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(c) In both cases (a) and (b) the aircraft is flown to Sweden on its foreign documents. It rests with the applicant to make sure that the aircraft is type accepted in Sweden.
(5) Documents concerning determination of weight and center of gravity, including list of basic equipment, weighing record with calculation of basic empty weight and, when applicable, loading schedule for the aircraft.
(6) Report on flight test with aircraft after production or preparation for delivery according to decision by the Board in each particular case.
(7) Statement of technical state of the aircraft at the time of export including engine(s), propeller(s), and other equipment of the aircraft. The statement shall include as applicable:
(a) Alterations carried out in accordance with AD notes, also major alterations introduced for other reasons and major repairs performed.
(b) The latest basic overhaul performed, or other extensive procedures of the type of overhaul.
(c) Time since latest major periodical maintenance procedure, total run if basic overhaul was not performed, and time since basic overhaul if performed, and - if possible - total run.
(NOTE: For aircraft that has been maintained in compliance with a specially approved maintenance system item (c) above implies a requirement for information of where the aircraft and its components are situated time-wise in the time schedule of the system at the time of acceptance examination.)
(d) Longest runs permitted (safe life) that have been prescribed to apply in the aircraft and the total runs of the components concerned.
(e) Measures taken for the preservation of the aircraft in storage and transport.
(8) Specification of the equipment of the aircraft for communication and navigation, etc.
d. Ferry Flight
(1) Documents to be available for a ferry flight include:
(a) Export Certificate of Airworthiness.
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(b) Temporary Nationality and Registration Certificate in accordance with BCL-M 1.2.
(c) Authorization for ferry flight, stating conditions.
(d) Journey log book, unless other acceptable log document 1a already available.
(NOTE: Items (b) and (c) and in some cases also (d) are 1ssued by the Board).
(2) In addition to the documents indicated in para. d.(1) the following documents shall be carried on board at the ferry flight.
(a) Flight Manual as stated in para. 3.a.(7), valid for the individual aircraft.
(b) The Manufacturer's Instruction Manual as stated in para. 3.a. (8).
(c) Weight and balance documents.
(d) Documents concerning extra equipment installed, as stated in para. d. (3) below.
(NOTE: When flight for special purpose, e.g. training, within the U.S.A. has been permitted in the authorization for ferry flight a special permit issued by the FAA may be required for such flight.)
(3) When an aircraft has been provided with special equipment for ferry flight from the place of delivery to a place in Sweden (such as extra fuel tanks), a statement regarding the approval of the installation shall be available and, in addition, appropriate instructions for handling the equipment. The installation of the mentioned equipment shall comply with the FAA requirements.
(4) The last maintenance inspection or corresponding procedures performed before the ferry flight shall, when appropriate, be performed by the manufacturer or by an FAA approved repair station, or by a maintenance engineer duly licensed by the FAA.
(5) When the Ferry Flight Permit includes permission for flight training the responsibility for the maintenance shall be defined.
(6) At ferry flight the aircraft shall be marked with the assigned nationality and registration marks.
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4. EXPORT - FLYAWAY AIRCRAFT
a. In addition to the requirements prescribed in Part 21 of the United States Federal Aviation Regulations, an aircraft, to be eligible for export to Sweden via flyaway, must be issued a Swedish interim Certificate of Registration and a Swedish temporary Certificate of Airworthiness.
b. These certificates will be carried in the aircraft during the delivery, flight from the United States exporter's base to Sweden. In such cases, however, the following is required:
(1) Title to the aircraft shall have been transferred to the Swedish purchaser.
(2) Swedish registration and nationality markings shall be properly displayed on the aircraft.
(3) An Export Certificate of Airworthiness, FAA Form 8130-4, shall be issued to cover the aircraft concerned.
c. The above Swedish certificates will be 1ssued by the Swedish Royal Board of Civil Aviation, Civilair, Sweden, to the Swedish purchaser for forwarding to the flight crew who is making the delivery flight.
5. ENGINE AND PROPELLER (not installed in aircraft). At the import of aircraft engine and propeller the following docuents shall be submitted:
a. Jype Documents, Engine and Propeller not previously type accepted in Sweden.
(1) Type Certificate and Type Certificate Data Sheet, issued by the FAA, or other equivalent documents.
(2) Instruction Manual (Operation Manual, Owner's Manual, etc).
(3) Maintenance Manual or equivalent document issued by the manufacturer
(4) Declaration regarding information service, i.e., a statement issued by the manufacturer of engine or propeller to the effect that he undertakes to provide the Board, without charge, with information in the form of service bulletins or equivalent concerning alterations or other actions recommended by the manufacturer for continued airworthiness of the product, and also amendments to the Maintenance Manual as indicated in para's 5.a. (2) and 5.a.(3).
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b. Documents, Engines and Propellers previously type accepted in Sweden (See note to 3.a).
(1) Type documents are to be submitted to the Board only if the Board finds additional documentation necessary.
c. Individual Documents. For separately imported aircraft, engine or propeller the following individual documents shall follow the product as base for documentation in connection with installation of the product in an aircraft.
(1) Export Certificate of Airworthiness or other document according to the FAA regulations, equivalent to such certificate. The certificate shall contain information sufficient for the identification of the product.
(2) Statement in accordance with FAA regulations of the technical state of the engine or propeller in question at the time of import. The statements shall in appropriate parts comply with the requirements of para. c.7.
6. AERONAUTICAL PRODUCTS NOT COVERED BY PARA'S 3 AND 4 In the case of separate export of components and parts of aircraft - other than aircraft engines and propellers - intended for aircraft which is entered on the Swedish register and alternative or special equipment intended for such aircraft which is not normally included in the type approval of aircraft, regulations to be applied are those contained in FAR, Part 21, Subpart La 109
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CONFEDERATION OF SWITZERLAND - SPECIAL REQUIREMENTS
1. In addition to the special requirements outlined below, all Class I II, and III products should be exported in accordance with the applicable provisions of Part 21 of the United States Federal Aviation Regulations, in order to be eligible for certification by the Government of Switzerland. Export Certificates of Airworthiness and other related data should be forwarded to the foreign purchaser, inasmuch as the air authority of the Government of Switzerland requires that the applicant (the foreign purchaser) shall submit to that government such substantiating evidence as may be necessary to establish airworthiness and eligibility for registration and certification by that government.
2. In addition to the foregoing, applicable parts of the following special requirements prescribed by Switzerland will be complied with when exporting aircraft:
a. If the aircraft is the first l/ of a model exported to Switzerland, the following material shall be furnished with new aircraft:
(1) 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, and a statement to this effect shall be made a part of the report. Established operational limitations, speeds, and approved loads shall be indicated.
(2) A copy of the manufacturer's production flight test report applying to the aircraft concerned, including a copy of the flight checkoff form utilized with respect to the testing of the aircraft.
(3) Three-view drawings of the major assemblies, installations, and primary structure.
(4) A type record or 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.
(5) A certified copy of the complete drawing list (quoting latest issue numbers issued by the manufacturer).
(6) A statement by an authorized representative of the manufacturer to the effect that all pertinent information, modification service bulletins will be automatically distributed to the technical section of the air authority of the government of the country of destination.
1/ When in doubt as to whether an aircraft is the first of a model, contact the air authority of the importing country.
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(7) A catalog of spare parts relating to the aircraft, aircraft engine(s), propeller(s), and major auxiliary equipment installed.
(8) Three copies each of operating, maintenance, overhaul, and repair manuals applying to the aircraft, engine, propeller, or to equipment installed on the aircraft.
(9) A list of the necessary special tools and equipment (including a tolerance chart) essential to the inspection and servicing of the aircraft, engines, propellers, and associated equipment. This should include inspection timetables, a chart of the lubricating system, and appropriate instructions relating to the fuel systems.
(10) Three copies of information or instructions essential to the assembly and rigging of the aircraft.
(l1) A list (in triplicate) of communications equipment installed, including model, capacity, frequency, operating instructions, etc.
b. In case an aircraft of the same model previously has been exported to and certificated in Switzerland, the following documents or material shall be furnished by the exporter or by the government of the country of origin.
(1) The Export Certificate of Airworthiness shall list the propeller serial numbers, as well as the engine serial numbers.
(2) Three copies each of operating, maintenance, overhaul, and repair manuals or other related information, as provided for in 2a(8).
3. A l1st of communications equipment installed, including model, capacity, frequency, operating instructions, etc.
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SYRIAN ARAB REPUBLIC - SPECIAL REQUIREMENTS (New - August 23, 1977)
1. Syrian requirements for U.S. civil air equipment.
a. There are no Syrian government requirements for modifications on U.S. manufactured aircraft into Syria. Syrian government agencies are only importers and users of aircraft.
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REPUBLIC OF TUNISIA - SPECIAL REQUIREMENTS (New - August 17, 1977)
1. Import of U.S. Manufactured Aircraft.
a. The Republic of Tunisia accepts for import and registration, with modification, U.S. aircraft manufactured to Federal Aviation Administration (FAA) standards.
1/15/80 AC 21-2D Appendix 2
UNITED KINGDOM- SPECIAL REQUIREMENTS SECTION 1 - INTRODUCTION A new bilateral agreement between the United Kingdom (U.K.) and the United States (U.S.) came into effect by the Exchange of Notes in December 1972 and superseded the Exchange of Notes of 1934 relating to the reciprocal acceptance of aeronautical products. The manner in which this agreement will be implemented is described below.
A. Administration and Procedures.
(1) The procedures which must be followed to obtain U.K. certification are dealt with in the current 1ssue of Section A of British Civil Airworthiness Requirements (BCAR) which also prescribes the documents which must be supplied for prototype and series aircraft.
(2) An Export Certificate of Airworthiness (or agreed alternative) with pertinent data attached will be required in connection with any Class I product and engine modules exported from the U.S. to the U.K.
Class II and Class III products to be eligible for installation on certificated civil aircraft registered in the UK. nust be processed in accordance with the applicable provisions of Part 21 of the United States Federal Aviation Regulations.
(3) Where the issue of an Export Certificate of Airworthiness is relevant, it shall be accompanied by a document (e.g., aircraft logbook), furnished by the applicant, which contains entries identifying those applicable FAA Airworthiness Directives (AD) and UK-CAA Additional Directives (CAA-AD) with which compliance has been achieved. This document shall also identify those AD's and CAA-AD's containing repetitive compliance requirements (e.g., inspection requirements for a particular component at 50-hour intervals) and when next compliance 16 due to be satisfied. All AD's and CAA-AD's must have been complied with prior to the issuance of the U.S. Export Certificate of Airworthiness unless is also responsible for satisfying all other U.K. Special Requirements (identified in Section 2 of this Appendix), as appropriate, for the particular product being exported to the U.K. and all applicable requirements of FAR 21, Subpart L, before the U.S. Export Certificate of
(5) British documents providing information on the procedures and requirements for U.K. acceptance of U.S. products are on file in each FAA Regional Office and are available for review by the exporter.
Appendix 2 B. Acceptance of Aircraft.
(1) In accordance with paragraph 4 of the U.K./U.S. bilateral agreement, the U.K. will require to become conversant with the design of all fixed-wing aircraft in excess of 2,730 kg (6,000 1bs.) weight intended for use in the U.K. Transport Category, the design of all aircraft exceeding 5,700 kg (12,500 1bs.) regardless of the intended certification category, and all rotorcraft offered for U•k. certification. Additionally, in accordance with the policy declared in CAA Airworthiness Notice No. 15, the CAA may require to evaluate certain aircraft of less than 5700 kg.
weight which have unusual design features. The CAA may then issue Special Conditions to cover certain features which would otherwise not meet the standards which are implicit in BCAR and the U.K. Air Navigation Order.
(2) Once the U.K. standard for certification has been determined and, where necessary, U.K. Special Conditions have been published, the U.K. will, in accordance with paragraph 9(h)(11) of the U.K./U.S.
bilateral agreement, accept aircraft and rotorcraft to this standard and U.K. Special Conditions, as applicable, together with the applicable AD's and U.K. equivalent retrospective requirements, while they continue in production, Modifications to the aircraft may also be made, provided the requirements used as the basis of U.K. certification are complied with, or alternatively, that the CAA agree that the modifications are acceptable
(3) For aircraft which are no longer in production, the CAA reserves the right to modify the basis of U.K. certification, or to refuse certification in accordance with paragraph 9(h)(111) of the U.K./U.S.
bilateral agreement. Where U.K. certification of such aircraft is sought, reference should be made to the Civil Aviation Authority who will advise the position pertaining at that time.
C. Acceptance of Engine, Auxiliary Power Units and Propellers.
(1) In accordance with paragraph 4 of the U.K./U.S. bilateral agreement a preliminary investigation may be required to establish the standard offered for U.K. certification and, where necessary, any Special Conditions the CAA may wish to apply. In the case of turbine engines for aeroplanes, the Special Condition requirements will be limited to those arising from unorthodox design features in accordance with the U.K./U.S.
reciprocal acceptance agreement.
(2) When compliance with the U.K. standard for certification has been established, the U.K. will accept engines (including engine modules), auxiliary power units, and propellers and parts therefore to the defined standard while they continue to be in production subject only to compliance with subsequent applicable AD's and U.K. equivalent retrospective requirements. Modifications will also be accepted subject to compliance with the U.K. certification basis.
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(3) For engines, auxiliary power units, and propellers which are no longer in production, the CAA reserves the right, in accordance with paragraph 9(h) (111) of the U.K./U.S. bilateral agreement, to modify the basis of acceptance or to refuse certification.
D. Acceptance of Appliances and Components.
(1) Radio The procedures which must be followed to obtain U.K. acceptance of radio equipment are dealt with in the current issue of Section A, Chapter A3-4, of the BCAR.
(2) Appliances (other than Radio) Those appliances (other than radio) as so defined in Section 3 must be registered to obtain U.K. acceptance. The procedures which must be followed to obtain acceptance of such appliances are dealt with in Section A, Chapter A3-3, of BCAR. An acceptable method of complying with these procedures is contained in Section 3.
(3) Components Components which are produced in the U.S. for export and used on products which are or may be certificated or approved in the U.K. will be accepted by the CAA provided:
(1) They are properly designated, and
(11) The FAA or its designee certifies that the components conform to the applicable design data and meet the applicable test and quality control requirements which have been notified by the CAA to the FAA. NOTE: These provisions apply to those components which are These providens. pursuant to a produced by a manufacturer in the U.S. pursuant to an agreement between the manufacturer and the product manufacturer in the U.K.
E. Restricted Category Aircraft.
(1) Applications for U.K. certification of aircraft certificated in the U.S. in a restricted category will be considered on an individual basis.
(2) The applicant for export certification must furnish to the CAA, information describing how the aircraft differs from the type certification basis for a standard certificate - if standard certification of the type design has been made. The applicant shall provide evidence of compliance with this requirement, to the FAA or its designee, at the time of issue of the export certificate. If the applicant does not have some form of approval under the FAR, the FAA will verify the correctness of this information and will so notify CAA by the appropriate means.
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(3) On the basis of this evidence, the CAA will decide whether it invoked.