Appendix 2 FEDERAL REPUBLIC of GERMANY
ENCLOSURE I
1. SUPPLEMENTARY AIRWORTHINESS REQUIREMENTS FOR NORMAL, UTILITY AND ACROBATIC CATEGORY AIRPLANES.
1.1 Glider Towing. If certification for the purpose of use for glider towing is requested, compliance with the applicable airworthiness requirements must be shown in connection with the type certification of the airplane.
be available on request from the LBA.
1.2 Parachute Jumping. If certification for the purpose of use for parachute jumping is requested, compliance with the appropriate airworthiness requirements must be shown in connection with the type certification of the airplane. Requirements concerning provision for parachute jumping will be available on request from the LBA.
1.3 Spins. If approval for spins is sought, compliance with the requirement FAR 23.807(b) (b)(5) must be shown.
2. SUPPLEMENTARY AIRWORTHINESS REQUIREMENTS FOR AIRCRAFT INTENDED FOR USE IN COMMERCIAL OPERATION. In connection with additional equipment as it may be required by the German operating regulations in regard of certain operational aspects, supplementary airworthiness requirements could come into effect. The LBA is prepared to inform on an individual basis according to the case under consideration.
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REPUBLIC OF GUATEMALA - SPECIAL REQUIREMENTS (New - August 26, 1981)
1. Aircraft and Aeronautical products to be eligible for export to the Republic of Guatemala from the United States must be exported in accordance with the provisions described in Part 21 of the United States Federal Aviation Regulations Subpart L.
a. An export Certificate of Airworthiness will be required by the Republic of Guatemala Civil Aviation Authority for all Class I products exported from the U.S. to Guatemala.
b. The following additional documents will be required:
1. Log books for aircraft engines and propellers.
2. Up-to-date airplane flight manual translated into the Spanish language.
3. Weight and balance report and equipment list not older than six months.
Record of major repairs, alterations to aircraft engines and propellers i.e.; FAA Form 337 [[Major Repair and Alteration]].
bulleting incorporating latest up-to-date ravisions for aircraft, engines, propellers, and appliances. Maintenance manual, structural repair manual, service
6. A complete list of Airworthiness Directives notes and mandatory service bulletins applicable to the aircraft, date of propeller or appliance indicating method of compliance, compliance, signature of licensed individual and certificate number.
7. A copy of latest up-to-date specification for aircraft, engines, and propellers.
Class Il and Class III products shall be exported in accordance with the provisions prescribed in Part 21 of the u.s.
Federal Aviation Regulations.
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REPUBLIC OF HONDURAS - SPECIAL REQUIREMENTS (New - November 6, 1981)
1.) The aeronautical products and aircrafts exported to the Republic of Honduras from the United States of America, should be exported in accordance with the Part 21 of the U.S. Federal Aviation Regulations Subpart I.
a) An Airworthiness Certificate for Export is necessary for the Civil Aeronautics Authorities of the Republic of Honduras for aircrafts exported from the United States to Honduras.
b) The following additional documents are requested:
1) Log book for Engines and Propellers Aircraft Maintenance Manual up-to-date and if possible translated to Spanish Language Weight and Balance report not older than six months;
2) Record of engines and propeller major repairs and alterations also from the aircraft i.e., FAA Form 337 [[Major Repair and Alteration]].
Maintenance and estructural reparation Manual Services Bulletin including the last revisions for the aircraft, engines, propeller and spare parts.
A complete list of notes Airworthiness Directives and mandatory Bulletins Services applicable for the aircrait, engines, propellers and spare parts indicating the correct method of compliance asaid bulletins, signature of the individual licence and certificate number.
3) The products Class II and III should be exported in accordance with the provisions prescribed on the Part 21 of the Federal Aviation Regulations.
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HONG KONG - SPECIAL REQUIREMENTS (New March 14, 1977) The territory of Hong Kong has the status of a British Crown Colony under the United Kingdom. when exporting aeronautical products to Hong Kong, the Special Requirements of the United Kingdom (appendix 2 [[of this advisory circular]]) should be similarly observed.
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REPUBLIC OF INDIA - SPECIAL REQUIREMENTS [[Reprinted from AC 21-2F dated August 7, 1987]] When an aircraft/engine/component exported to India is the first of a model, the manufacturer must supply to the Director General of Civil Aviation the following documents and subsequent revisions:
Copies of type certification documents and relevant drawings, specification, etc.
b. Two sets of maintenance manuals.
c. Two sets of overhaul/shop manuals.
d. Two sets of engine operations manuals.
e. One set of flight manuals, if applicable.
f. One set of repair manuals.
Two sets of Service Bulletins and subsequent new issues in addition to revisions.
h. Recommended maintenance schedules.
2. The exporter must show evidence that the products or parts thereof were manufactured under one or more of the following approvals, unless otherwise approved by the Government of India, Director General of Civil Aviation:
a. The current valid FAA Production Certificate for the product involved, as outlined in Subpart G of Part 21 of the FAR.
b. An FAA-Approved Production Inspection System (FAA-APIS) letter of approval, as stated in Subpart F of Part 21 of the FAR.
c. An FAA Replacement and Modification Parts Manufacturers Approval (FAA-PMA) letter of approval issued by the FAA in accordance with Subpart K of Part 21 of the FAR. In this case, each part (or package of small parts) must be marked with the symbol "FAA-PMA" tc indicate approval. In addition, each part (or package or small parts) must be marked with the company's name (or trademark), the part number, and the make and model of the type certificated product on which the part is eligible for installation. The make and model information may be on a tag attached to the part (reference FAR 45.15 and FAA Advisory Circular No. 21.303-1A).
A Technical Standard Order (TSO) acknowledgement or authorization letter, issued by the FAA per FAR Part 21, Subpart O, or those airworthiness parts of the FAR relative to the products involved.
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3. Reconditioned, used, or surplus parts must be accompanied by a certification statement signed by an FAA certified repair station holding a currently valid approval certificate, or by a certified aircrait and powerplant mechanic, as provided for under FAR Parts 145 and 65, respectively. The return to service maintenance records required by FAR 43, appendix B, shall accompany the parts.
• In all instances, suppliers must certify on the face of their solved was ic factured under of their of the following procedures; i.e., FAA PC No. invoice that the product involved was manufactured under one or more _; TSO No.; FAA-APIS letter dated ¡ FAA-PMA letter dated _; SAE No.
¡ MIL Spec. other Government or Industrial Specifications 72
Appendix 2
REPUBLIC OF INDONESIA - SPECIAL REQUIREMENTS (Revised December 1, 1988) SECTION 1 INTRODUCTION. The development of aviation in Indonesia in the last few years dictates the special requirements as stated in FAA Advisory Circular AC 21-2E, dated May 18, 1981, need be revised as follows:
A. Administration and Procedures.
(1) The procedures which must be followed to obtain Indonesian Certification are dealt within the current issue of Civil Aviation Safety Regulations Part I.
(1) Aircrait and other Class I products, to be eligible for export to indonesia, should be covered by Export Certificate oi Airworthiness issued under Part 2l of the United States Federal Aviation Regulations.
(3) An Export Certificate of Airworthiness and the supporting data and other material required to be furnished in accordance with these requirements should be delivered to the Directorate General of Air Communications, Jalan Angkasa I No. 2, Jakarta, P.O. Box 389, Indonesia.
(4) The Export Certificate of Airworthiness shall be accompanied by documents (e.g., aircrait logbook, engine logbook, ament) furnished propeller logbook, etc.) furnished by the applicant, which contains entries identifying those applicable Airworthiness Directives (AD's) with which compliance has been achieved. These documents shall also identify those AD's containing repetitive compliance requirements, and when next compliance is due to be satisfied. All AD's must have been complied with, prior to issuance of the U.S. Export Certificate of Airworthiness.
(5) The applicant for a U.S. Export Certificate of Airworthiness is also responsible for satisfying all other Indonesian sections of FAR 21, before the U.S. Export Certiticate of Airworthiness can be issued.
B. Delivery of Aircraft.
(1) In addition to the requirements stated in the Special Requirements (identified in Section 2), an aircrait which is being exported to Indonesia via flyaway should display Indonesian Nationality and Registration Marks and carry the following documents onboard the aircraft during delivery flight:
(i) Indonesian Certificate of Registration.
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(ii) Indonesian Delivery Flight Authorization.
(iii) U.S. Export Certificate of Airworthiness.
(iV) Signed copy of telegram to Jakarta referred to in paragraph B(3) of this section.
Certificate of Deregistration or written statement certifying that the aircraft has never been registered in USA, issued by FAA.
(vi) Letter of authority to cover the use of installed radio apparatus for the duration of the delivery flight.
(vii) Approved flight manual, operation manual, maintenance manual, and such other documents as may be essential to the safe operation of the aircraft.
(2) It will be the responsibility of the Indonesian and carried in the aircraft during the delivery flight.
(3) The Directorate General of Air Communications, Jakarta, should be advised by telegram of the issuance of an Export Certificate of Airworthiness in respect of any aircraft which is to be exported to Indonesia via flyaway.
Advance notification by telegram of the following particulars is required in respect of each aircraft being exported by flyaway;
reference number of the Export Certificate of Airworthiness being issued; the subject aircraft type; serial number; and assigned Indonesian identification markings.
The telegram shall be transmitted to the Director General of Air Communications, Jakarta (cable address: Civilair, Jakarta-Indonesia;
relex 49482 CIVAIR IA; Fax No. 62-21-420-4268) by the exporter. Ir addition, a telegram pertaining to the cancellation of the aircraft from the United States Aircraft Register, shall be transmitted to the same address.
The responsibility for sending these telegrams, cables and/or Facsimile messages and any expense involved lies with the exporter.
(4) An aircraft which is being exported to Indonesia other than via ilyaway, the following documents shall be delivered to the Director General of Air Communications, Jalan Angkasa 1 No. 2, Jakarta, P.O. Box 389, Indonesia.
(i) Export Certificate of Airworthiness.
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(ii) Letter certifying that the U.S. registration of the aircraft has been canceled from the state registry/exporting state.
(5) An aircraft to be operated in Indonesia must be equipped with:
(i) HF Communication (Ref. CASR Part 42).
(ii) Emergency Locator Beacon for Aircraft (Rei. DGAC Decision Letter No. SKEP/982/IV/1977 dated April 22, 1977).
(iii) ATC Transponder
(iv) All turbine engine powered aircraft with:
- MTOW of more than 20,000 kg should be equipped with Flight Data Recorder
- MTOW of more than 27,000 kg should be equipped with Cockpit Voice Recorder.
Ref. DGAC Decision Letter No. SKEP/112/VI/1979 dated June 18, 1979.
SECTION 2 SPECIAL - REQUIREMENTS. The following identifies those special administrative requirements which must be satisfied at the time of export for a particular product/aircraft to be eligible for Indonesian Registration Certification and/or Airworthiness validation.
The following documents and data should be delivered to the Director General of Air Communications, Jakarta, Indonesia:
A. New Aircraft.
Statement of Build Standard. This statement to include the aircraft specification, differences from previously accepted aircraft on the Indonesian Register (as required by indonesian Special Conditions) and a list of Service Bulletin's 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.
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(iii) Service Bulletin Compliance.
(iv) Alert Service Bulletin Compliance.
(3) Export Certificate of Airworthiness. Included with the Certificate must be a clear statement of those Indonesian Special Conditions which have been complied with, as well as a statement of those conditions for which compliance has not been shown.
(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.
(6) A list of defects to be rectified by the Indonesian Operator at the time of issue of the Export Certificate of Airworthiness, if any.
(7) Engine/airframe/propeller/APU logbooks.
(8) MRB program, where applicable.
(9) Time/life limitations.
* (10) Electrical load analyses.
* (11) Minimum equipment list.
* (12) Wiring diagram.
(13) Weight schedule and weighing report.
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(14) Manuals: Number Required * (i) Flight Manual. 2 Or * (ii) Maintenance Pilot Operating Handbook.
* (iii) Operations.
* (iv) Weight and Balance, Loading Procedures.
(V) Overhaul.
* (vi) Structural Repair.
* (vii) Component Overhaul.
*(viii) Engine Maintenance and Overhaul.
(ix) Standard practices.
* (X) NDT • * (xi) Structurally significant items.
* (xii) Maintenance Planning Guide.
*(xiii) Parts Catalogue. 1 * (15) One copy of the flight test report.
(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 (14) (xiii).
* NOTE: Required only with first aircraft of a particular type and model exported to Indonesia.
B. USED AIRCRAFT. In addition to the information referred to above, the following requirement is also required for used aircraft to be imported into Indonesia.
A used aircraft shall have a service history acceptable to the Directorate General of Air Communications.
2. The aircraft shall be made available to the Directorate General of Air Communications for survey at a suitable time and for such period as necessary prior to certification.
3. The aircraft shall be prepared to permit access to its structure, control system, equipment and installation, and such tests and checks as required by the Directorate General of Air Communications shall be performed.
4. All Airworthiness Directives (mandatory modifications and inspections) issued by the State of Manufacturer and/or the State of 77
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5. An up-to-date record of modifications and service bulletins embodied shall be produced.
6. The following documents must be supplied:
(i) Documents relating to deregistration of the aircraft from previous register of the State of Registry.
(ii) Legal documents relating to previous ownership of the aircraft.
(iji) Documents relating to change of ownership, purchase contract, etc.
(iv) Log book or equivalent records for the aircraft, engines and propellers (if applicable).
(v) Aircraft Acceptance Flight Test Report.
7. The following minimum information shall be supplied in respect of each used aircraft for which a Certificate of Airworthiness is applied:
(i) The total airframe hours since manufacture.
(ii) The total number of landings.
(iii) The total number of cabin pressurization cycles and the pressure to which the cabin has been subjected during its life.
(iv) A statement describing the post operational life and uses of the aircraft, including any special mission role.
(v) A record of all major structural component changes such as those of wings, tailplane, etc., and the individual history of such components.
(vi) A record of all time-controlled items, including details of service life remaining and modification standards.
(vii) A record of last overhaul or major check carried out.
(viii) A record of all major repairs, including the nature of the damage in each case, e.g., corrosion, cracking, accidental damage, etc.
(ix) A record of aircraft accidents, if any.