Appendix 2
KINGDOM OF SAUDI ARABIA - SPECIAL REQUIREMENTS (REVISED - NOVEMBER 1990)
1. General.
eligible for export to the Kingdom of Saudi Arabia, maR'S¿ a) Aircraft and other Class I, II, and III products to be addition to the requirements prescribed in Part 21 of the U.s. must be eligible for airworthiness certification in the "standard" classification and comply with the applicable special requirements.
NOTE: Aircraft eligible for certification in the United States, "restricted," "limited," or "experimental" classification, may be exported to the Kingdom of Saudi Arabia only if a prior and specific approval of the President of Civil Aviation (PCA) is obtained.
b) In all instances, manufacturers or suppliers must certify on the face of their invoice that the product involved was manufactured under one or more of the preceding procedures: i.e., FAA PC No.
FAA-APIS letter dated _; FAA-PMA letter dated _; TSO NO.
MIL. Spec. ; other government or industry specifications.
2. In addition to the foregoing, the following administrative requirements and material shall be furnished to the PCA including revision service:
a) New Aircraft.
1) Statement of Build Standard. This statement to include the aircraft specification and a list of Service Bulletins incorporated in production.
2) Statement of Modification status. This must include:
i) Customer options incorporated.
ii) Equipment incorporated.
iii) Service Bulletin including Alert Service Bulletin compliance.
3) FAA Export Certificate of Airworthiness.
4) Airworthiness Directives. A declaration of compliance with all Airworthiness Directives issued by the FAA must be provided.
Where optional means of compliance are offered, the means chosen shall be stated.
* 5) Type Certificate Data Sheets or Specifications. FAA Aircraft, Engine, and Propeller Data Sheets including any supplemental type specifications.
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6) Equipment List.
* 7) Wiring Diagram.
8) Weight schedule and weighing report.
* 9) Electrical load analyses.
* 10) MRB program, where applicable.
11) Time/life limitations.
12) Copy of Production Flight Test Report related to the specific aircraft.
13) Record of Compass System and Magnetic compass swings.
14) Detailed list of radio equipment constituting the radio station.
15) Statement of compliance with mandatory equipment and radio apparatus.
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16) MANUALS: Number Required
(i) Flight Manual 1 (+1 for each aircraft) * (ii) Aircraft Maintenance and Overhaul 1 * (iii) Operations 1 * (iv) Engine Maintenance and Overhaul 1 * (V) Maintenance Planning Guide 1 * (vi) Structural Repair 1 * (vii) Parts Catalog 1 *(viii) Weight and Balance Loading Procedures 1 * (ix) Standard Practices 1 * (x) Propeller Maintenance and Overhaul 1 * (xi) Structurally Significant items 1 * (xii) Complete set of Service Bulletin (Aircraft) * (xiii) Complete set of Service Bulletins (Engines) * (xiv) Complete set of Service Bulletins (Propellers) NOTE: * Required only with first aircraft of a particular type and model exported to the Kingdom of Saudi Arabia.
b) Used Aircraft. In addition to the information referred to above, the following is also required for used aircraft:
1) A complete history of the aircraft, engines, components and equipment including:
(1) The number of landings and pressurization cycles where the aircraft is subject to mandatory life limitations.
(ii) The maintenance program to which the aircraft have previously been maintained.
2) The flight time since new of any components of the aircraft, engines, or equipment which are subject to mandatory life limitations.
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3) The flight time since new or overhaul, as appropriate, of any components of the aircraft, engines, or equipment which are subject to an approved overhaul period.
4) Detaiis or ali changes or major structura_ components such as wings, taliplanes, helicopter rotors or transmission components, and histories of the replacing components.
Details of major structural repairs including the nature of damage in each case.
c) Aircraft Parts.
1) Airworthiness Approval Tag (FAA Form 8130-3);
2) Compliance with FAR 21 (Subpart L).
d) Engines/Propellers.
1) Export Certificate of Airworthiness (FAA Form 8130-4);
2) Compliance with FAR 21 (Subpart L);
3) Statement of Mandatory Service Bulletins complied with.
e) Engine/Propeller Parts.
1) Airworthiness Approval Tag (FAA Form 8130-3);
2) Compliance with FAR 21 (Subpart L).
£) Components.
1) Airworthiness Approval Tag (FAA Form 8130-3);
2) Compliance with FAR 21 (Subpart L);
3) Statement of Mandatory Service Bulletins complied with.
g) Appliances.
1) Airworthiness Approval Tag (FAA Form 8130-3);
2) Statement of Mandatory Service Bulletins complied with.
3. Export - flyaway aircraft.
a) An aircraft which is being exported to the Kingdom of Saudi Arabia via flyaway should display Saudi Arabian nationality and registration marks and should carry the following documents on the delivery flight:
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1) Saudi Arabian Certificate of Registration.
2) Saudi Arabian Certificate of Airworthiness or Delivery Flight Authorization.
3) U.S. Certificate of Airworthiness for Export.
4) Approved Flight Manual.
5) MNPS Authorization, if applicable.
Such other documents as may be essential to the safe operation of the aircraft.
b) The Saudi Arabian Presidency of Civil Aviation requests to be advised by telegram of the issuance of a Certificate of Airworthiness for Export in respect of any aircraft which is to be exported to the Kingdom of Saudi Arabia via flyaway.
NOTE: It will be the responsibility of the Saudi Arabian purchaser to ensure that the identification markings are properly displayed upon the aircraft prior to departure from the exporter's base and to ensure that the necessary flight documents are installed and carried in the aircraft during the delivery flight.
Mailing Address:
Presidency of Civil Aviation Vice President, Aviation Standards & Saiety Dept.
P.O. Box 887, Jeddah 21165 Kingdom of Saudi Arabia Cable Address:
Telex: 603235 FSDPCA SJ Fax: 685-5745 / 685-5142 146
Appendix 2
REPUBLIC OF SINGAPORE - SPECIAL REQUIREMENTS (Revised December 26, 1990)
1. INTRODUCTION. The following identifies those special 633237 administrative requirements which must be satisfied at the time of export (in addition to any other validation requirements) for a particular product to be eligible for Singapore registration, certification, or airworthiness validation.
2. SPECIAL ADMINISTRATIVE REQUIREMENTS.
2.1 New Aircraft.
(a) FAA Export Certificates of Airworthiness for the aircraft, engines, and propellers.
(b) A list of Service Bulletins, including Alert Service Bulletins, complied with.
(c) Statement of Modification Status which shall include:
(i) Customer options incorporated.
(ii) Equipment incorporated.
(d) Airworthiness Directives.
(1) A declaration of compliance with all Airworthiness Directives issued by the FAA must be provided. Where optional means of compliance are offered, the means chosen shall be stated.
(ii) FAA Airworthiness Directives containing repetitive compliance requirements must be identified. Information as to when the next compliance is due must also be provided.
(e) Statement of compliance with mandatory equipment and radio apparatus requirements specified in the Schedules of the Singapore Air Navigation Order.
(f) Statement of compliance with requirements specified in the Singapore Airworthiness Notices.
g) A iist oi deiects, ii any, that are to be rectified by the Singapore operator at the time of issue of the Export Certiticate of Airworthiness.
(h) Equipment List.
(i) Weight Schedule and weighing report.
(j) Time/Life limitations.
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(k) Records of compass system and magnetic compass swing.
(1) Noise Certificate.
2.2 First-of-type Aircraft. In addition to the requirements in paragraph 2.1, the following is required for a first-of-type aircraft exported to Singapore, unless otherwise notified:
(a) Statement of build standard which shall include the aircraft specification.
(b) A copy of the aircraft and engine type certificates and applicable Supplemental Type Certificates.
(C) Type Certificate Data Sheets or specifications for aircraft, engine, and propeller, including any supplemental type specifications.
(d) Wiring diagram.
(e) Electrical load analysis.
(‡) Maintenance Review Board Report, where applicable.
(9) Maintenance Planning Data.
(h) FAA approved Master Minimum Equipment List, where applicable.
(i) Noise type certificate.
(]) One copy each of the following manuals:
(1) Flight Manual or Pilot Operating Handbook (in addition to the copy for each aircraft).
(2) Operations (in addition to the copy for each aircraft).
(3) Aircraft Maintenance.
(4) Engine Maintenance.
(5) Propeller Maintenance.
(6) APU Maintenance.
(7) Parts Catalog•
(8) Standard Practices.
(9) Structural Repair.
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(10) Structurally Significant Items.
(11) Loading Procedures.
(12) Weight and Balance.
(13) Non-destructive Testing.
(K) Complete sets of Service Bulletins for aircraft, engine, propeller, and APU. Amendment service for the above documents must be provided.
2.3 Used Aircraft. In addition to the requirements in paragraph 2.1 and, where applicable, in paragraph 2.2, the following is also required for used aircraft:
(a) A complete history of the aircraft, engines, propellers, components and equipment including:
(i) The number of landings and pressurization cycles where the aircraft is subject to mandatory life limitations.
(ii) The maintenance program to which the aircraft has previously been maintained, including previous check cycle and future check cycle.
(b) The flight time since new of any components of the aircraft, engines, propellers, or equipment which are subject to mandatory life limitations.
(c) The flight time since new and since overhaul of any components of the aircraft, engines, propellers, or equipment which are subject to an approved overhaul period.
(d) Details of all changes of major structural components such as wings, tailplanes, helicopter rotors or transmission components, and histories of the replacing components.
(e) Details of major structural repairs including the nature of damage in each case.
2.4 Aircraft Parts.
(a) Airworthiness Approval Tag (FAA Form 8130-3).
(b) Compliance with FAR 21 (Subpart L).
(c) Statement of Airworthiness Directives and Service Bulletins (including Alert Service Bulletins) complied with.
Appendix 2 2„5 Engines/Propellers.
(a) Export Certificate of Airworthiness (FAA Form 8130-4).
(b) Compliance with FAR 21 (Subpart L).
(C) Statement of Airworthiness Directives and Service Bulletins (including Alert Service Bulletins) complied with.
2-6 Engine/Propeller Parts.
(a) Airworthiness Approval Tag (FAA Form 8130-3).
(b) Compliance with FAR 21 (Subpart L).
(c) Statement of Airworthiness Directives and Service Bulletins (including Alert Service Bulletins) complied with.
2.7 Components.
(a) Airworthiness Approval Tag (FAA Form 8130-3).
(b) Compliance with FAR 21 (Subpart L).
(c) Statement of Airworthiness Directives and Service Bulletins (including Alert Service Bulletins) complied with.
2.8 Appliances.
(a) Airworthiness Approval Tag (FAA Form 8130-3).
(b) FAA Certificate of Conformity.
(c) Statement of Airworthiness Directives and Service Bulletins (including Alert Service Bulletins) complied with.
Appendix 2
REPUBLIC OF SOUTH AFRICA - SPECIAL REQUIREMENTS [[Reprinted from AC 21-2F dated August 7, 1987]]
1. An aircrait 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 1 and sata lation on settificited Regulations. Class ll and Class lll products, to be eligibie ror approval and installation on certificated civil aircraft of South pete of bart the at states
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 oi maintenance, overhau_, parts, repair, and operations manuals issued by the manufacturers 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 aircraft, 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 aircrait 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 equivalent document.
(e) The approved flight manual or an equivalent document.
(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.
(c) An approved flight manual or equivalent document.
Appendix 2
KINGDOM OF SPAIN (Revised January 24, 1992)
SPECIAL REQUIREMENTS FOR THE IMPORT OF AIRCRAFT FROM THE UNITED STATES OF AMERICA.
SECTION 1 - INTRODUCTION. This document prescribes special requirements supplementing the Agreement on the Reciprocal Acceptance of Export Certificate of Airworthiness between the Kingdom of Spain (KOS) and the United States of America (USA) that came into effect by the Exchange of Notes in October 13, 1978.
The civil airworthiness authority in the KOS is the Direction General of Aviation Civil (DGAC), and their address is:
Direccion General de Aviacion Civil Telemaco, 54 28071 Madrid, Spain Telex: 27702 CIAIR E or 48339 CIAL E Fax: 34 1 5535014 SECTION 2 - EFFECTIVITY. Effective October 9, 1987, in accordance with the Director General de Aviacion Civil resolution on import of aircraft, to be eligible for a Spanish standard airworthiness certificate, an aircraft of a particular type and model, not previously registered in Spain, must be of a type which has beer issued a Spanish Type Airworthiness Certificate and comply with the special requirements prescribed in this document.
SECTION 3 - REQUIREMENTS FOR ISSUANCE OF SPANISH TYPE AIRWORTHINESS CERTIFICATE. The process to obtain a Spanish Type Airworthiness Certificate for new aircraft (aircraft not previously registered anywhere), defined in Section 2 is initiated by the DGAC upon receipt of the application letter from the manufacturer, through the Federal Aviation Administration (FAA) office responsible for the particular previously registered), defined in Section 2 is initiated upon receipt of the application letter from the prospective registered owner.
The application letter should include a general description and a three-view drawing of the aircraft.
At an early date a schedule will be developed between the manufacturer or prospective registered owner, the FAA, and the DGAC to accomplish the following.
A. Al. Aircraft categories Except Restricted.
A presentation of technical data with a description of the aircraft design emphasizing unusual design features.