Appendix 2
(4) Flight test report according to production flight test schedule.
(5) Maintenance records. The products must be accompanied by maintenance records equivalent to those specifiec below that reflect the status of required inspections, life limits, . etc.
(a) Records of the maintenance (including FAA form 337 or equivalent), preventive maintenance, and alteration, and records of the 100-hour, annual, progressive, and other required or approved inspections, as appropriate, for each aircraft (including the airframe) and each engine, propeller, rotor, and appliance of an aircraft. The records must include:
(1) a description (or reference to data acceptable to the RAI) of the work performed;
(2) the date of completion of the work performed; and
(3) the signature and certiticate number of the person approving the aircraft for return to service.
(b) Records containing the following information:
(1) the total time in service of the airframe, each engine and each propeller;
(2) the current status of life-limited parts of each airframe, engine, propeller, rotor, and appliance;
(3) the time since last overhaul of all items installed on aircraft which are required to be overhauled on a specific time basis; and
(4) the identification of the current inspection status of the aircraft, including the times since the last inspections required by the inspection program under which the aircraft and its appliances are maintained.
(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 I.
Appendix 2
(3) Statement of Service Bulletins complied with.
(4) Operational check.
(5) Maintenance records.
(6) Life limited parts record.
(e) Engine/Propellers Parts.
(1) Airworthiness Approval Tag (FAA Form 8130-3).
(2) Compliance with FAR 21, Subpart L.
(I) Appliances.
(1) Airworthiness Approval Tag' (FAA Form 8130-3).
(2) Compliance with FAR 21, Subpart L.
(g) Components.
(1) Airworthiness Approval Tag (FAA Form 8130-3).
(2) Compliance with FAR 21, Subpart L.
(3) Statement of Service Bulletin complied with.
Appendix 2
JAPAN - SPECIAL REQUIREMENTS (Revised February 24, 1992)
1. Aircraft and other Class I products to be eligible for certification by the Government of Japan should be covered by Export Certificates of Airworthiness, as provided for in Part 21 of the United States Federal Aviation Regulations. Class II and III products will be exported in accordance with procedures prescribed in the applicable provisions of Part 21 of the United States Federal Aviation Regulations. Export Certificates of Airworthiness and other related data should be forwarded by the manufacturer or the exporter to the Airworthiness Division, Engineering Department, Civil Aviation Bureau, Ministry of Transport, No. 3 Godo-Chosha, 2-1-3, Kasumigaseki, Chiyoda-ku, Tokyo, 100, Japan. This does not include data required to be carried in the aircraft in the case of flyaway delivery.
2. In addition to the foregoing, the following materials should be furnished with aircraft to be exported to Japan:
a. If the aircraft is the first (see 1/) of a model to be exported to Japan, the following materials should be furnished with aircraft (this should include aircraft, with Supplemental Type Certificate and being the first of a model exported to Japan):
(1) One copy oi the current oificial aircrait, engine, and propeller specifications and special conditions and/or exemptions included in the certification basis.
(2) Engineering description of the aircraft including general design philosophy and required illustrations.
(3) Aircraft, engines, and propellers certification compliance table (checklist) based on the selected applicable requirements, and indicating that these requirements are complied
(4) Master equipment list.
(5) Evidence of strength of primary structure as ascertained by physical tests and/or calculation including load analysis report on airframe, and electrical load analysis report.
(6) Evidence of substantiation regarding stress level, low cycle fatigue, endurance, icing, ingestion and blade containment of engine. (For turbine engine only.)
(7) Schematic drawings, descriptions, and failure analysis reports on aircraft systems.
1/ When in doubt as to whether an aircraft is the first of a model, contact the Civil Aviation Bureau of Japan.
Appendix 2 One copy of the type flight test report and one copy of production flight test report including procedures and tolerances.
One copy of minutes of type certification board meetings and issue papers.
(10) One copy of maintenance review board report and minimum equipment list for aircraft type certificated in transport category.
(11) One copy of parts catalog and operating, maintenance, overhaul, repair manuals, and service bulletins applying to the aircraft, engines, propellers, and major equipment installed on aircraft.
(12) One copy oi approved ilight manual and weight and balance report applicable to the particular aircraft.
(13) Certified aircraft, engines, and propellers, logbooks, or other equivalent historical records showing total time and time since last overhaul.
(14) Record of all modifications accomplished prior to exporting, mandatory as well as non-mandatory.
(15) If the aircraft is certificated in the restricted category, the following materials shall be furnished with the aircraft in addition to above (1) through (14).
le manner in which the A statement by the Federal Aviation Administration, describing the manner in which the aircraft has been modified from the "standard category" configuration to make it suitable for "special purpose" operation.
(b) A statement indicating part of the Federal Aviation Regulations, 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.
(16) In case of aircraft equipped with turbo-jet engines, one copy of the report for noise certification, which should consist of the following items:
(a) Certified maximum noise levels and their 90 percent confidence limits in accordance with the applicable chapters and appendices of ICAO Annex 16, volume I, Second Edition (1988), or certified maximum noise levels and their 90 percent confidence limits in accordance with applicable aircraft noise requirements of the U.s.
Federal Aviation Regulations.
NOTE: In the latter case, maximum noise levels and their 90 percent confidence limits measured and/or calculated in 94
Appendix 2 accordance with the applicable chapters and appendices of ICAO Annex 16, volume I, Second Edition (1988), should also be attached.
(b) Description of noise measuring and analyzing procedures including correction methods.
(c) Statement of any additional modification incorporated for the purpose of compliance with the applicable noise certification standards.
NOTE (1): The manufacturer or exporter will be advised by the purchaser on the basis of information furnished to the purchaser by the Civil Aviation Bureau of Japan when the aircraft is the first of a type or model to be imported into Japan.
NOTE (2): All the applicable changes and future issues of tal applia be the above material should be automatically forwarded to the Airworthiness Division, Engineering Department, Civil Aviation Bureau, Ministry of Transport.
NOTE (3) : The Civil Aviation Bureau of Japan may request additional type design data other than the foregoing materials for the issuance of Japanese Airworthiness Certificate.
b. In case aircraft of the same model has been exported to, and certificated in Japan, the following materials should be furnished with aircraft:
(1) One copy of parts catalog and operating, maintenance, overhaul, and repair manuals applying to the aircraft, engines, propellers, and major equipment installed on aircraft.
(2) One copy of approved flight manual and weight and balance report applicable to the particular aircraft.
(3) Certified aircrait, engines, and propellers logbooks, or other equivalent historical records showing total operating time anc time since last overhaul.
(4) Record of all modifications accomplished prior to exporting, mandatory as well as non-mandatory.
(5) Electrical load analysis report applicable to the particular aircraft.
NOTE: The Civil Aviation Bureau of Japan may request additional type design data other than the foregoing materials for the issuance of Japanese Airworthiness Certificate.
Appendix 2
3. If the aircraft is to be exported via flyaway to Japan without U.S. registration, the manufacturer or exporter should display on the aircraft Japanese nationality and registration marks and carry Japanese certificate of registration and ferry permit in the aircraft.
a. Upon application of the purchaser, Civil Aviation Bureau of Japan will issue certificate of registration and ferry permit when the Japanese importer or the U.S. exporter furnishes Civil Aviation Bureau of Japan the following information:
(1) Make and model of the aircraft.
(2) Serial number of the aircraft.
(3) Purchaser's name and address.
(¼) U.S. exporter's name and address.
(5) Document which certifies transfer of ownership of the aircraft together with data of transfer.
(6) Document which certifies airworthiness of the aircraft (Export Certificate of Airworthiness, FAA Form 8130-4).
b. After the Civil Aviation Bureau of Japan receives the foregoing application and information, Japanese certificate of registration and ferry permit will be delivered to the applicant.
The applicant will then forward these certificates to the U.S.
exporter for installation in the aircraft. After this, the aircraft may be flown from the U.S. to Japan.
c. After the issuance of U.S. Export Certificate of Airworthiness, only the modification for ferry flights covered by FAA Form 337 is acceptable.
4. If a product which does not meet special requirements of Japan is intended to be exported, a Japanese statement waiving a certain requirement applied and validating the export airworthiness certificate is required. All exceptions covered by the statement will be listed in the export airworthiness certificate.
Appendix 2
REPUBLIC OF SOUTH KOREA - SPECIAL REQUIREMENTS (Revised December 27, 1990)
1. To be eligible for certification by the Government of the Republic of South Korea, all Class I, II and III products should be issued export certificates of airworthiness or approvals in accordance with the provisions of Subpart L of Part 21 of the Federal Aviation Regulations.
In addition to the foregoing, the following materials will be furnished for aircraft to be exported to the Republic of South Korea.
A. New Aircraft.
(1) Statement of Build Standard.
This statement to include the aircraft specification and list of Service Bulletins incorporated in 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.
(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) A copy of the aircraft type certificate plus any applicable Supplemental Type Certificates, and a copy of the aircraft noise certification.
(6) Engine/Airframe/APU log books.
Appendix 2
(7) Seating confiquration approval document, where appropriate. (For "r" category.)
(8) MRB Program, where applicable. (For "r" category.)
(9) Production aircraft test report.
(10) Time/Life limitations.
(11) Electrical load analyses.
(12) Minimum equipment list.
(13) Wiring diagram.
(14) Weight schedule and weighing report.
(15) Manuals:
Number Required Classification of Manuals "#" Flight Manual 1 Maintenance 2 1 Operations (or Pilot Operating Handbook) 3 1 Weight and Balance Loading Procedures 1 - Overhaul 2 Structural Repair 2 Component Overhaul 2 Engine Maintenance and Overhaul 2 NDT 2 - Structurally significant items 1 Maintenance planning guide Parts catalogue 2 1 Remarks "#" The required only with first aircraft of a particular type and model exported to Republic of South Korea.
"*" Normally the required with same model has been exported to, and certified in Republic of South Korea.
Appendix 2
(16) Record of Compass System and Magnetic Compass swings.
(17) Record of rigging checks.
(18) Detailed list of radio equipment constituting the radio station.
(19) Antenna performance patterns.
(20) List of Serial Numbers of significant component parts, including serial numbers, which are not listed in the parts catalogue.
B. Used Aircraft.
In addition to the information referred to above the following is also required for used aircraft (for "p" category):
(1) The maintenance program to which these aircraft have previously been maintained including:
(i) previous check cycle; and
(ii) future check cycle.
(2) Component overhaul life summary, including details of service life remaining and modification standards.
(3) Compliance with structural inspection program. This to include details of any structural sampling program in which these aircraft have been included, together with details of their position in this program.
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 Service Bulletins complied with.
E. Engine/Propeller Parts.
(1) Airworthiness Approval Tag (FAA Form 8130-3).
(2) Compliance with FAR 21 (Subpart I).
Appendix 2 F. Appliances.
(1) Airworthiness Approval Tag (FAA Form 8130-3).
G. Components.
(1) Airworthiness Approval Tag (FAA Form 8130-3).
(2) Compliance with FAR 21 (Subpart L).
(3) A statement of Service Bulletin compliance standard.
Appendix 2
REPUBLIC OF LEBANON - SPECIAL REQUIREMENTS (New - September 20, 1977)
1. Lebanese acceptance of U.S. aeronautical products.
a. Lebanon's policy is to accept, without modification, aircraft which meet requirements of the competent authority in the country of manufacture. All U.S. equipment meeting Federal Aviation Administration (FAA) requirements are therefore acceptable.
Appendix 2
MALAYSIA - SPECIAL REQUIREMENTS (Revised December 1984)
1. GENERAL.
conditions to be satisfied for the certification and use in Malaysia 1.1 This document specifies the special requirements and tented state of aeronautical products of United States origin imported from the United States.
1.2 Authority for aircraft registration and certification is vested in the Department of Civil Aviation (DCA); correspondence should be addressed to:
Airworthiness Unit Department of Civil Aviation Subang International Airport Selangor, Malaysia
1.3 Malaysia does not issue Type Certificates.
1.4 Eligibility for the issue of a Malaysian Certificate of Airworthiness is determined by:
compliance with the appropriate requirements of paragraph 2, 3, and 4 of this document (but see also paragraph 5).
(b) compliance with:
(1) Additional Directives and Airworthiness Notices issued by the United Kingdom Civil Aviation Authority.
(ii) Advisory Notices issued by the DCA which are classified as requiring a mandatory action.
NOTE: Compliance with this sub-paragraph (b) is not essential before export to Malaysia. However, as it may pe difficult to establish conformity in Malaysia, details of any relevant service document and modification status will be helpful to the Malaysian user.
(c) Completion of a flight test in accordance with a DCA approved Airworthiness Flight Test Schedule unless otherwise agreed by the DCA.
2. ELIGIBILITY FOR EXPORT TO MALAYSIA.
2.1 Class I, II and III products must comply with the requirements of Subpart L of FAR Part 21 and the requirements of this document.