance center with expired airworthiness certificate.

3. º Flights with an expired airworthiness certificate, without any immediate renewal.

4. No flights out of established airworthiness limitations, for specific and determined operations (e.g. with excess weight, without the totality of operational instruments, on the sea, etc.).

5. Test flights for the issue of certificates of airworthiness or renewal for which they have lost their validity.

2. In all cases, the safety conditions and the corresponding flight limitations shall be established by the holder or the technical personnel responsible for the material, and approved by the aeronautical engineer designated for the issue of the certificate.

3. In the case of military aircraft or air systems piloted by remote control of non-Spanish ownership, a certificate of type as defined in this Regulation shall not be required. The restricted certificate shall be issued only for flights of verification of the work carried out and it shall be a prerequisite for their dispatch that there is a request from the owner of the aircraft or military air system flown by control. remote and a delegation to the AAD of the airworthiness authority that issued the type certificate for the aircraft or military air system flown by remote control. In these exceptional cases the restricted airworthiness certificate shall be issued only for verification or acceptance flights.

4. The validity of this certificate shall be limited to the number of flights specified and shall never be longer than three months, although in special circumstances it may be renewed as long as these persist.

Article 47. Certificate of airworthiness for experimentation.

1.This certificate applies to aircraft or military aircraft systems piloted by remote control which are used for in-flight tests for development and research and for demonstration of certification bases, as well as for training of Test crews.

2. The certificate shall be issued by an aeronautical engineer empowered by the AAD, the responsible testing centre in which the test flights are to be carried out or the Competent Technical Authority.

3. The applicant shall submit a declaration of airworthiness for the issue to be accepted by the aeronautical engineer empowered to ensure an adequate level of safety.

4. The validity of the certificate shall be six months maximum, renewable for equal periods, during which the following requirements shall be met:

(a) In the case of aircraft or military air systems piloted by remote control that are the responsibility of an industry:

1. º The test orders issued by the applicant to perform the test flights shall be within the limits set out in the airworthiness declaration accepted by the Competent Technical Authority.

2. The configuration of the prototype, changes in that configuration and its associated documentation will follow the applicable procedure issued by the Competent Technical Authority.

(b) In the case of aircraft or military air systems piloted by remote control which are the responsibility of or linked to the Ministry of Defence, the test centre shall follow the control processes of the configuration and approval of modifications approved by the Board of Airworthiness and duly sanctioned by the AAD.

Article 48. Certificate of airworthiness for export.

1.This certificate guarantees that the aircraft or military air system operated by remote control to which it has at least the level of security sufficient for the flight of shipment to the importing country, with the limitations that in it specify.

2. This certificate does not constitute a document authorising the free movement of the aircraft or military air system flown by remote control and shall only allow the flights necessary for export.

CHAPTER X

Repairs

Article 49. Definition and classification of repairs.

1.Repair means the elimination of damage and/or recovery of airworthiness conditions after initial commissioning.

2. Removing damage by replacing items or equipment without the need for any design activity will be considered a maintenance task and therefore is not considered a repair or requires approval.

3. Repairs are classified in larger and smaller ones with the same criteria as those specified in Article 22.

Article 50. Approval of repairs.

1. For the approval of major repairs by the Competent Technical Authority, the applicant shall submit the substantial data (technical documents, calculations, demonstration of compliance with the certification bases, etc.).

2. Minor repairs must be approved by the Competent Technical Authority, unless it has delegated this faculty to the applicant, once its technical training has been recognized. The procedures for such delegation shall be set and approved by the Board of Airworthiness.

3. In the case of repairs necessary to fly a military aircraft or military air system operated by remote control outside the national territory, the Army, agency, institute or service that has the responsibility of the maintenance of airworthiness, as an emergency situation, shall designate an aeronautical engineer for the approval of the repair to allow the flight to a maintenance centre.

ANNEX I

Abbreviations

AAD: Defense Airworthiness Authority.

ANAC: National Quality Assurance Authority.

DGAM: General Directorate of Armament and Material.

ESF: Equivalent Safety Finding.

INTA: National Aerospace Technique Institute "Esteban Terradas".

MCRI: Military Certification Review Item.

RAC: Official Quality Assurance Representative.

ROD: Design Organization Recognition.

STANAG: NATO Standardisation Agreement.

UAV: Unmanned aerial vehicle.

ANNEX II

Definitions

For the purposes of this regulation, the following definitions apply:

Aircraft: is every vehicle capable of navigating through the air. For the purposes of this Regulation, the vehicle may be equipped with a fixed or a throwable installation and is part of the vehicle itself.

Airworthiness: is the quality that makes a aircraft safe for the flight. It is the property of an air system in a given configuration, to safely achieve, maintain and finish a flight according to the approved usage limitations.

Continued airworthiness or maintenance of airworthiness: it is the set of actions conducive to maintaining initial flight safety conditions by means of established and approved procedures.

Certification bases: Set of airworthiness requirements and associated compliance methods for a specific product certification process.

Service Bulletin: is the document issued by a manufacturer that defines the modifications that are intended to be made to products in service and the procedures for incorporation.

Aeronautical rating: is the official declaration of compliance with military standards or, failing that, civilians for aeronautical use.

Configuration: The physical and functional characteristics of the product as described in the design.

Declaration of Airworthiness: the declaration made by the applicant prior to the conduct of the first flight or in-flight tests, where the results of the studies, analyses and ground tests are established, as well as the airworthiness and operational limitations necessary to ensure the acceptable security conditions for such operations in the proposed flight envelope.

Airworthiness Directive: Document issued or adopted by the Board of Airworthiness and ratified by the AAD, which defines mandatory actions to be carried out on one or more aircraft, when evidence shows that the airworthiness of these aircraft may be otherwise compromised.

Manufacturing Design Standard: is the product definition manufactured in accordance with the type design and all modifications and operation procedures subsequently approved.

Manufacturer: Company responsible for product warranty.

Propeller: A mechanism that, by turning around its axis, produces traction, driving, or support forces.

Model: It is all development of an approved type that differs from it in minor and minor modifications not important enough to constitute a new type.

Engine: a machine designed to produce movement at the expense of a source of energy. All types of aircraft engines are included regardless of the power source used and the propulsion system.

Maintenance Plan: is the plan established to prepare instructions for the continued airworthiness of each type of aircraft, engine, or propeller. These instructions should contain the information necessary to perform the maintenance of the product and should include a section entitled "airworthiness limitations", which should contain the necessary information on the elements with life limited, the mandatory inspection intervals for the structure and the related systems and procedures.

Technical order: is any military technical document that affects operation, maintenance, or type design.

Remote-controlled military air systems: Comprises individual elements of the unmanned aerial vehicle system (hereinafter "UAVs"), which include the UAV, the ground control station and any other element required to allow the flight, such as the communications link or the launch and recovery system.

Software: set of programs, instructions, rules, etc., that allow the computer to perform certain tasks.

Type: Design of a product that meets each and every one of the standards and technical specifications imposed on the certification bases.

Holder: in relation to a type certificate, it is the public or private body or entity with the capacity to assume the responsibilities and rights deriving from its concession.

Unmanned Aerial Vehicle (UAV): A propelled aerial vehicle that does not carry personnel as an operator on board. The UAVs include only those vehicles controllable on all three axles. In addition, a UAV:

a) You are able to stay in flight by aerodynamic means.

b) It is remotely piloted or includes an automatic flight program.

c) It is reusable.

d) It is not classified as a guided weapon or a similar single-use device designed for the launch of weapons.

Version: It is all development of an approved model that differs from this one only in minor modifications.

Note: any technical document relating to airworthiness not covered by the names referred to here shall be classified, in accordance with its specific content, in one of those of this Regulation.

ANNEX III

Regulatory photographs

The photographs of the aircraft for the file must conform to the following rules:

Size to allow the aircraft or military air system to be viewed by complete remote control, with non-margin and color-based, flat-bottom, smooth and uniform format.

Side view of the left side of the aircraft or military air system by remote control, with the longitudinal direction, axis X, of the aircraft, located at the perpendicular of the optical axis of the used chamber.

The aircraft or military air system piloted by remote control shall occupy as much space as possible from the photograph, with no part or part of it being cut into the margins.

In the case of helicopters, the rotors ' blades shall be positioned so that the length of the helicopter is maximum in the photograph.

The military registration or identification of the military aircraft or military air system shall be distinguished by remote control, as well as its tactical flag.

ANNEX IV

Data sheet content

The data sheet is part of the type certificate and the technical certificate and includes the certification bases, the limitations prescribed in them, and any other limitations or information deemed necessary for ensure the safe operation of the products.

The information contained in the data sheet can have security classification, so it may or may not be in public use and be subject to the restrictions that the security regulations set.

For aircraft, at least contain:

a) General information:

Identification of aircraft type.

Identification of certificate holder.

The revision number and date of this.

List of effective pages.

Each model will be in a separate section, accepting a common data section.

b) Specific information:

Include the required for each aircraft model when applicable. It shall be at least the following:

Engines and their limitations.

Helices and their limitations.

Approved fuels and lubricants.

Speeds and their limits.

Accelerations and their limitations. Burst and maneuver diagrams.

Center of gravity and position margin.

Weights based on the center of gravity. Maximum, minimum and operating weights. Manual of weights and centering.

Shipped general software and its limitations.

Geometric references of aircraft, aerodynamic mean cord, levelling devices.

Minimum crew.

Maximum number of seats.

Maximum load capacity.

Maximum capacity of fuels and lubricants.

Maximum altitude and radius of action.

Movement of control surfaces and tolerances of these.

Ground-specific equipment.

-RESERVED weaponry.

Certification bases.

List of approved teams.

Flight manuals. List of limited-life items.

List of approved models and versions.

Maintenance Plan.

For military air systems by remote control, at least contain:

a) General information:

Identification of the aircraft class and ground station that integrate the military air system piloted by remote control.

Identification of certificate holder.

The revision number and date of this.

List of effective pages.

b) Specific information:

Definition of the military air system type design by remote control.

It will include the required information for each aircraft model (UAV) that is part of the system. It shall be at least that referred to in the previous paragraph.

It will include the required control station information:

Aircraft operators.

Mission operators.

Operation Limits

Operation zones.

c) Certification bases:

Applicable airworthiness requirements.

Special conditions, deviations, non-compliances, and exceptions.

Security Equivalent Determinations.

For engines, at least contain:

a) General information:

Engine Type/Variant.

Type certificate holder.

Identification of the certificate.

List of effective pages.

Date of issue of type certificate.

Each engine model will be in a separate section, accepting a common data section.

b) Specific information:

Definition of type layout.

Schema description of the engine type.

Equipment.

Dimensions and weights.

Operating Regimes.

Control system.

Approved fluids (fuels, lubricating oils, etc. ..).

c) Operation limits:

Temperature limits.

Maximum Allowable Rotational Speed.

Pressure limits.

Installation conditions.

Limitations for delivery.

d) Certification bases:

Applicable airworthiness requirements, including those deducted from MCRIs.

Special conditions, deviations, non-compliances, and exceptions.

Equivalent security determinations (FHS ' s).

e) Operation and commissioning instructions:

Engine operation instructions.

Engine maintenance plan.

Environmental conditions.

For propellers, at least contain:

a) General information:

Type/variant.

Type certificate holder.

Manufacturer of the propeller.

Date of issue of type certificate.

b) Specific information:

Definition of type layout.

Schematic description of the type of propeller.

Equipment.

Dimensions and weights.

Plans and schemas.

Operating Regimes.

Control system.

Approved fluids (hydraulic, lubricating oils, etc. ..).

c) Operation limits:

Power and maximum rotational speed at liftoff.

Power and maximum rotational speed continues.

Step angle.

Installation conditions.

Limitations for delivery.

d) Certification bases:

Applicable airworthiness requirements, including those deducted from MCRIs.

Special conditions, deviations, non-compliances, and exceptions.

Equivalent security determinations (FHS ' s).

e) Operation and commissioning instructions:

The operation instructions for the propeller.

Propeller maintenance plan.

Environmental conditions.