Appendix 2
2.2 - DAC - Departamento de Aviacão Civil (Department of Civil Aviation) The DAC is responsible for the issuance of maintenance, operation and related approvais. The DAC issues ¿Certificados de Aeronavegabilidade (Standard Airworthiness Certificate) and other maintenance and operation certificates in accordance with the "Instrucões de Aviacão Civil" (Instructions for Civil Aviation).
DAC address:
DEPARTAMENTO DE AVIACÃO CIVIL PRACA SENADOR SALGADO FILHO S/N° AEROPORTO SANTOS DUMONT - 4° ANDAR 20021 - RIO DE JANEIRO/RJ
2.3 - DEPV - Directoria de Eletrônica e Protecão ao Voo TElectronics and Fight Protection Directorate) The DEPV is responsible for the Air Traffic Control System.
DEPV address:
DIRETORIA DE ELETRONICA E PROTEÇÃO AO VOO PRACA SENADOR SALGADO FILHO, S/N° AEROPORTO SANTOS DUMONT - 4° ANDAR 20021 - RIO DE JANEIRO/RJ
2.4 - CENIPA - Centro de Investigacão e Prevencão de Acidentes Aeronauticos (Aeronautical Accidents Investigation and Prevention Center) The CENIPA is responsible for accidents investigation.
CENIPA address:
CENTRO DE INVESTIGACÃO E PREVENCÃO DE ACIDENTES AERONAUTICOS ANEXO DO M.AER. 1° ANDAR ESPLANADA DOS MINISTÉRIOS - BLOCO "M" 70045 - BRASILIA/DF 21
Appendix 2
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 import, issued on the basis of a U.S. Type Certificate, following the procedures established in § 4.
3.2 - To be eligible for registration on the Brazilian Registry, an aircratt 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 § 5.
3.3 - Except as provided in paragraph 3.6, to be eligible for installation on Brazilian registered aircraft, any aircraft 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 To be eligible for installation on Brazilian registered aircraft for which a Type Certificate is required, any TSO approved product exported to Brazil, must receive a Brazilian approval for installation issued on the basis of a U.S. TSO approval, following the procedures established in § 7.
3.5 - Other class Il or class Ill 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 § 8.
3.6 - Certain models of aircraft, aircraft engines and propellers which have been exported to Brazil at a time where a Type Certificate for 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 exporter shall obtain a CTA's written statement to this effect.
Appendix 2
4. PROCEDURES FOR ISSUANCE OF IMPORT TYPE CERTIFICATES FOR AIRCRAFT
4.1 - An application Form ADH-300-11 (sample enclosed as Annex I) or an application letter shall be completed by the U.S. manufacturer of the concerned aircraft and forwarded to the CTA through the FAA, together with sufficient engineering information to permit the CTA to become acquainted with the type design.
4.2 - ine text of all FAA speclal conditions, equivalent satety 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 and number of the corresponding substantiation document (report, drawing, specification, etc), shall be made available to the CTA for review and approval.
4.4 - The required markings and placards installed in passenger cabin; in sargo, baggage or stowage compartments and in the aircrart exterior, shall be presented in Portuguese or bilingual (Portuguese and English) for.
The Airplane Flight Manual shall be identified as a 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 aircraft instruments, required markings and placards and tor 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 regiments pete shall bettoucted cough meetings wah thaft 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.
Appendix 2
4.8 - The CTA data needs will be listed in the validation report mentioned in the above paragraph and shall include all published documents (Airplane Flight Manual, Maintenance and Repair Manuals; 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.
The published documents shall be supplied in duplicate, being one copy destinated to the CTA and the other to the DAC. Both Organizations must be included in the manufacturer's mailing list to receive regular up-datings 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;
- 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 for airworthiness certification. Such installations will be reviewed and approved by the CTA during the engineering review mentioned in § 6 above.
4.11 - A Praritate) and "Crespond despecticacao de Aero" ve (Type Certificate Data Sheet) will be issued upon compliance with the requirements established on the validation report referred in § 7 above.
Appendix 2
PROCEDURES FOR ISSUANCE OF IMPORT SUPPLEMENTAL TYPE CERTIFICATES FOR AIRCRAFT
5.1 - An Application Form ADH-300-11 (sample enclosed as Annex I) or an application letter shall be completed by the U.S. holder of the FAA SIC and torwarded to the CIA 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.
5.3 - 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.
5.4 - The required markings and placards installed in passenger cabin; in cargo, baggage or stowage compartments and in the aircrait exterior, shall be presented in Portuguese or bilingual (Portuguese and English) form, unless otherwise prescribed by the CTA.
5.5 - The Airplane Flight Manual Supplement shall be identified as a Brazilian Airplane Flight Manual Supplement and shall include a statement regarding its applicability to Brazilian registered aircraft.
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 for acceptance of the modified aircraft model.
This review shall be conducted through meetings with the holder of the acceptance of the modified aircraft model.
Appendix 2
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;
Illustrated Parts Catalogs; Wiring Diagrams; weight and Balance Manuals; 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 modified afrcraft 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 up-datings of such documents.
5.8 - At least the following documents are also required for each aircraft delivered:
- Up-dated weight and balance report;
- Up-dated wiring diagrams; - Up-dated electrical load analysis; and por nur cat ap campions performed during the
- Production flight test report;
- List of applicable FAA AD's indicating compliance status;
- Summary of maintenance, repairs and alterations performed during the afrcraft life (for used aircraft only).
5.9 - A Brazilian CHST - "Certificado de Homologacão Suplementar de Tipo" (Supplemental Type Certifcate) and corresponding "Adendo" (Addendum) will be issued upon compliance with the requirements established on the validation report referred in § 6 above.
Appendix 2
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) or an application letter 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.
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 cort, shall be made ation to the cia for redrawing specification,
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.
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 up-datings of such documents.
6.6 - A Brazilian CHT - "Certifacado de Homologacão de Tipo" and corresponding "Especificacão de motor ou hēlice" (Type Certificate Data Sheet) will be issued upon compliance with the requirements established on the validation report referred in § 4 above.
Appendix 2
PROCEDURES FOR ISSUANCE OF INSTALLATION APPROVALS FOR TSO APPROVED PRODUCTS
7.1 - An Application Form ADH-300-11 (sample enclosed as Annex I) or an application letter 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;
- One complete collection of all existing published documents such as:
Maintenance and Overhaul Manuals; Parts Catalog; Service Bulletins;
etc as well as a statement from the manufacturer that the CTA address was included in the manufacturer mailing list to receive up-datings of such documents.
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 §§ 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.
Appendix 2
CONTINUING AIRWORTHINESS The U.S. manufacturer of a product which has received a Brazilian design approval according to paragraphs 4 thru 8, shall 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 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 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) n° 1391/01 or the ICAO Annex 16 rules.
10.2 - 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 n° 1391/01 1.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 n° 1391/01 1.e., the modified aircraft 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 sub-part L 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 Annex I Application for Type Ceral ficato, Certificate Centro Técnico Aeroespacial Certificate, Supplemental Type Inst. de Famento e Coord. Ind.
and Attestation of Approved Aeronautical Vico-Direção de Honolugação Product Divisão do Honologaçao
1. Name and address of 2. Application mado for 3. Product involved applicant Type Certification Aircraft
• Production Certification Engine 1 Suppl. Type Certification Prope Her
• Attest. of Approved Aer. Prod. Parts/Components
4. Type Certification:
A. Model Designation (s) (All models listed are to be completely described in the required technical data, including dravings, representing the design, material, specifications, construction, perfomance of the aircraft, aircraft engine, propeller & parts).
S. Production Certification:
A. Factory address B. Application is for: • New P C Certificate n° in force
• Modifications to P C Pattern...
Class..... .......
Date..... ......
C. Applicant is holder of or a licenses inder TC or STC n°..
D. Type of Service (under legislation in force) B. Remarks:
A. If necessary, list the additional details on products or service for which the certification is required.
B. list the documents attached to this application.
ADH-300-11 30
Appendix 2
BRUNEI - SPECIAL REQUIREMENTS (New - October 17, 1985)
1. GENERAL This document specifies the special requirements and conditions to be satisfied for the certification and use in Brunei of aeronautical products of United States origin imported from the United States.
1.2 Authority for aircraft registration and certification is vested in the Department of Civil Aviation (DCA); correspondence should be addressed to :- Department of Civil Aviation, Ministry of Communications, Brunei International Airport, Bandar Seri Begawan, BRUNEI.
1.3 Brunet does not issue Type Certificates.
1.4 Eligibility for the issue of a Bruneian Certificate of Airworthiness is determined by :-
(a) compliance with the appropriate requirements of paragraphs 2, 3 and 4 of this document (but see also paragraph 5).
(b) compliance with :- (†) Additional Directives and Airworthiness Notices issued by the United Kingdom Civil Aviation Authority.
(11) Advisory Notices which may be issued by the DCA from time to time, which are classified as requiring a mandatory action.
NOTE: Compliance with this sub-paragraph (b) is not essential before export to Brunei. However, as it may be difficult to establish conformity in Brunel, details of any relevant service document and modification status will be helpful to the Bruneian user.
(c) Completion of a flight test in accordance with a DCA approved Airworthiness Flight Test Schedule unless otherwise agreed by the DCA.
Appendix 2
2. ELIGIBILITY FOR EXPORT TO BRUNEI
2.1 Class I, II and III products must comply with the requirements of sub-part L of FAR Part 21 and the requirements of this document.
2.2 In addition, aircraft must be eligible for the issue of a standard afrworthiness certificate as prescribed in sub-part H of FAR Part 21 unless otherwise agreed by the DCA.
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 Bruneian certification.
3.2 Additional Requirements for Bruneian certification are not specified for fixed wing aircraft :-
(a) below a maximum authorised weight of 2730 kg (6000 1bs).
below a maximum authorised weight of 5700 kg (12500 lbs) when certification will not be applied for in the Brunei Transport or Aerial Work Categories.
NOTE: Air Navigation legislation in Brunei 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. Equipment required to be carried on flights for the purpose of public transport, to satisfy Bruneiar air naviation legislation, will also be specified.
3.4 Additional Requirements need not necessarily be complied with before the Export Certificate of Airworthiness (FAA Form 8130-4) is issued.
However, if the applicant for certification in Brunei elects to satisfy any or all of the relevant Additional Requirements before che Certificate is issued, the Certificate must be endorsed ir accordance with paragraph 4.4(b) of this document. in such cases the applicant shall notify the DCA to enable details of the Additional Requirements to be provided to the FAA or appropriate designee.