AC 21-2B Appendix 2 10/2/69 Page 53
SINGAPORE, REPUBLIC OF - SPECIAL REQUIREMENTS
1. To be eligible for export to the Republic of Singapore, an aircraft must meet the requirements prescribed in Federal Aviation Regulations Part 21, Subpart L.
2. The applicant for certification of the aircraft in the Republic of Singapore must provide the following documents to the Director of Civil Aviation, Department of Civil Aviation, Singapore Airport, Singapore 19, Republic of Singapore.
a. For each aircraft:
(1) F.A.A, Export Certificate of Airworthiness.
NOTE: It will be necessary for this to be supplied in advance of the aircraft delivery date, so that the Singapore Certificate of Validation may be issued and accompany the aircraft during training flying and delivery flight.
(2) Weight and balance report.
(3) Equipment List.
(4) Modification statement and List of F.A.A. Airworthiness Directives complied with.
(5) Copy of Production Flight Test Report related to the specific aircraft.
b. For each model aircraft, one copy of:
(1) F.A.A. approved flight manual.
(2) Weight and balance manual.
(3) Operating manual,
(4) Maintenance Planning Data,
(5) Maintenance Manual (Airframe).
(6) Maintenance Manual (Engine).
(7) Overhaul Manual (Airframe).
(8) Overhaul Manual (Engine).
Appendix 2 AC 21-2B Page 54 10/2/69
(9) Structural Repair Manual.
(10) Complete set of Service Bulletins (Airframe).
(11) Complete set of Service Bulletins (Engine).
(12) F.A.A. Aircraft Data Sheet.
(13) F.A.A. Engine Data Sheet.
c. Amendment service for the above documents must be provided as applicable.
AC 21-2B Appendix 2 10/2/69 Page 55
REPUBLIC OF SOUTH AFRICA - SPECIAL REQUIREMENTS
1. An aircraft or any other Class I product, to be eligible for registration and airworthiness certification by the Government of the Republic of South Africa, must be eligible for certification in the United States standard or restricted category and should be covered by an Export Certificate of Airworthiness, FAA Form 8130-4, in accordance with Part 21 of the United States Federal Aviation Regulations. Class II and Class III products, to be eligible for approval and installation on certificated civil aircraft of South African registry, should be exported in accordance with the applicable provisions of Part 21 of the United States Federal Aviation Regulations.
2. When the aircraft is the first of the type or model to be imported into South Africa, the importer will advise the exporter of this fact and the exporter is to supply the Secretary for Transport, Department of Transport, Private Bag 193, Pretoria, Republic of South Africa, with the information and data material as shown below:
(a) A set of maintenance, overhaul, parts, repair and operations manuals issued by the munufacturers of the aircraft, its engine (s), propeller (s) and installed equipment and containing such information as is necessary to assemble, maintain, overhaul, repair and operate the aircrait, its engine(s), propeller (s), and installed equipment.
(b) A set of all current service bulletins, service letters and modification bulletins, issued in respect of the aircraft, its engine(s), propeller(s) and installed equipment and written confirmation from the manufacturer of the aircraft that, as and when they are issued, he will supply the Secretary for Transport with copies of amendments to and new issues or revisions of the publications referred to in this and the preceding subparagraph;
(c) A three-view general arrangement drawing of the aircraft;
(d) A type certificate data sheet or cquivalent document;
(e) The approved flight tual or an equivalent document;
and
(f) A copy of the manufacturer's production flight test report for the aircraft being exported.
3. The exporter must supply the following documents in respect of every aircraft for which a South African Certificate of Airworthiness is desired:
(a) A certified statement issued by the manufacturer, indicating that all mandatory modifications and special inspections have been complied with;
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(b) A copy of the aircraft weight and balance report and equipment list showing the weights and arms of the main components and installed equipment; and
(c) An approved flight manual or equivalent document.
AC 21-2B Appendix 2 10/2/69 Page 57
SWEDEN - SPECIAL REQUIREMENTS
1. 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.
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:
a. Title to the aircraft shall have been transferred to the Swedish purchaser.
b. Swedish registration and nationality markings shall be properly displayed on the aircraft.
c. An Export Certificate of Airworthiness, FAA Form 8130-4, shall be issued to cover the aircraft concerned.
2. The above Swedish certificates will be issued by the Swedish Royal Board of Civil Aviation to the Swedish purchaser for forwarding to the flight crew who is making the delivery flight.
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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 substan- s erection vy tiating 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- 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 When in doubt the air authority of the inportingcrain is the first of a model, contact importing country.
AC 21-2B Appendix 2 10/2/69 Page 59 service bulletins, and revisions to such bulletins will be automatically distributed to the technical section of the air authority of the Government of the country of destination.
(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 aircrait, engines, propellers, and associatedequipment.
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.
(11) 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 list of communications equipment installed, including model, capacity, frequency, operating instructions, etc.
Appendix 2 AC 21-2B Page 60 10/2/69
UNITED KINGDOM - SPECIAL REQUIREMENTS
1. The special conditions associated with the Exchange of Notes, Treaty series No. J8 (1934) relating to the reciprocal validatlon of export certificates of airworthinessl/ which came into effect on the Ist July 1956 have been shown by experience to be in need of revision, and the amended version below is effective as from lst November 1960.
a. Types of Aircraft, the United States Export Certificates of Airworthiness of which were validated by the United Kingdom prior to the 1st November 1960.
(1) Certain types of aircraft designed and constructed in the United States and issued with an export certificate of airworthiness prior to 1st November 1960 may continue to be imported on a similar basis to that agreed for previous aircraft of the identical type.
(2) This condition will not be invalidated by minor changes to the aircraft which do not reduce the previously accepted airworthiness standard.
(3) The main types of aircraft referred to in paragraph (1) are as follows:
Boeing 377 Boeing 707-436 Douglas DC.3-C47 Series Douglas DC,4 C54A-DC, C54B-DC, C54D-DC Douglas Douglas DC.6A Douglas DC.6B Douglas DC.7C Lockheed Constellation Type 049 and 749
(4) Additional information on performance, however, wlil be required in respect oi certain of the above-mentioned aircraft certificated against Part 25 of the Federal Aviation Regulations in order that they may be operated in accordance with the United Kingdom Air Navigation Order 1960. The schedule of additional information required will be made available by the Air Registration Board on request.
b. Special Conditions for Conventional Fixed-Wing Aeroplanes intended for Public Transport. Aeroplanes in either the transport, normal, utility, or acrobatic categories may have their export certificate 1/ British documents necessary to determine compliance with U.K. Special Ceview by the xpofilf in each FAA Regional Office and are available for
AC 21-2B Appendix 2 10/2/69 Page 61 of airworthiness validated subject to compliance with the following conditions:
(1) Compliance shall be established with the performance and any directly associated handling requirements of the British Civil Airworthiness Requirements, Section D, appropriate to the relevant performance group and current at the date of application for validation.
(2) The information on the performance and the handling shall be scheduled in the flight manual in accordance with the British Civil Airworthiness Requirements, current at the date of application for validation.
(3) The aeroplane shail be equipped, or shail be capable of being equipped, for the conditions under which it is intended to be operated and in accordance with the requirements of the United Kingdom Air Navigation Order current at the date of validation.
(4) The radio installation shall comply with the appropriate United Kingdom legislation,
(5) The aeroplane shall, to the extent deemed essential by the Air Registration Board, comply with such additional requirements as may be specified in writing. These additional requirements will be determined having regard to the differences between the relevant airworthiness codes of the United States and the United kingdom, and to any additional requirements as would be prescribed for comparable aircraft constructed in the United Kingdom.
C• Applicability of the Special Conditions Stated in Paragraph b.
The applicability is, to some extent, governed by the all-up-weight of the aeroplane and is as shown hereunder. Unless otherwise stated, the conditions as given above apply in full.
(1) Piston-engined Aeroplanes having an all-up-weight not exceeding 6000 pounds.
(a) (Reference subparagraph b(1).) Advantage may be taken of the British simplified requirements for small aeroplanes appropriate to Performance Groups C or D. The performance date required may be scheduled in a simplified form, details of which may be obtained from the Air Registration Board.
Aeroplanes in this section which will not be certificated in the public transport category while on the British Register may have their export certificates of airworthiness validated without establishing compliance with subparagraphs b(1) and b(2).
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(c) (Reference subparagraph b(5).) The invoking of this condition is strictly limited to, what would be deemed by the Air Registration Board, exceptional circumstances.
(2) Piston-engined Aeroplanes having an all-up-weight between 6000 pounds and 12,500 pounds.
(a) (Reference subparagraph b(1).) Advantage may be taken of the British Simplified Requirements for small aeroplanes appropriate to Performance Groups C and D.
(b) Aeroplanes in this section which will not be certificated in the public transport category while on the British Register may have their export certificates of airworthiness validated without establishing compliance with subparagraphs b(1) and b(2), and only in exceptional cases would subparagraph b(5) be invoked.
(3) Piston-engined Aeroplanes having a maximum all-up-weight in excess of 12,500 pounds.
(a) (Reference subparagraph b(1).) As an alternative to this subparagraph, the Air Registration Board will normally be prepared to recommend validation of an aeroplane certificated in the United States transport category for operation in accordance with the rules appropriate to Performance Group X of the Air Navigation (General) Regulations 1960.
(b) The information contained in the flight manual for operations in the United States to Federal Aviation Regulations, Part 121 is usually adequate for this purpose, subject to the provisions of the following additional information:
1 A statement in the flight manual to the effect that the aeroplane must be operated to rules appropriate to Performance Group X of the Air Navigation (General) Regulations 1960.
Data on the effect of the ambient air temperature on the rates of climb with two engines inoperative.
A statement of the air speed to be assumed when complying with the regulations relating to flight over water. (See BCAR, D2-2, paragraph 41.1).
4 The provision of data on the effect of temperature on the en route rate of climb with one engine inoperative is optional. (This data is only needed if the operator wishes to take advantage of the rules permitting use of "drift down" procedures.)
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d. In the case of other than conventional fixed-wing aeroplanes, the Air Registration Board may, for the issue of a recommendation for the validation of the United States export certificate of airworthiness, require compliance to be established with the appropriate British Civil Airworthiness Requirements and such additional requirements as are applied in the United Kingdom.
Administration and Procedures. The administrative procedures which must be followed by the applicant for validation are dealt with in BCAR, Section A. Unless otherwise agreed by the Air Registration Board, each aeroplane submitted for validation shall be accompanied by the following documents:
(1) An export certificate of airworthiness 1ssued within a period of 60 days immediately preceding the date of validation.
(2) Three copies of the flight manual pertaining to the particular aeroplane.
(3) Two copies of the maintenance manual pertaining to the particular aeroplane and prepared in a form which will provide information for the maintenance of the airworthiness of the aeroplane.
NOTE: With reference to (2) and (3) above, fewer copies may be sufficient in cases where there is already an aircraft of the same type on the British Register.
f. Certification of Aeronautical Products. An export certificate of fate attached will be the hied states airworthiness with pertinent data attached will be required in connection with any Class I product exported from the United States to the United Kingdom. To be eligible for installation on certificated civil aircraft registered in the United Kingdom, Class Il and Class III products must be processed in accordance with the applicable provisions of Part 21 of the United States Federal Aviation Regulations.
8 • Special Conditions for Restricted Category Aircraft. Applications for United Kingdom validation of U.S. export certificates of airworthiness issued in respect of restricted category aircraft will be considered on an individual basis and generally subject to the following conditions:
(1) The aircraft type must hold a valid United States 'type certificate and be eligible for export to the United Kingdom.
(2) A statement, endorsed by the Federal Aviation Administration, shall be furnished to the Air Registration Board describing the manner in which the aircraft has been modified from the "standard category" configuration to make it suitable for some "special
Appendix 2 AC 21-2B Page 64 10/2/69 purpose" operation. This statement should also indicate that part of the Federal Aviation Regulations and the FAA Aircraft Specifications or Type Certificate Data Sheet under which the aircraft would have been eligible for type certification in the "standard category" except for those "special purpose" modifications accomplished by the manufacturer and which are approved by the Federal Aviation Administration. Other aspects of the validation procedure being acceptable, the Air Registration Board will, on the basis of the information provided under g(2) and such advice as it may seek from the FAA, decide whether or not to make a recommendation for the United Kingdom validation of the United States export certificate of airworthiness.
Aircraft certificated in the "restricted category" or designed to airworthiness requirements other than FAR, Part 23 or Part 25, will not normally be eligible for United Kingdom validation.
The general procedures as laid down in the United Kingdom Special Conditions dated the lst November 1960 will continue to apply.
* U, S. GOVERNMENT PRINTING OFFICE: 1889 O - 968-340