Appendix 2
(b) An FAA Parts Manufacturing Approval (PMA) granted under United States of America, Federal Aviation Regulations Part 21, Subpart K; or
(c) A Technical Standard Order (TSO) authorization granted under United States of America, Federal Aviation Regulations Part 37 Subpart A;
or
(4) In the case of any aircraft component - a document issued by an FAA Certificated Repair Station and which quotes the certificate number issued to that Repair Station under United States of America, Federal Aviation Regulations, Part 145.
NOTE: Class I, II and III are defined in United States of America, Federal Aviation Regulations, Part 21, Subpart L, Section 21.321.
Appendix 2
KINGDOM OF BELGIUM - SPECIAL REQUIREMENTS (Revised January 24, 1979) INTRODUCTION:
This document prescribes requirements supplementing the Agreement on the reciprocal acceptance of export certificates of airworthiness. It is based on the Bilateral Agreement between the Governments of the United States and Belgium of May 14, 1973.
2• GENERAL:
Aircraft and other class I products to be eligible for export to Belgium must, in addition to the requirements prescribed in Part 21, Subpart L of the U.S. Federal Aviation Regulations, be eligible for airworthiness certification in the United States "Standard" classification and comply with the applicable additional requirements under paragraph 4 of this document.
2020 Class Il and III products to be eligible to export to Belgium must comply with the applicable provisions of Part 21, subpart L of the U.S.
Federal Aviation Regulations.
DOCUMENTS AND DATA REQUIRED:
When an aircraft is exported to Belgium, the documents listed below must be provided to the Belgian Civil Aeronautics Administration:
For each individual new aircraft:
The FAA Export Certificate of Airworthiness issued no longer than 60 days before the date the aircraft is entered into Belgium;
The weight and balance report containing a complete inventory of all equipment and instruments;
3. A list of radio communication and navigation equipment installed, including make and model, capacity, frequencies and operating instructions.
4. The FAA approved flight manual. A pilot's operating handbook or similar manual will be provided when no approved flight manual 1s
5. The list of modifications that have been incorporated during production for the airframe, the engine(s), the propeller(s), and the major equipment and components (such as APU).
6. A copy of the manufacturer production flight test report applying to the aircraft being operated.
3.2. For each individual used aircraft:
In addition to the documents listed in paragraph 3.1, the following technical data are required:
Appendix 2 The certified logbooks, or equivalent historical records, ior the aircraft, the engine(s), the propeller(s), the major equipment and components (such as APU), containing information on operational times and cycles (since new and since last overhaul), maintenance, overhaul, repairs and modifications, status of parts with limited lifetime.
A detailed listing of all modifications, including the operator's modifications Service Bulletins or equivalent documents, and Airworthiness Directives complied with;
3. The past maintenance schedule and programs;
The components operating and storage limits.
3.3. For aircraft first of the type exported to Belgium:
In addition to the documents listed in paragraphs 3.1. and 3.2., the following technical data are required:
1. One copy of the Type Certificates and Type Certificate Data Sheets for the aircraft, the engine(s) and the propeller(s);
2. Iwo copies of the FAA approved flight manual, or the pilot's operating handbook when no flight manual is required by the FAA.
3. One complete set of current technical manuals for the aircraft operation, service, maintenance, overhaul and repair manuals, catalog of spare parts.
4. Same technical manuals as in 3 above for the engines(s) and the propeller (s), if they are of a model exported to Belgium for the first time;
5. A list of the necessary special tools and equipment (including a tolerance chart) essential to the inspection and servicing of the aircraft, the engine(s), the propeller(s) and associated equipment;
6. Information or instructions essential to the assembly and rigging of the aircraft;
7. A statement by the manufacturer, or its authorized representative, to the effect that all pertinent information, modification, services bulletins, and revisions of such bulletins and manuals will be automatically distributed to the Aeronautics Administration of Belgium, to guarantee the airworthiness of the aircraft, the engine(s), the propeller(s), and the major components.
8. A copy of the type flight test report. Flight characteristics of the aircraft shall be described in this report in a manner convenient for calculating the performance of the aircraft over a reasonable range of weights, altitudes, and atmospheric conditions.
Performance figures contained in, or furnished with the type flight test report shall have been corrected to standard atmospheric conditions, and a statement to this effect shall be made a part of the report. Established operational limitations, speeds, and approved loads shall be indicated.
9. Three-view drawings of the major assemblies, installations, and primary structure.
Appendix 2
10. A type record of stress analysis summary showing, for all members of the primary structure, their design loads, dimensions, materials, strength, and margins of safety, or a copy of the static strength test reports when type approval was granted on the basis of such tests.
ll. The list of reports and notes prepared for U.S. type certification of the aircraft.
4• SPECIAL TECHNICAL REQUIREMENTS:
Noise limits:
An aircraft will be eligible for a Certificate of Airworthiness only if it complies with the noise standards of ICAO Annex 16. Subsonic jet airplanes for which application for U.S. type certification was carried out before 6 October 1977 have to comply with the noise limits laid down in chapter 2 of Annex 16, regardless of their date of manufacture.
4.20 Radio equipment:
Radio equipment must be FAA approved and comply with TSO/FAA TC specifications. When a radio equipment model is exported to Belgium for the first time, one copy of the following documentation will be furnished:
- the manufacturer's statment of conformance submitted to FAA
- the letter of acceptance issued by FAA
- the technical manuals and bulletins (Service Bulletins, etc.)
Special technical requirements regarding the radio equipment are:
- VHF radio-communication equipment must be compatible for use with 25 kHz spacing between channels;
- VHF radio-navigation equipment must be compatible for use with 50 kHz spacing between VOR and LOC channels and 150 kHz between associated Glide Slope channels.
- communication and navigation antennas are to be distinct;
- VOR/LOC and Glide Slope antennas are to be distinct.
4.3• Flight instruments:
- Air Speed Indicators must show airspeed in KNOTS only.
- Altimeters must be of the sensitive type, showing altitude in FEET, with adjustable setting in MILLIBAR scale.
Flight data recorder and cockpit voice recorder:
Turbine powered transport category airplanes of a maximum weight of over 5,700 kg must be equipped with an approved flight data recorder. When the maximum weight is over 27,000 kg, an approved cockpit voice recorder is also required. The technical manuals and the last calibration charts pertinent to the installed recorders will be furnished.
Appendix 2
5. NOTES:
5.1. The aircraft must be equipped in accordance with the requirements of the Belgian regulations for its intended use.
5.2. Complementary information may be obtained at:
Administration de l'Aeronautique Direction Technique rue de la Fusee, 90 B - 1130 BRUSSELS (BELGIUM).
TELEX : 22715 DGAIR B.
Appendix 2
REPUBLIC OF BOLIVIA - SPECIAL REQUIREMENTS (New - Auguet 13, 1976)
1. Bolivian Special Requirements are applicable to the import of aeronautical products. The requirements are in accord with the procedural requirements for the issue of U.S. Export Airworthiness Approvals under Federal Aviation Regulations (FAR) Part 21, Subpart L.
2. The Director General of Civil Aviation requests that the FAA issue export airworthiness approvals applicable to Class I, Il and Ill aeronautical products being exported to Bolivia. Eligibility for importing aeronautical products into Bolivia, in addition to the provisions or subpart i of Part 2l of the Federal Aviation Regulations, must comply with applicable special requirements prescribed below:
All aircraft exported to Bolivia via flyaway should display Bolivian nationality and registration marks and carry the following documents on the delivery flight:
(1) Bill of Sale;
(2) Bolivian Certificate of Registration;
(3) Bolivian authorization for the delivery flight;
(4) Export Certificate of Airworthiness;
(5) Notification of the Aircraft having been canceled from the U.S.
aircraft registry;
(6) Authority to cover the use of the installed communication equipment for the duration of the delivery flight; and
(7) Approved airplane flight manual, maintenance and operation manuals, logbooks and such documents essential to the safe operation of the aircraft including loading charts.
b. Types and models of aircraft which have been exported to Bolivia previously, shall have the following additional documents and data delivered to the purchaser:
(1) Maintenance, overhaul and repair manuals, including maintenance/inspection schedule;
(2) Airworthiness Directives (AD) and Type Certificate Data Sheets or specifictions and manufacturer service bulletins applicable to the aircraft;
1/15/80 AC 21~2D Appendix 2
(3) List of inventory of equipment installed by make, model, and serial number.
(4) Historical records of aircraft, engine(s), propeller(s) and time or life controlled items.
(5) Weight and balance report, including a loading schedule or chart.
(6) Engine(s) must not have operated in excess of 500 hours and propellers(s) 1,000 hours since new or approved overhaul.
(7) Afrcraft and FAA time controlled components must not have operated in excess of 50% of whichever 1s the lesser of the FAA approved or manufacturer recommended overhaul times.
(8) Shall have installed and functional a minimum of:
Single Engine Aircraft:
1-VOR/ILS, 1-ADF, 1-HF, 1-VHF, 1-DME, 1-ELT, 1 altimeter calibrated in inches and millibars.
c. An aircraft being the first of its type and model exported to Bolivia, shall in addition to the above, furnish to the purchaser and to the Director General of Civil Aviation the following documents:
(1) Parts catalog for the aircraft, engine, propellers and inatalled major auxiliary equipment.
(2) Instructions or information essential to the asembly and rigging of the aircraft is to be assembled at the point of destination.
(3) List of special tools, equipment and tolerance charts essential to the servicing and maintenance of the aircraft, engines, propeller and major auxiliary units or components.
(4) General arrangement and three-view drawing of the aircraft.
Appendix 2
REPUBLIC OF BOTSWANA - SPECIAL REQUIREMENTS (New - Apr11 19, 1978) 1• GENERAL a • Any aircraft to be eligible for the issue of a Certificate of Airworthiness by the Government of the Republic of Botswana must qualify for certification in the United States of America in the Standard or Restricted Category and an Export Certificate of Airworthiness, FAA Form 8130-4, should have been 1ssued in accordance with Part 21 of the United States Federal Aviation Regulations.
b. Class II and Class III products should be accompanied by documentation which confirms that the item is in accordance with the relevant Section of Part 21 of the United States Federal Aviation Regulations. An Airworthiness Approval Tag, FAA Form 8130-3 1s acceptable.
If the aircraft is to be entered on the Botswana Register of Civil Aircraft, the importer must make application to the Botswana Department of Civil Aviation for the necessary Certificate of Registration, Permit to Fly, and Radio Station License which must be carried during the delivery flight.
d. Inquiries should be addressed to the Director of Civil Aviation, P.O. Box 250, Gaborone, Botswana, marked to the attention of the Chief Flight Safety Engineer.
2. First Aircraft of type to be Registered in the Republic of Botswana
a. The following documents and data are required:
(1) A complete set of maintenance, overhaul, and repair manuals, and parts catalogs for:
(1) Airplane
(11) Engine(s)
(111) Propeller(s)
(iv) Any equipment not previously imported to the Republic of Botswana.
(2) A full set of service bulletine, instructions, letters, nodification leatlets, etc., issued by the manufacturer with respect to the airframe, engine(s), propeller(s), and installed equipment.
(3) A statement confirming that any amendments or new issues of the above manuals and catalogs will be forwarded to the Department of Civil Aviation as they are issued.
Appendix 2
(4) A copy of the Type Certificate Data Sheet or Aircraft Specification unless this is already held by the Department of Civil Aviation.
(5) Three (3) identical copies of the Flight Manual for the aircraft, including a copy allocated to the specific aircraft.
Each Aircraft for which a Botswana Certificate of Airworthiness is to be requested.
a. A statement must be signed by a manufacturer's representative to the effect that all mandatory modifications have been embodied, that al!
Airworthiness Directives have been complied with, and that any special inspections required have been complied with.
b. An Export Certificate of Airworthiness, FAA Form 8130-4.
c. Two (2) copies of the Flight Manual including a copy allocated to the specific aircraft.
d. A statement confirming that all amendments to the Flight Manual (s) will be forwarded to the Department of Civil Aviation as they are issued.
e. Two (2) copies of the Weight and Balance information for the specific aircraft.
f. Two (2) copies of the Equipment List for the specific aircraft, marked to show the installed equipment.
Appendix 2
FEDERATIVE REPUBLIC OF BRAZIL - SPECIAL REQUIREMENTS
1. To be eligible for registration and airworthiness certification by the Government of Brazil, Class I, II, and III products will be processed in accordance with the instructions contained in paragraphs a., b., and c.
below.
a. The manufacturer or supplier must hold or obtain one or more of the following FAA approvals, unless otherwise approved by a Brazilian governmental agency, e.g., Brazilian Air Force, etc.:
(1) A current valid FAA production certificate for the product involved, as outlined in Federal Aviation Regulations Part 21.
(2) An FAA Approved Production Inspection System (FAA-APIS), as provided in Federal Aviation Regulations, Part 21, Subpart F.
(3) An FAA replacement and modification parts manufacturer approval (FAA-PMA) as provided in Federal Aviation Regulations Part 21, Subpart K.
in this case, parts, containers, and invoices will be evidence of the manufacturer's name, address, the part number registered trademark, when described in FAA approval letter, and the symbol "FAA-PMA."
(4) Technical Standard Order (TSO) letter of acceptance, or authorization issued by the FAA per Federal Aviation Regulations Part 37.
b. Reconditioned, used, or surplus parts, must be accompanied by a certifcation statement signed by an FAA certified repair station holding a currently valid certificate, or by a certified aircraft and powerplant mechanic, as provided for under FAR Parts 145 and 65, respectively. The return to service maintenance records required by Federal Aviation Regulations 43 shall accompany the parts.
NOTE: The provisions of the above paragraphs are not applicable to standard parts (such as nuts and bolts) conforming to established industry or Government specifications, e.g., Standard Aircraft Equipment (SAE), and Military Specifications (MIL Spec.).
c. In all instances, suppliers must certify on the face of their above procedures; 1.e., FAA PC N°; SAR No. - invoice that the product involved was manufactured under one or more of the _; FAA-APIS letter dated ; FAA PMA letter dated _; ISO No. ; MIL Spec. _; other Government or Industry Specifications 20
Appendix 2
DOMINION OF CANADA - SPECIAL REQUIREMENTS (Revised February 7, 1979)
1. Aircraft and aeronautical products, to be eligible for export to Canada, must in addition to requirements prescribed in Part 21 of the United States requirements prescribed below. It should be noted that the Canadian Department of Transport (DOT) will accept for certification in Canada only those aircraft which are eligible for U.S. certification as "standard" aircraft and have been manufactured in the United States under a Type Certificate currently issued in accordance with FAR 21.21. This excludes "restricted", "limited", and "experimental" aircraft, which will require a суре validation inspection by Department of Transport in accordance with Part I, Chapter II, Section 2.10.2.4 of the Engineering and Inspection Manual. Persons wishing to export transport category sircraft to Canada shall contact the DOT for policies and procedures governing such export.
An export certificate of airworthiness will be required by the DOT for all Class I products exported from the U.S. to Canada, except for used U.S. manufactured aircraft imported under the Inspect, Test, Repair as Necessary (ITRAN) procedure (see Note following paragraph c). Class II and Class III products exported to Canada will be processed in accordance with the provisions contained in FAR Part 21, Subpart L.
b. An aircraft exported to Canada, except as indicated in paragraph c below, shall not have been flown for any purpose other than that required to accomplish the manufacturer's production flight test, flight tests for modifications, crew training flights for Canadian purchaser, and such time as may be involved in effecting delivery.
c. Used aircraft may be exported to Canada, provided that such aircraft comply with the export certification requirements in FAR Part 21, are certificated in the "standard classification", and are accompanied by records or logbooks applying to the aircraft and engine(s).
NOTE: Used aircraft exported from the United States without an Export Certificate of Airworthiness are eligible for a Canadian Certificate of Airworthiness when the ITRAN requirements of Part I, Chapter II, Section 2.9, of the Canadian Department of Transport Engineering and Inspection Manual have been complied with.
d. Ski and ski installations must be designed to meet the requirements of the DOT Engineering and Inspection Manual Part II, Chapter I, Sections
1.1.39 and 1.1.40.
Appendix 2
e. When the first aircraft of a type is exported to Canada, the exporter is required to provide the Canadian Department of Transport at no charge, seven copies of the Flight Manual, Maintenance Manual, Structural when a at shy sode copter of the Repair Manual, Illustrated Parts Catalog, and Service Bulletins and subsequent amendments thereto. When a model!/of an aircraft type previously registered in Canada is exported to Canada, seven copies of the new Manuals or appropriate amendments and Service Bulletins must be provided. In the case of transport category aircraft, the required number of copies of manuals may be negotiated with the Canadian Department of Transport when the aircraft are exported to Canada.
f. United States exporters of aircraft and aeronautical products manufactured in a country other than the United States should contact the Department of Transport for certification policies and procedures.
2. To facilitate the licensing of aircraft, the following documentation should be forwarded to the Regional Administrator of the Region in which the purchaser resides (address of the six Regional Offices of the Canadian Department of Transport may be found in paragraph 4):
a. Export Certificate of Airworthiness;
b. Evidence of transfer of ownership to the Canadian purchaser from the last U.S. recorded owner, or the manufacturer in the case of a new aircraft; and,
c. The appropriate Canadian Regional Administrator should be informed by telegram or telex of the issuance of an Export Certificate of Airworthiness for an aircraft being exported via flyaway to Canada.
(1) The following is an example of the telegram referred to above:
Regional Administrator Canadian Air Transportation Administration Transport of Canada 739 West Hastings Street Vancouver, British Columbia V6C 1A2
Export Certificate of Airworthiness E-covering
(Make and Model of Afrcraft) 1/ When in doubt as to whether an aircraft 1s the first of a model, contact the Department of Transport, Ottawa, Ontario, Canada, KIA ON8.