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).
Appendix 2 AC 21-2B Page 62 10/2/69
(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.)
AC 21-2B Appendix 2 10/2/69 Page 63
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
AC 21-2B CHG 1 Appendix 11/13/70 Page 65
ZAMBIA, REPUBLIC OF - SPECIAL REQUIREMENTS
1. GENERAL.
Any aircraft, to be eligible for the issue of a Certificate of Registration issued by the Government of the Republic of Zambia, must quality 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 issued in accordance with Part 21 of the United States Federal Regulations.
b. Class 2 and Class 3 products should be accompanied by documentation which conform 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 is acceptable.
If the aircraft is to be entered on the Zambia Register of Civil Aircraft prior to departure from the United States of America, the Importer will make application to the Zambian 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. Enquiries should be addressed to the Director of Civil Aviation, P. O. Box RW 137, Ridgeway, Lusaka, Zambia, marked for the Attention of the Chief Aircraft Inspector.
2. AIRCRAFT FIRST OF THE TYPE TO BE REGISTERED IN THE REPUBLIC OF ZAMBIA.
The following documents and data are required:
a. Complete set of maintenance and overhaul manuals, and parts catalogues, for:
(1) Airplane.
(2) Engine (s)
(3) Propeller (8)
(4) Any equipment not already installed in an aircraft on the Zambian Register of Civil Aircraft.
b. Full set of Service Bulletins, Letters, and Modification Leaflets issued by the manufacturers in respect of the airframe, engine (s), propeller (s), and installed equipment.
c. A copy of the Type Certificate, if not already held by the Department,*
Appendix 2 AC 21-2B CHG 1 Page 66 11/13/70
d. Three copies of the flight manual for the aircraft.
e. One copy of the production flight test report issued by the manufacturer.
3. EACH AIRCRAFT FOR WHICH A ZAMBIAN CERTIFICATE OF AIRWORTHINESS IS TO BE REQUESTED. The following documentation 1s required:
A statement, signed by an official representative of the manufacturers, showing that all mandatory modifications and special inspections have been complied with.
b. The Export Certificate of Airworthiness, FAA Form 8130-4.
C. Two copies of the Approved Flight Manual.
Two copies of the Weight & Balance report showing the weights and arms of the main components, and a list of installed equipment.
AC 21-2B CHG 1 Appendix 3 11/13/70 Page 1 FAA Regional Offices Responsible for Civil Aviation Matters in Foreign Countries Country or Area
a. Canada
b. Caribbean Area, South America Central America, (excluding Mexico) Panama, and the Canal Zone
c. Mexico
d. Area East of East Pakistan and India, including all free nations south and east of China
e. Europe, Africa, Middle East west of Burma, Iceland Greenland, and Bermuda FAA Regional Office Address Federal Aviation Administration Federal Building John F. Kennedy International Airport Jamaica, New York 11430 Federal Aviation Administration P. O. Box 20636 Atlanta, Georgia 30320 Federal Aviation Administration P. O. Box 1689 Fort Worth, Texas 76101 Federal Aviation Administration P. O. Box 4009 Honolulu, Hawaii 96812 Federal Aviation Administration Tour-Madou Building 1 Place Madou Brussels 3, Belgium
AC 21-2B CHG 1 Appendix 4 11/13/70 Page 1
COUNTRIES WITH WHICH THE UNITED STATES HAS
CONCLUDED AGREEMENTS FOR RECIPROCAL
ACCEPTANCE OF AIRWORTHINESS CERTIFICATES The agreements with the following countries are valid for aircrait, aircrait engines, and propellers, and for spare parts for aircraft, aircraft engines, and propellers which have been exported under the terms of the agreements. (Note: The agreement with Japan also includes appliances and spare parts for appliances exported under the terms of the agreement).
8. Australia
b. Austria
c. Israel
d. Japan
e. Switzerland
2. The agreements with the following countries are valid only for aircraft, and components of aircraft exported under the terms of the agreements:
a. Belgium
b. Canada C • Denmark
d. France
e. Germany, Federal Republic of Italy
g. Netherlands
h. Norway
1. South Africa, Republic of Spain
k. Sweden
1. United Kingdom
3. The agreements with the following countries are valid for gliders only and spare parts for gliders exported under the terms of the agreements:
a. Finland
b. Poland U. S. GOVERNMENT PRINTING OFFICE: 1970 O - 410-605
CHANGE AC NO: 21-2B CHG 1 DATE: 11/13/70
EDERAL AVIATION ADVISORY
TMINISTRATO CIRCULAR
DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION SUBJECT:
EXPORT AIRWORTHINESS APPROVAL PROCEDURES.
PURPOSE. This advisory circular transmits revised pages to AC No. 21-2B, dated October 2, 1969.
2. CHANGES:
a. The basic text is revised to:
(1) Provide an explanation of special requirements and bilateral agreements.
Clarify that export certificates of airworthiness do not constitute authority to operate an aircraft.
(3) Provide additional guidance for completion of an application for Export Certificate of Airworthiness, FAA Form 8130-1.
(4) Delete paragraph lf(3) (b) which required the exporter to provide the FAA representative who issued the Export C of A with the name and address of the foreign purchaser.
(5) Delete the reference to FAA International Offices (A new appendix is added giving the FAA Regional Office addresses to which inquiries should be directed).
(6) Renumber the paragraphs and to incorporate other nonsubstantive changes.
b. Appendix 1 is revised to provide a sample application form which shows the "engines" and "propellers" blocks completed for an aircraft.
Initiated by: FS-180
Page 2 AC 21-2B CHG 1 11/13/70
c. Appendix 2 1s revised to:
(1) Incorporate special requirement changes requested by the civil air authority of:
(a) Australia
(b) France
(c) Japan
(d) Kingdom of the Netherlands
(2) Add new special requirements for:
(a) Netherlands Antilles
(b) Republic of Zambia
d. New Appendix 3 and 4 have been added to provide FAA Regional Office addresses and a list of countries with which the U.S. has bilateral agreements.
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