Appendix 2
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.
Appendix 2
TAIWAN - SPECIAL REQUIREMENTS (REVISED NOVEMBER 22, 1990) SECTION 1 - INTRODUCTION. This section briefly describes administrative procedures for airworthiness acceptance of aeronautical products for import to Taiwan from the United States of America. Since Taiwan and the United States of America have no bilateral agreement for the reciprocal acceptance of aeronautical products, Taiwan reserves the right to either accept or deny importation of aeronauticai products. To simplify the acceptance of all aeronautical products, the United States of America, Federal Aviation Regulations applicable to exporting aeronautical products will be acceptable and will be complied with by the exporter.
Administration and Procedures:
1. All aeronautical products Class I, II and III to be eligible for export to Taiwan must comply with the applicable provisions prescribed in Part 21, Subpart L, of the U.S. Federal Aviatior equlations, In particular, each Class I product will be exportec with an Export Certificate of Airworthiness (FAA Form 8130-4) issued no longer than 90 days or 100 operating hours, whichever is the lesser period, since the date of issuance, and each Class II and III product will be exported with an Airworthiness Approval Tag (FAA Form 8130-3).
2. Aircraft and other Class I products to be eligible for export to Taiwan 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 Special Requirements under Section 2 of this document.
3. All aeronautical products located outside the United States may be eligible for export to faiwan, however, they must have airworthiness approval for export in accordance with the U.S. Federal Aviation Regulations, Part L1.
4. The exporter must show evidence that the products or parts thereof were manufactured under one or more of the following approvals:
a. The current, valid FAA Production Certificate for the products involved, as prescribed in Subpart G of Part 21 of the U.S.
Federal Aviation Regulations.
b. An FAA Approved Production Inspection System (FAA-APIS) letter of approval, as stated in Subpart F of Part 21 of the U.S.
Federal Aviation Regulations.
(Product that has been manufactured under Type Certificate only, a Statement of Conformity, FAA Form 8130-9, must be included.)
Appendix 2 C. An FAA Replacement and Modification Parts Manufacturers Approval (FAA-PMA) letter of approval issued by FAA in accordance with Subpart K, Part 21, of the U.S. Federal Aviation Regulations.
d. A Technical Standard Order (TSO) acknowledge or authorization issued by FAA per the U.S. FAR Part 21, Subpart O.
5. Class I products to be eligible for export to Taiwan are those listed in the aircrait, engine, and propeller Type Certificate Data Sheets (TCDS) and are in production currentiy.
All Class I products exported in unassembled condition shall have sufficient instructions which describes working procedures, methods of rigging/alignment, ground testing, inspection methods, and other pertinent data for the assembly in Taiwan. The Export Certificate of Airworthiness will be invalid if all data to properly assemble the
7. A statement must be signed by a manufacturer's representative to the effect that all Airworthiness Directives (AD) have been complied with, that all mandatory modifications have been embodied, and that any special inspections required have been carried out.
8. To be eligible for operation under the importing country registration, the aircraft must be equipped/installed in accordance with the requirements of the operating regulations/special regulations required in Taiwan. Complementary information may be obtained from:
Chief, Airworthiness Branch Flight Standards Division Civil Aeronautics Administration Taipei Sung Shan Airport Taipei, Taiwan R.O.C. 10592 SECTION 2 - SPECIAL REQUIREMENTS. The following is the special administrative requirements which must be satisfied at the time of export for products to be eligible for airworthiness certification by Taiwan. The documents listed below must be provided and addressed to:
Chief, Airworthiness Branch Flight Standards Division Civil Aeronautics Administration Taipei Sung Shan Airport Taipei, Taiwan R.O.C. 10592
1. For each individual new aircraft.
The original Export Certificate of Airworthiness, FAA Form 8130-4.
b. An aircraft Bill of Sale or other evidence of ownership.
Appendix 2
c. A list of all equipment installed on the particular product and Buyer Furnished Equipment (BFE/Buyer Options), containing serial numbers, part numbers, and locations instruction. (A statement of being compatible with the Type Specifications for BFE's.)
d. A list of radio communication and navigation equipment installed, including make, model, locations, capacity, frequencies and operating instructions.
e • The current weight and balance report and loading schedule, containing a complete inventory of all equipment and instructions.
Notification of the aircraft having been canceled from the exporting country registration.
and a statement of compliance shown at the time of issuance of the g. The List of all Airworthiness Directives (AD) issued by FAA, Export Cértificate of Airworthiness.
h. A copy of the manufacturer production flight test report, and all the discrepancies found during the flight test have been rectified.
i. Modification Standard, including Production Modification, Customer Options, and Equipment incorporated not necessarily installed by the manufacturer.
particular aircraft must be included in the Type Certificate Data A copy of Type Certificate Data Sheets (TCDS).
k. A copy of Supplemental Type Certificate (STC), if any, and details of alterations embodied under STC.
. Statement of Build Standard, including aircraft specifications, additional requirements, special conditions, equivalent safety items, and exemptions.
m. Language. The required marking and placards installed in passenger cabin, in cargo baggage or storage compartments, and in the aircraft exterior should be represented in bilingual--Chinese and English.
n. Seating configuration approval document. The applicant shall forward to the importing country for certification prior to issuance of Export Certificate of Airworthiness.
o. Record of rigging checks.
p. Record of compass system and magnetic compass swings.
Appendix 2
2. For aircraft first of the type/model. In addition to the documents listed above in paragraph 1, the following technical data are required:
a. One copy of the Type Flight Test Report.
b. One copy of Production Certificate with, Production Limitation Record, or the Approved Production Inspection System.
c. FAA approved Master Minimum Equipment List.
d. Structurally Significant Items and System Significant Items.
e • Three-view drawings of the major assemblies, installations, and primary structure.
f. Noise Type Certificate.
g. A statement of compliance with the current requirements of fuel venting and engine exhaust emissions.
h. Manuals:
h.1. Maintenance Review Board Report (MRB).
h.2. Maintenance Planning Document (MPD).
h.3. Flight Manual. Provides aircraft performance operating limitations and other flight data required by relevant Airworthiness Authorities for certification. It includes the Configuration Deviation List.
h.4. Operations Manual. Provides aircraft and system descriptions, normal, abnormal, and emergency procedures and operational performance.
h.5. Maintenance Manual.* /Wiring diagram.*
h.6. Structural Repair Manual.*
h.7. Illustrated Parts Catalog (IPC).*
h.8. Weight and Balance Manual.
h.9. Components Manual
- Overhaul/Component Maintenance Manual Manufacturer.*
- Overhaul/Component Maintenance Manual Vendor.*
h.10. Non-destructive Inspection Manual.*
h.11. Overhaul/Repair Standard Practices Handbook.
Appendix 2
h. 12. One complete set of Service Bulletins or the equivalent.
h.13. Engineering Documents
- Standards Manual: contains data about standards approved by the exporter including reference lists.
- Process and Material Specification: contains data related to manufacturing processes and material identification and treatments used in the construction assembly of the Aircraft.
NOTES: Marking * means either microfilm or microfiche will be accepted.
3. For each individual used aircraft. In addition to the documents listed in paragraph 1 and 2, the following technical data are required:
A photocopy of canceled U.S. Standard Airworthiness Certificate.
b. The certified logbooks or equivalent historical records for the Class I product and the major equipment and components (such as APU), contains information on operational times and cycles (since new and since last overhaul), maintenance, overhaul, repairs, and modifications, and status of parts with limited life time.
c. The past maintenance schedule and programs.
d. The components operating and storage limits, overhaul life summary, including details of service remaining and modification standards.
Component and structure retirement life summary, including details of service life remaining.
f. Compliance with structural sampling schedule and location/position, and description of the details of sampling procedures and practices.
g. Maintenance reliability programs for previous operator's fleet which include the exported aircraft
- Previous and recurring inspection cycles of system/components.
- Analysis and calculating methods for monitoring the maintenance programs.
- Performance standards of the monitored system/components.
4. For engine and propeller.
a. Export Certificate of Airworthiness, FAA Form 8130-4.
b. Compliance with FAR Part 21, Subpart I.
Appendix 2
c. Statement of all AD's and Mandatory SB's complied with.
d. Manuals
- Maintenance, Illustrated Parts Catalog, and Overhaul documents.*
- Service Bulletins and, if applicable, Service Information/Letters.*
5. For aircraft/engine/propeller parts and components.
a. Airworthiness Approval Tag, FAA Form 8130-3.
b. Compliance with FAR Part 21, Subpart L.
c. Statement of all AD's and Mandatory SB's complied with.
6. For radio/APU/appliances and other Class II and III products.
a. Airworthiness Approval Tag, FAA Form 8130-3.
b. Compliance with FAR Part 21, Subpart L.
c. Statement of all AD's and Mandatory SB's complied with.
7. NOTES:
a. Marking * means either microfilm or microfiche will be accepted.
b. The amendments or new issues of all the manuals listed in the above paragraphs will be the responsibility of the exporter.
Appendix 2
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. aircrait manufactured to Federal Aviation Administration (FAA) standards.
Appendix 2
UNITED KINGDOM - SPECIAL REQUIREMENTS (Revised - April 1992) SECHON. - 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 issue of Section B 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 U.K must 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 is 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 otherwise waived by the UK-CAA.
(4) The applicant for a U.S. Export Certificate of Airworthiness is also responsible for satisfying all other U.K.
Special Requirements (identified in Section 2 of this appendix), as appropriate, ior the particular product being exported to the U.K.
and all applicable requirements of FAR 2l, Subpart I, before the U.S.
Export Certificate of Airworthiness can be issued.
(5) British documents providing information on the procedures and requirements for U.K. acceptance of U.S. products are on file in each FAA Aircraft Certification 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.
oilateral 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 lbs.) weight intended for use in the U.K. Transport Category, the design of all aircraft exceeding 5,700 kg (12,500 lbs.)
regardless of the intended certification category, and all rotorcraft offered for U.K. certification. Additionally, in accordance with the olicy declared in CAA Airworthiness Notice No. 15, the CAA may equire to evaluate certain aircraft of less than 5,700 ko weichi 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) (ii) 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) (iii) 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.
Appendix 2
(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)(iii) 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 Section B, Chapter B4-10, 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 B, Chapter B4-8, of BCAR.
(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:
(i) They are properly designated, and
(ii) 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 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 [[the]] CAA by the appropriate means.
(3) On the basis of this evidence, the CAA will decide whether it is necessary to seek further information from the FAA and 176
Appendix 2 which, if any, of the procedures described in paragraphs (1) and (2) above shall be invoked.
SECTION 2 - SPECIAL REQUIREMENTS. The following identifies those special administrative requirements which must be satisfied at the time oi export (in addition to any U.K. Special Conditions) for a particular product to be eligible for U.K. registration, certification and/or airworthiness validation.
A. All Aircraft.
* (1) Statement of Build Standard. This statement to include changes in design (as required by U.k.
Special Conditions) and a list of Service Bulletins incorporated ir production. The list of Service Bulletin incorporation is to identify:
(i) Production versions of the Service Bulletins.
(ii) Service Bulletin compliance.
(iii) Alert Service Bulletin compliance.
(2) Modification Standard. This must include:
(i) Customer options incorporated.
(ii) Equipment incorporated, including items of equipment not necessarily installed by the manufacturer.
(iii) Service Bulletin compliance.
(iv) Alert Service Bulletin compliance.
(3) Export Certificate of Airworthiness. The U.S. Export Certificate of Airworthiness must list the status of compliance with U.K. Special Conditions including, by issue and date, those which have been complied with and those which have not. Accordingly, the following information should be noted on the U.S. Export Certificate of Airworthiness when issued for any aircraft to which the U.K.
Special Conditions are applicable:
The date and issue number of the U.K. Special Condition which has been complied with.
(ii) The list of Special Condition numbers which have been complied with.
(iii) The list of Special Condition numbers which have not been complied with.
(iv) List the operating hours accumulated of the aircraft engine (s) and propeller (s).