Appendix 2 APAA - "Atestado de Produto Aeronautico Aprovado" (Attestation of Approved Aeronautical Products) for Class II or III products and, CHE - "Certificado de Homologacao de Empresa" (Production Approval Certificate) for manufacturers of approved aeronautical products.
CTA address:
Centro Tecnico Aeroespacial Instituto de Fomento e Coordenacao Industrial Divisao de Homologacao Aeronautica P.O.Box 6001 Sao Jose Dos Campos - SP - 12225 Telex No. 1233393 BR Fax No. (55) (123) 41-4766 Phone No. (123) 41-4600
2.3 DEPV - Directoria de Eletronica e Protecao ao Voo (Electronics and Flight Protection Directorate). The DEPV is responsible for the Air Traffic Control System.
DEPV address:
Diretoria de Eletronica e Protecao ao Voo Praca Senador Salgado Filho, S/N Aeroporto Santos Dumont - 4 Andar 20021 - Rio de Janeiro/RJ Phone No. (021) 220-0515
2.4 CENIPA - Centro de Investigacao e Prevencao de Acidentes Aeronauticos (Aeronautical Accidents Investigation and Prevention Center). The CENIPA is responsible for accidents investigation.
CENIPA address:
Centro de Investigacao e Prevencao de Acidentes Aeronauticos Anexo Do M.Aer. 1 Andar Esplanada Dos Ministerios - Bloco "M" 70045 - Brasilia/DF Fax No. (061) 313-2597 hone No. (061) 313-2345
3. CERTIFICATION REQUIRED.
3.1 Except as provided in paragraph 3.6, to be eligible for registration on the Brazilian Registry, any aircraft model exported to Brazil (under a purchasing or leasing agreement) regardless of being new or used, must receive a Brazilian Type Certificate for 22
Appendix 2 import, issued on the basis of a U.S. Type Certificate, following the procedures established in [[paragraph]] 4.
3.2 To be eligible for registration on the Brazilian Registry, an aircraft model modified in accordance with an FAA Supplemental Type Certificate exported to Brazil, must receive a Brazilian Supplemental Type Certificate for import issued on the basis of the U.S. Supplemental Type Certificate following the procedures established in [[paragraph]] 5.
3.3 Except as provided in paragraph 3.6, to be eligible for installation on Brazilian registered aircraft, any aircrait engine or propeller model exported to Brazil, regardless of being new or used, must receive a Brazilian Type Certificate for Import, issued on the basis of a U.S. Type Certificate following the procedures established in [[paragraph]] 6.
3.4 To be eligible for installation on Brazilian registered aircraft for which a Type Certificate is required, any Technical Standard Order (TSO) approved product exported to Brazil, must receive a Brazilian approval for installation issued on the basis of a U.S. Technical Standard Order approval, following the procedures established in [[paragraph]] 7.
3.5 Other class II or class III products installed on Brazilian aircraft for which a Type Certificate is required, will be approved for installation through the Brazilian Type Certificate, following the procedures established in [[paragraph]] 8.
3.6 Certain models of aircraft, aircraft engines and propellers which have been exported to Brazil at a time where a Type Certificate tor Import has not been required, may continue to be exported with an exemption of the certification requirements established in this paragraph. To benefit from such exemption the applicant shall obtain a statement from the DAC validating the FAA type certification for operation in Brazil.
4. PROCEDURES FOR ISSUANCE OF IMPORT TYPE CERTIFICATES FOR AIRCRAFT.
4.1 An application Form FDH-300-11 (sample enclosed as Annex I) [[not enclosed in this advisory circular]] or an application letter shall be completed by the U.S. manufacturer of the concerned aircraft and forwarded to the DAC through the FAA, together with sufficient engineering information to permit the DAC to become acquainted with the type design.
4.2 The text of all FAA special conditions, equivalent safety items and exemptions from the airworthiness or noise requirements shall be made available to the CTA for review and approval.
4.3 A compliance check list with the certification basis indicating for each item of the requirement how it was complied (by test, analysis, calculation, design provisions, etc.) and the title 23
Appendix 2 and number of the corresponding substantiation document (report, drawing, specification, etc.), shall be made available to the CTA for review and approval.
The required markings and placards installed in passenger cabin, in cargo, baggage or stowage compartments and in the aircraft exterior, shall be presented in Portuguese or bilingual (Portuguese and English) form.
Brazilian Airplane Flight Manual and shall include a statement regarding its applicability to Brazilian registered aircraft.
Alterations eventually required to be incorporated in the Airplane Flight Manual will therefore be included directly on the affected pages of the Brazilian Airplane Flight Manual.
4.6 The use of the International System of Units, with the possible exceptions established in ICAO Annex 5, is required for the aircrait instruments, required markings and placards and for the Brazilian Airplane Flight Manual.
4.7 An engineering review of the type certification program conducted in the USA, shall be performed by the CTA, to establish the Brazilian requirements and special conditions for acceptance of the aircraft model. This review shall be conducted through meetings with the manufacturer and FAA representatives. At the end of such meetings the CTA will present a final validation report listing the requirements for acceptance of the aircraft model.
4.8 The CTA data needs will be listed in the validation report mentioned in the above paragraph and shall include all published Illustrated Parts Catalogs, Wiring Diagrams, Weight and Balance Manuals, Service Bulletins, etc.) and non-published documents (engineering reports, drawings, manufacturer specifications, etc.)
deemed necessary to substantiate the Brazilian approval and support the continuing airworthiness of the aircraft in Brazil.
being one The published documents shall be supplied in duplicat Both copy destinated to the CTA and the other to the DAC.
organizations must be included in the manufacturer's mailing list to receive regular updatings of such documents.
4.9 At least the following documents are also required for each aircraft delivered:
- Weight and Balance report.
- Electrical load analysis.
- Wiring diagrams.
- Production flight test report.
Appendix 2
- List of applicable FAA AD's indicating compliance status.
- Summary of maintenance, repairs, and alterations performed during the aircraft life (for used aircraft only).
4.10 To be eligible for operation under the Brazilian Registry, compliance with the DAC operating regulations (IAC) and special regulations appropriate to the envisaged flight operations, must be established. These regulations, which are incumbent upon the Brazilian operator, may require the installation of equipment and/or application of standards in addition to those required ior airworthiness certification. Such installations will be reviewed and approved by the CTA during the engineering review mentioned in [[paragraph]] 6 above.
4.11 A Brazilian CHT - "Certificado de Homologacao de Tipo" (Type Certificate) and corresponding "Especificacao de Aeronave" (Type Certificate Data Sheet) will be issued upon compliance with the requirements established on the validation report referred in [[paragraph]] 7 above.
PROCEDURES FOR ISSUANCE OF IMPORT SUPPLEMENTAL TYPE CERTIFICATES FOR AIRCRAFT.
5.1 An Application Form ADH-300-11 (sample enclosed as Annex I) [[not enclosed in this advisory circular]] or an application letter shall be completed by the U.S. holder of the FAA Supplemental Type Certificate (STC) and forwarded to the CTA through the FAA, together with sufficient engineering information to permit the CTA to become acquainted with the modification introduced in the type design.
5.2 A copy of the FAA Supplemental Type Certificate and its Addendum together with the text of all FAA special conditions, equivalent safety items and exemptions from the airworthiness Or noise requirements shall be made available to the CTA for review and approval.
A compliance check list with the requirements affected by the modification indicating for each item how it was complied (by test, analysis, calculation, design provisions, etc.) and the title and number of the corresponding substantiation document (report, drawing, specification, etc.), shall be made available to the CTA for review and approval.
The required markings and placards installed in passenger and Engie) form, image otherwise pectibed by the cript tugueset
5.5 The Airplane Flight Manual Supplement shali be identified as a Brazilian Airplane Flight Manual Supplement and shall include a statement regarding its applicability to Brazilian registered aircraft.
Appendix 2
5.6 An engineering review of the supplemental type certification program conducted in the USA, shall be performed by the CTA, to establish the Brazilian requirements and special conditions acceptance of the modified aircraft model.
This review shall be conducted through meetings with the holder of the FAA STC and FAA representatives. At the end of such review the CTA will present a final validation report listing the requirements for acceptance of the modified aircraft model.
5.7 The CTA data needs will be listed in the validation report mentioned in the above paragraph and shall include all alterations of the aircraft published documents developed by the STC holder (Airplane Flight Manual, Operations Manual, Maintenance and Repair Manuals, lllustrated Parts Catalogs, Wiring Diagrams, Weight anc Balance Manuals, etc.) and non-published documents (engineerinc reports, drawings, manufacturer specifications, etc.) deemed necessary to substantiate the Brazilian approval and support the continuing airworthiness of the modified aircraft in Brazil.
The alterations of the published documents shall be supplied in duplicate, being one sample destinated to the CTA and the other to DAC. Both organizations must be included in the STC holder mailing list to receive regular updatings of such documents.
5.8 At least the following documents are also required for each aircraft delivered:
- Updated weight and balance report.
- Updated electrical load analysis.
- Updated wiring diagrams.
- Production flight test report.
List of applicable FAA Airworthiness Directives (AD) indicating compliance status.
Summary of maintenance, repairs and alterations performed during the aircraft life (for used aircraft only).
5.9 A Brazilian CHST - Certificado de Homologacao Suplementar de Tipo" (Supplemental Type Certificate) and corresponding "Adendo" (Addendum) will be issued upon compliance with the requirements established on the validation report referred in [[paragraph]] 6 above.
6 . PROCEDURES FOR ISSUANCE OF IMPORT TYPE CERTIFICATES FOR AIRCRAFT ENGINES AND PROPELLERS.
6.1 An Application Form ADH-300-11 (sample enclosed as Annex I) [[not enclosed in this advisory circular]] or an application letter 26
Appendix 2 shall be completed by the U.S. manufacturer of the concerned aircraft engine or propeller, and forwarded to the CTA through the FAA, together with sufficient engineering information to permit the CTA to become acquainted with the type design.
6.2 The text of all FAA special conditions, equivalent safety items and exemptions from the airworthiness or noise requirements shall be made available to the CTA for review and approval.
6.3 A compliance check list with the certification basis indicating for each item of the requirement how it was complied (by test, analysis, calculation, design provisions, etc.) and the title and number of the corresponding substantiation document (report, drawing, specification, etc.), shall be made available to the CTA for review and approval.
6.4 An engineering review of the type certification program conducted in the USA, shall be performed by the CTA, to establish the Brazilian requirements and special conditions for acceptance of the aircraft engine or propeller model. This review shall be conducted through meetings with the U.S. manufacturer and FAA representatives.
At the end of such review the CTA will present a final validation report listing the requirements for acceptance of the aircraft engine or propeller models.
6.5 The CTA data needs will be listed in the validation report mentioned in the above paragraph and shall include all published documents (Installation and Operation Manual, Maintenance and Overhaul Manual, Illustrated Parts Catalog, Service Bulletins, etc.)
and non-published documents (engineering reports, drawings, manufacturer specifications, etc.) deemed necessary to substantiate the Brazilian approval and support the continuing airworthiness of the aircraft engine or propeller in Brazil.
The published documents shall be supplied in duplicate, being one copy destinated to the CTA and the other to DAC.
Both organizations must be included in the manufacturer mailing list to receive regular updatings of such documents.
6.6 A Brazilian CHT - "Certifacado de Homologacao de Tipo" and corresponding "Especificacao de motor ou helice" (Type Certificate Data Sheet) will be issued upon compliance with the requirements established on the validation report referred in [[paragraph]] 4
7. PROCEDURES FOR ISSUANCE OF INSTALLATION APPROVALS FOR ISO APPROVED PRODUCTS.
7.1 An Application Form ADH-300-11 (sample enclosed as Annex I) [[not enclosed in this advisory circular]] or an application letter 27
Appendix 2 shall be completed by the U.S. manufacturer of the concerned equipment and forwarded to the CTA through the FAA, enclosing the following:
Sufficient technical data to describe the product and its intended utilization;
- Installation and operational instructions;
Copy of the certification basis including the adopted standard or specification;
- Statement of compliance with the certification basis including a list (by title and number) of the substantiation reports developed for FAA certification; and
- The published documents such as: Maintenance and Overhaul Manuals, Parts Catalog, Service Bulletins, etc., may be also required.
7,2 After reviewing such documents, the CTA will advise the applicant by letter of any additional Brazilian requirements or special condition to approve the installation of the product on Brazilian aircraft.
7.3 A CTA letter of installation approval will be issued upon compliance with the requirements established in [[paragraphs]] 1 and 2 above.
8. PROCEDURES FOR APPROVAL OF OTHER CLASS II AND CLASS III PRODUCTS.
8.1 The U.S. manufacturer of such equipment may be required to supply information and documentation as may be deemed necessary by the CTA to justify its installation on a Class I product for which Brazilian certification is sought.
8.2 The Brazilian approval of such equipment will be granted by the issuance of the CTA Type Certificate for the Class I product on which they are installed.
which has received a Brazilian design approval according to paragraphs 4 thru 8, shai. be responsible for maintaining the CTA informed of all relevant information regarding the continuous airworthiness of its product in Brazil. This shall include prompt remittance to CTA of all information regarding hazardous service difficulties, corresponding design corrections, proposed operational design pirectives.
precautions and FAA Airworthiness Directives.
10. NOISE REQUIREMENTS.
10.1 The manufacturer who applies for an import type certification of a new type of aircraft, i.e., aircraft of a type 28
Appendix 2 which does not operate in Brazil, or for an Amendment to an existing CTA Type Certificate for a new model of aircraft, shall comply with the noise requirements of the RBHA (Brazilian Requirements for Aeronautical Certification) No. 36 or the ICAO Annex 16 rules.
The manufacturer who applies for an import type certification of an aircraft model whose type operates already in Brazil, although not type certificated by the CTA, shall comply with the acoustic alteration requirements of the RBHA No. 36, i.e., the model for which certification is sought shall not exceed the noise levels of the aircraft model of the same type which operates already in Brazil or the acoustical changes of the ICAO Annex 16 rules.
10.3 The STC holder who applies for an import supplemental type certification of an aircraft model which operates already in Brazil, regardless of having been or not type certificated by the CTA, shall comply with the acoustic alteration requirements of the RBHA No. 36,
i.e., the modified aircrait model shall not exceed the noise levels of the basic model or the acoustical changes of the ICAO Annex 16 rules.
11. EXPORT AIRWORTHINESS APPROVALS. Each Class I, II or III product exported to Brazil shall receive an FAA export airworthiness approval in accordance with Subpart I of FAR 21 which shall indicate that the product is in compliance with the Brazilian special requirements established in the final validation report.
Appendix 2
BRUNEI DARUSSALAM - SPECIAL REQUIREMENTS (Revised February 13, 1991)
1. GENERAL.
1.1 This document specifies the special requirements and conditions to be satisfied for the certification and use in Brunei Darussalam of aeronautical products of United States origin imported from the United States.
Authority for aircraft registration and certification is vested in the Department of Civil Aviation (DCA); correspondence should be addressed to:
Department of Civil Aviation Brunei International Airport Bandar Seri Begawan, 2015 Brunei Darussalam
1.3 Brunei Darussalam does not issue Type Certificates.
1.4 Eligibility for the issue of a Brunei Certificate of Airworthiness is determined by:
Compliance with the appropriate requirements of paragraphs 2, 3 and 4 of this document (but see also paragraph 5).
(b) Compliance with:
(1) Additional directives issued by the United Kingdom Civil Aviation Authority.
(ii) Airworthiness Notices issued by the United Kingdom Civil Aviation Authority.
NOTE: Compliance with this sub-paragraph (b) is not essential before export to Brunei Darussa_am. However, as it may be difficult to establish conformity in Brunei Darussalam, details of any relevant service document and modification status will be helpful to the Brunei user.
(c) Completion of a ilight test in accordance with a DCA approved Airworthiness Flight Test schedule unless otherwise agreed by the DCA.
2. ELIGIBILITY FOR EXPORT TO BRUNEI DARUSSALAM.
requirements of irements of this dacument. products must comply with the
2.2 In addition, aircraft must be eligible for the issue of a standard airworthiness certificate as prescribed in Subpart H of FAR Part 21 unless otherwise agreed by the DCA.
Appendix 2
3. ADDITIONAL REQUIREMENTS.
3.1 This subject identifies those design requirements additional to the FAR certification basis which must be satisfied for a particular aircraft type to be eligible for Brunei certification.
3.2 Additional Requirements for Brunei certification are not specified for fixed wing aircraft:
(a) below a maximum authorized weight of 2730 kg (6000 1bs).
(b) below a maximum authorized weight of 5700 kg (12500 lbs) when certification will not be applied for in the Transport or Aerial Work Categories.
NOTE: Brunei air navigation legislation requires the carriage of equipment on scales related to the purpose for which the aircraft is being flown. The aircraft commander is responsible for determining that an aircraft is properly equipped for any proposed flight.
3.3 For all aircraft other than those defined in paragraph 3.2 the DCA may prescribe Additional Requirements. Details for any individual aircraft type will be supplied on written application; a limited type evaluation by the DCA may be required when no previous example has been certificated in Brunei Darussalam. Equipment required to be carried on flights for the purpose oi pubiic transport, to satisfy Brunei air navigation legislation, will also be specified.
4. SPECIAL REQUIREMENTS.
4.1 This subject identifies those special administrative requirements which must be satisfied for particular products to be eligible for Brunei registered aircraft.
Applicability Code:
+ Required only with first of type and model exported to Brunei Darussalam.
* Required only for aircraft with a maximum authorized weight greater than 5700 kg (12500 lbs).
4.2 All Aircraft.
* (a) Statement of build standard. This statement must include the aircraft specification, changes in design to satisfy Brunei Additional Requirements and a list of Service Bulletins incorporated during manufacture. The list of Service Bulletins incorporated must identiiy:
Appendix 2
(i) Production versions of the Service Bulletins.
(ii) Service Bulletins.
(iii) Alert Service Bulletins.
(b) Copy of the production flight test report or a statement that no flight test has been completed.
(c) Modification standard. This must include:
(i) Customer options and equipment incorporated including items of equipment not necessarily installed by the manufacturer of the aircraft.
(ii) Service Bulletins compliance.
(d) Export Certificate of Airworthiness (see paragraph 4.4 of this document).
+ (e) A copy of the aircraft Type Certificate Data Sheet.
(f) Details of any alterations which may have been embodied under the Supplemental Type Certificate (STC) procedure.
NOTE: Any STC which has been embodied but not previously investigated by the DCA will be subject to evaluation before a Brunei Certificate of Airworthiness is issued.
(g) A list of the defects, if any, at the time of issue of the Export Certificate of Airworthiness which will require rectification by the Brunei operator.
(h) The FAA Approved Flight Manual or Pilot's Operating Handbook for the individual aircraft concerned, for approval by the
(i) Airframe/engine/propeller/auxiliary power unit log books.
* (j) Seating configuration approval document, where relevant.
+ (k) Maintenance Review Board document, where relevant.
(1) A summary of FAA approved retirement life limitations.
+ (m) Electrical load analysis.
NOTE: For aircraft other than first of type, the DCA requires sufficient information to be available to determine the errect or customer options, etc., on the supp-y ol electrical energy to essential services.
Appendix 2 + (n) FAA approved Master Minimum Equipment List, where applicable.
(0) Weighing report and associated weight schedule.
+ (P) Manuals required by the DCA:
NO. REQUIRED
i) The FAA approved Flight Manual 2 (but see or Pilot's Operating Handbook. also 4.2 (h)) ii) Airframe Maintenance Manual. 1 iii) Operations Manual. 2 iv) Weight and Balance/Loading Procedures. 1 V) Engine Maintenance Manual. 1 vi) Structural significant items. 1 viil Maintenance planning guide including manufacturers recommended component overhaul lives. 1 viii) Set of Service Bulletins and Service Letters or equivalent documents. 1 NOTE: A condition of Brunei certification of the first of a type is the provision by the Brunei applicant for certification of a continuing amendment service for the required manuals.
(g) Record of compass system and magnetic compass swings.
(r) Record of rigging checks.
(s) A statement that suitable tests and measurements have been made and recorded to establish the satisfactory performance of the installed radio/radar apparatus and their associated antennae.
A list of antennae positions must be provided.
(t) Detailed list of equipment constituting the navigation and communications installation.
+ (u) Noise Type Certificate.