Appendix 2 One copy each of the maintenance and repair manual applicable to the airframe (see Notes 1 and 2).
(9) One copy of the parts catalog applicable to the airframe (see Notes 1 and 2).
(10) One copy of information regarding reassembly and rigging oi the aircraft, if not contained in (7) above. This requirement is applicable only to aircraft that are shipped disassembled.
(11) One three-view drawing of the aircraft, scaled to not less than 1/50, if not contained in (7) above (see Note 2).
(12) One copy each of the approved Aircraft Flight Manual and/or related manuals required for the safe operation of the aircraft (e.g., Operation/Performance Manuals, Owner's Manuals, Veight and Balance Manua.s, etc.). These documents shall include all approved supplements established by the type certificate holder.
(13) _ Noise certification reports and data in accordance with ICAO Annex 16, Volume I.
(14) Emissions certification reports and data in accordance with ICAO Annex 16, Volume II (for turbine engines only).
(15) One copy each of the applicable Type Certificate and the respective Type Certificate Data Sheet.
Let on in one copy each o (16) A complete set of pertinent manufacturer's information, modifications, service bulletins, service letters and/or similar documentation in one copy each.
A statement by the manufacturer or his authorized representative to the effect that all pertinent operational and maintenance documentation listed above will be automatically updated and kept current free-of-charge for the Swiss FOCA reference files until written cancellation by the Swiss Authority.
2.2 If application is made for acceptance of an aircraft model in Switzerland that was certified in the United States by extension of an existing Type Certificate that was previously documented to the Swiss FOCA, the following shall apply:
(1) If data as already certified and accepted by the Swiss Authority remains unchanged, the manufacturer shall provide a statement to this effect.
(2) If data as already certified and accepted by the Swiss Authority is amended or revised, only those parts shall be documented as required in 2.1.
Appendix 2
(3) Full operational documentation as listed under 2.1(12) is required in any case.
2.3 All Class I products exported to Switzerland, regardless of the conditions set forth under 2.1 and 2.2 (first of a model documentation) must be accompanied by the following documentation:
(1) An Export Certificate of Airworthiness, FAA Form 8130-4.
(2) For each individual aircraft, the following documents are required:
- One approved Aircraft Flight Manual.
- Two copies of the required approved Aircraft Flight Manual supplements (see Note 3).
- Two copies of the weight and balance statement and the equipment list or the Weight and Balance Manual (see Note 3).
- One copy each of any related manuals established by the manufacturer and required for the safe operation of the aircraft
(e.g., Owner's Manual, Pilot's Manual, etc.).
(3) Logbooks that show any previous time in service and all maintenance action performed.
(4) A statement or a list to show compliance with any Airworthiness Directives for the airframe, engine, propeller, and the installed accessories.
(5) Full documentation for any alteration incorporated under the provisions of a Supplemental Type Certificate approved by the United States FAA or an authorized representative.
(6) Two copies of any Major Repair and Alteration, FAA Form 337, applicable to the product (see Note 3).
2.4 All Class II products exported to Switzerland shall carry an Airworthiness Approval Tag, FAA Form 8130-3. In case of overhauled or repaired Class II products, one copy of the overhaul or repair report is to be supplied with the product. Any previous time in service shall be documented.
2.5 Class III products, if properly marked and identifiable need no additional documentation.
NOTES:
1) Documentation mentioned under 2.1(1), (2), (4), (7) and (8) may be supplied in microfiche format, if available.
Appendix 2
2) These documents are not required for airline type aircraft certified in the transport category.
These documents are required in one copy only for airline type aircraft certified in the transport category.
4) Documentation for engines, propellers, accessories, and avionic equipment is only to be supplied on special request by the Swiss FOCA.
5) Mailing address for all documentation is:
Swiss Federal Office for Civil Aviation Division for Aeronautical Material Federal Building Inselgasse 3003 Berne, Switzerland 165
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.