AC 21-2B CHG 1 Appendix 2 11/13/70 Page 65
ZAMBIA, REPUBLIC OF - SPECIAL REQUIREMENTS
1. GENERAL.
8 - Any aircraft, to be eligible for the issue of a Certificate of Registration issued by the Government of the Republic of Zambia, must qualify for certification in the United States of America in the standard or restricted category, and an Export Certificate of Airworthiness, FAA Form 8130-4, should have been 1ssued in accordance with Part 21 of the United States Federal Regulations.
b. Class 2 and Class 3 products should be accompanied by documentation which conform that the item is in accordance with the relevant section of Part 21 of the United States Federal Aviation Regulations.
An Airworthiness Approval Tag, FAA Form 8130-3 is acceptable, If the aircraft is to be entered on the Zambia Register of Civil Aircraft prior to departure from the United States of America, the Importer will make application to the Zambian Department of Civil Aviation for the necessary Certificate of Registration, Permit to Fly and Radio Station License, which must be carried during the delivery flight.
d. Enquiries should be addressed to the Director of Civil Aviation, P. O. Box RW 137, Ridgeway, Lusaka, Zambia, marked for the Attention of the Chief Aircraft Inspector.
2. AIRCRAFT FIRST OF THE TYPE TO BE REGISTERED IN THE REPUBLIC OF ZAMBIA.
The following documents and data are required;
a. Complete set of maintenance and overhaul manuals, and parts catalogues, for:
(1) Airplane.
(2) Engine (s)
(3) Propeller (s)
(4) Any equipment not already installed in an aircraft on the Zambian Register of Civil Aircraft.
b. Full set of Service Bulletins, Letters, and Modification Leaflets issued by the manufacturers in respect of the airframe, engine (s), propeller (s), and installed equipment.
c. A copy of the Type Certificate, if not already held by the Department, *
Appendix AC 21-2B CHG 1 Page 66 11/13/70
d. Three copies of the flight manual for the aircraft.
e. One copy of the production flight test report issued by the manufacturer.
3. EACH AIRCRAFT FOR WHICH A ZAMBIAN CERTIFICATE OF AIRWORTHINESS IS TO BE REQUESTED. The following documentation is required:
A statement, signed by an official representative of the manufacturers, showing that all mandatory modifications and special inspections have been complied with.
b. The Export Certificate of Airworthiness, FAA Form 8130-4.
c. Two copies of the Approved Flight Manual.
d. Two copies of the Weight & Balance report showing the weights and * arms of the main components, and a list of installed equipment.
AC 21-2B CHG 1 Appendix 11/13/70 Page 1 FAA Regional Offices Responsible for Civil Aviation Matters in Foreign Countries Country or Area
a. Canada
b. Caribbean Area, South America Central America, (excluding Mexico) Panama, and the Canal Zone
c. Mexico
d. Area East of East Pakistan and India, including all free nations south and east of China
e. Europe, Africa, Middle East west of Burma, Iceland Greenland, and Bermuda FAA Regional Office Address Federal Aviation Administration Federal Building John F. Kennedy International Airport Jamaica, New York 11430 Federal Aviation Administration P. 0. Box 20636 Atlanta, Georgia 30320 Federal Aviation Administration P. O. Box 1689 Fort Worth, Texas 76101 Federal Aviation Administration P. O. Box 4009 Honolulu, Hawaii 96812 Federal Aviation Administration Tour-Madou Building 1 Place Madou Brussels 3, Belgium
AC 21-2B CHG 1 Appendix 4 11/13/70 Page 1 * COUNTRIES WITH WHICH THE UNITED STATES HAS
CONCLUDED AGREEMENTS FOR RECIPROCAL
ACCEPTANCE OF AIRWORTHINESS CERTIFICATES The agreements with the following countries are valid for aircrait, aircraft engines, and propellers, and for spare parts for aircraft, aircraft engines, and propellers which have been exported under the terms of the agreements. (Note: The agreement with Japan also includes appliances and spare parts for appliances exported under the terms of the agreement).
a. Australia
b. Austria
c. Israel
d. Japan
e. Switzerland
2. The agreements with the following countries are valid only for aircraft, and components of aircraft exported under the terms of the agreements:
8. Belgium
b. Canada
c. Denmark
d. France
e. Germany, Federal Republic of £. Italy Netherlands
h. Norway South Africa, Republic of } - Spain
k. Sweden
1. United Kingdom
3. The agreements with the following countries are valid for gliders only and spare parts for gliders exported under the terms of the agreements:
a. Finland *
b. Poland U. S. GOVERNMENT PRINTING OFFICE: 1970 O - 410-605
CHANGE AC NO: 21-28 CHG 2 DATE: 8 Feb 71
FEDERA IATION ADVISORY
TAMINISTRATOS CIRCULAR
DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION SUBJECT: EXPORT AIRWORTHINESS APPROVAL PROCEDURES PURPOSE. This change transmits revised pages to AC 21-2B dated 10/2/69.
CHANGES. Appendix 2 18 revised to delete "Except as provided" through to 'Inspection Manual" and addition of a NOTE insert. Correction was made on page 37 due to a typographical error.
PAGE CONTROL CHART Remove Pages Dated Insert Pages Dated Appendix 2 Appendix 2 9 and 10 10/2/69 2/8/71 10 10/2/69 37 and 38 10/2/69 37 2/8/71 38 10/2/69 Acting Director, Flight Standards Service Initiated by: FS-180
AC 21-2B CHG 2 Appendix 2 8 Feb 71 Page 9
CANADA - SPECIAL REQUIREMENTS
1. Aircraft, to be eligible for export to Canada, in addition to requirements prescribed in Part 21 of the United States Federal Aviation Regulations, must comply with applicable special requirements prescribed below. It should be noted that the Department of Transport will accept for certification in Canada only those aircraft which are eligible for U.S. certification as "atandard" aircraft. This excludes "restricted," "limited," and "experimental" aircraft, except on an individual basis, after referral to the Canadian DOT.
* NOTE: USED AIRCRAFT imported from the United States without an Export Certificate of Airworthiness may obtain a Canadian Certificate of Airworthiness when the requirements of Part I, Chapter II, paragraph 2.9 of the Canadian Department of Transport Engineering Manual have been complied with.
a. An aircrait exported to Canada, except as indicated in paragraph b, below, shall not have been flown for any purpose other than that required to accomplish the manufacturer's production flight test, and such time as may be involved in effecting delivery flights.
b. USED AIRCRAFT may be exported to Canada, provided that such aircraft comply with the export certification standards and requirements in Part 21 of the United States FARS, are certificated in the standard classification, and provided such aircraft are accompanied by current historical records or logbooks applying to the aircraft and engine (s).
This will include surplus military aircraft which have been investigated and type certificated by the FAA, for which a covering FAA aircraft specification or type certificate data sheet has been issued.
c. At least one portable fire extinguisher of an approved type, accessible to the pilot and to the copilot, will be installed in each aircraft exported to Canada.
d. For skiplanes designed to requirements other than those contained in FAR 23 (excluding skiplanes which have been designed to the Canadian ski gear requirements), the structure should be designed for a limit torque load of .667W or the supplementary skiplane conditions specified in FAR 23. In using the torque load condition of .667W, the ultimate factor of safety shall be 1.5.
e, An export certificate of airworthiness will be required by the Canadian Government in connection with any Class I product which is exported from the U.S. to Canada. Class II and Class III products exported to Canada will be processed in accordance with the provisions contained in Part 2l of the United States FARS.
I. ixport certiiicates or airworthiness, with pertinent data attached, whether issued to cover a complete aircraft, engine, propeller, or other Class I product, will be forwarded by the exporter direct to the Regional Director having surveillance over the Region in which the Canadian purchaser resides. In order that the exporter may comply with this requirement with respect to any Class I product which is shipped to its
Appendix 2 AC 21-2B Page 10 10/2/69 destination, the Canadian purchaser will inform the exporter regarding the specific region in which he resides, concurrent with the conclusion of the purchase contract. Additional requirements relating to an aircraft which is delivered via flyaway to its destination are contained in paragraphs g. and h. below. The complete addresses of the six Regional Offices of the Canadian Department of Transport (CDOT) are listed at the conclusion of these requirements.
In addition to the data forwarded to the Regional Office (Regional Director, Air Services), the following material should accompany the aircraft, or otherwise be delivered to the Canadian purchaser:
(1) One copy of the weight and balance report.
(2) One copy of each of the aircraft flight manual, operating manual, repair and overhaul manual, maintenance and service manual, loading chart, and service bulletins, when such material would be required and furnished if the aircraft in question were certifiwhen in fir standard category as an aircraft of U.S. registry. aircrait of a model is exported into Canada, it 1s required that the manufacturer supply the CDOT with eight copies of the pertinent manuals and service bulletins.
(3) One copy of the manufacturer's production flight test report with respect to new aircraft which are exported by the manufacturer.
(4) Evidence of transfer of title to the foreign purchaser from the last U.S. recorded owner, or the exporter.
h. Prior to departure from the exporter's base, an aircraft which 16 being exported to Canada via flyaway shall display Canadian nationality and registration markings, and shall have installed therein a temporary Canadian certificate of registration and airworthiness, and a letter of authority to cover the use of radio, if installed, valid for the delivery flight involved.
2. The Canadian nationality and registration markings, the certificates of registration and airworthiness, and the letter authorizing the use of a radio will be obtained by the Canadian purchaser from the Regional Director, Air Services, of the region in which he resides. To obtain these, the Canadian purchaser will advise the Regional Director involved regarding the name and address of the vendor (exporter), and regarding the make, model, and serial number of the aircraft being purchased, and whether a radio 16 installed in the aircraft. The Canadian purchaser or the Regional Office involved will advise the United States exporter of the 1/When in doubt as to whether an aircraft is the first of a model, contact the air authority of the importing country.
AC 21-2B CHG 2 Appendix 2 8 Feb 71 Page 37
(1) One copy each 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 or data contained in the type flight test report including weight and balance report applicable to the particular aircraft,
(3) Certified aircraft, engines, and propellers logbooks or other equivalent historical records showing total operating time and time since last overhaul.
3. If the aircraft is to be exported via flyaway to Japan without U.S.
nationality and marking, the manufacturer or exporter should display on the aircraft Japanese nationality and registration markings and should install in the aircraft Japanese certificate of registration and Japanese certificate of airworthiness. Upon application of the purchaser, Civil Aviation Bureau of Japan will 1ssue nationality and registration markings, certificate of registration and certificate of airworthiness when the Japanese importer or the U.S. exporter furnishes Civil Aviation Bureau of Japan the following information:
a. Make and model of the aircraft.
b. Serial number of the aircraft.
c. Purchaser's name and addreas.
d. U.S. exporter's name and address.
e. Document which certifies transfer of ownership of the aircraft together with date of transfer.
f. Document which certifies airworthiness of the aircraft (Export * Certificate of Airworthiness, FAA Form 8130.4). If the certificate itself 18 not available, submit its ip" number.
4. After the Civil Aviation Bureau of Japan receives the foregoing application and information, the Japanese registration markings will be sent as soon as possible to the place where the aircraft is located and Japanese registration and airworthiness certificates 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.
Appendix 2 AC 21-2B Page 38 10/2/69
KOREA - SPECIAL REQUIREMENTS
1. To be eligible for certification by the Government of the Republic of 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.
Export certificates of airworthiness and other related data should be forwarded to the Korean purchaser, inasmuch as the Civil Aviation Authority of the Republic of Korea requires that the applicant (Korean purchaser) shall submit to the authority such subatantiating evidence as may be necessary to establish airworthiness and eligibility for registration and certification by the Republic of Korea.
3. In addition to the foregoing, the following materials will be furnished for aircraft to be exported to Korea.
a. If the aircraft is the first model exported to Korea, the following material shall be furnished.
Three (3) copies of each parts catalog; operating, overhaul, maintenance (including maintenance schedule) and repair manuals applying to the aircraft, engines, propellers and major ancillary equipment installed on the aircraft, NOTE: If possible the documents specified in (1) shall be delivered well in advance of the intended delivery date for the aircraft.
(2) One copy each of approved flight manual and the manufacturer's production flight test report including the weight and balance report applicable to the aircraft.
(3) A certified copy of the complete drawing list.
(4) A type record or atress analysis summary showing, for all members of the primary structure, their design loads, dimensions, materials strength and margins of safety, or a copy of the static strength teat reports when type approval was granted on the basis of such tests.
(5) A statement by an authorized representative of the manufacturer to the effect that all pertinent information, modification, service bulletins and revisions to such bulletins will be automatically distributed to the Civil Aviation Authority of the Republic of Korea.
GP 0 904.282