AC 21-2B Appendix 2 10/2/69 Page 45 Manufacturer Model Manufacturer Model CESSNA 150C GRUMMAN AGCAT G 164 A 150E P&W R 985-An-I 150F (450 hp) 150G Ham.Std.6101-A-12 172 172A N.A.AVIATION AT-6 172฿ 172E HUGHES 269B 172F LOCKHEED L-188C 172G 182B 182F I-1049G L-1049H A188 MOONEY M-20A P206 U206A PIPER J3C-65 (L-4J) CONVAIR 640 PA-18-125 PA-18A-135 DOUGLAS DC-3C-S1C-3G PA-18-150 C54B-DC PA-18A-150 DC -6 PA-19 DC-6A PA-22-108 DC-6B PA-22-150 DC-7C PA-22-160 DC-8-33 PA-23-160 DC-8-53 PA-23-235 DC-8-55 PA-24-250 DC-8F-55 PA-25-235 DC-8-63 PA-28-140 DC-9-15 PA-28-160 DC-9-32 PA-28-180 DC-9-33F PA-30 ERCOUPE 415-D SIKORSKY S-61 N S-62 A FAIRCHILD 24R 46 A STINSON L-5B
Appendix 2 AC 21-2B CHG 1 Page 46 11/13/70
KINGDOM OF THE NETHERLANDS - SPECIAL REOUIREMENTS NETHERLANDS ANTTLLES
1. General. The special conditions associated with the Exchange of Notes between the United States and the Kingdom of the Netherlands of September 19 and November 4, 1955, relating to the reciprocal validation of export certificates of airworthiness for aircraft are prescribed below.
These conditions apply only to export of aircraft to the Netherlands Antilles.
The aircraft, in addition to the requirements prescribed in Part 21 of the United States Federal Aviation Regulations, must be eligible for certification in the "standard" classification. This excludes "restricted," "limited," and "experimental" aircraft, except on an individual basis after referral to the Department of Civil Aviation, Netherlands Antilles (Department van Luchtvaart Nederlandse Antillen (D.V.L. N.A.)) (See Note 6a.)
b. Aircraft with a certification basis older than March 5, 1952, and being of a type which had no Netherlands Antillean airworthiness approval during the last six years, are excluded from import into the Netherlands Antilles except on an individual basis after referral to the D.V.L. N.A.
Without prejudice to the foregoing, aircraft types, the United States Export Certificates of Airworthiness of which were validated by the D.V.L. N.A. prior to July 1, 1967, may continue to be imported on a similar basis to that agreed for previous aircraft of the identical type. An aircraft is considered of an identical type if the changes are none or only minor and do not reduce previously accepted airworthiness standards. The types of aircraft referred above are as follows:
Manufacturer Model Manufacturer Model Aero Commander 100 Curtiss Wright Super C-46 Beech C-50 Dornier DO 28A-1 D 50 B 65-A80 Fokker F 27-500 Cessna 150 H McDonnel Douglas DC9-15 172 C Mooney M20-5 172 H 172 I de Havilland DHC -6 175 c Piper PA 23-160 182 E PA 28-160 182 M PA 28-180 PA 22-150 Convair 340 J-3
AC 21-2B CHG 1 Appendix 2 11/13/70 Page 46-1
2. DOCUMENTS AND DATA REQUIRED. The following documents and data shall be submitted to the D.V.L. N.A.
a. For all aircraft.
(1) Certificate of airworthiness for export issued not more than 60 days prior to the application for validation.
(2) FAA approved Airplane Flight Manual and weight and balance report with equipment list.
Certificated aircraft and engine logbooks, and when available propeller logbooks, or other equivalent historical records
(4) A certified statement regarding any flight or operational limitations, exemptions, or restrictions, which may have been prescribed by the FAA, because of design or structural characteristics or features incorporated which are not in conformity with data forming the basis for the initial type certification of aircraft of this type.
(5) A certified statement regarding the modification status of aircraft with respect to airworthiness directives or other changes prescribed by the FAA subsequent to issuance of the original type specification or type certificate for the aircraft. Major repair and alteration form, F.A.A, Form 337, or equivalent, if repairs and/or alterations have been accomplished on the exported aircraft.
b. For Aircraft being the First of a Type Exported to the Netherlands Antilles (See Note 6c). In addition to the documents and data mentioned in the preceding paragraph the following documentation and data shall in general be submitted: (The D.V.L. N.A. will inform on request regarding such of the listed documents and data as may be required in each specific area.)
(1) Manuals related to aircraft. The Maintenance Manual, Overhaul Manual, Repair Manual, Parts Catalog, and a copy of the customer's specification for the aircraft, together with a specimen copy of the approved Airplane Flight Manual. A copy of information or instructions essential to the assembly and rigging of the aircraft.
(2) ' Manuals related to major parts. The approved Operating Manual, Maintenance Manual, Overhaul Manual, and Repair Manual for each type of engine, propeller, and major auxiliarly equipment fitted to the aircraft. A list of communications equipent
Appendix 2 AC 21-2B CHG 1 Page 46-2 11/13/70 installed, including model, capacity, frequency, operating instructions, etc.
NOTE: If possible, the documents specified in (1) and
(2) shall be delivered well in advance of the intended delivery date of the aircraft.
(3) Bulletins. A complete set of service publications including bulletins issued by the manufacturers of the aircraft and by the manufacturers of engines, propellers and other type certificated equipment installed thereon, and a statement by an authorized representative of the aircraft manufacturer to the effect that he will undertake to supply the D.V.L. N.A. with a copy of all new such bulletins.
(4) Design and test data. The design data and test data listed in Annex A (see Note 6b.)
3_ TECHNICAL REQUIREMENTS.
a. The aircraft shall to the extent deemed essential by the D.V.L. N.A.
comply with such additional requirements as may be specified in writing. These additional requirements will be determined having regard to the differences between the relevant airworthiness codes of the United States and the Netherlands, and to any additional requirements as would be prescribed for comparable aircraft in the Netherlands.
Unless otherwise stated the conditions listed in Annex B apply (See Note 6b).
4. USED AIRCRAFT. For each used aircraft the D.V.L. N.A. will after inspection of the aircraft establish on the basis of their findings and on the basis of the maintenance records of the aircraft, the phase in the D.V.L.
N.A. approved maintenance schedule from which this schedule must be followed and the additional maintenance to be performed for this phase of the maintenance schedule.
5. FLY-AWAY AIRCRAFT.
& . In the case of aircraft delivered via flyaway, the export certificate of airworthiness, certified logbooks, FAA approved Airplane Flight Manuals, weight and balance report and equipment list and such other documents as may be essential to the safe operation of the aircraft, shall accompany the aircraft and be delivered to the D.V.I. N.A. on arrival in the Netherlands Antilles.
AC 21-2B CHG 1 Appendix 2 11/13/70 Page 46-3 If delivery of an aircraft is via fly-away, the aircraft shall carry certificates of airworthiness and registration and a letter of authority to cover the use of radio, valid for the delivery flight, issued by the D.V.L. N.A. All inquiries relating to the issuance of Netherlands Antilles certificates of registration and certificates of airworthiness should be addressed to the D.V.L. N.A.
6. NOTES.
The address of the Department of Civil Aviation:
Department van Luchtvaart Dr. A. Plesman Luchthaven Curacao, Nederlandse Antillen.
b. Annexes A and B are available from the D.V.L. N.A.
c. The D.V.L. N.A. will inform on request whether an aircraft is the first of a type to be exported to the Netherlands Antilles.
Appendix 2 AC 21-2B 10/2/69
NEW ZEALAND - SPECIAL REQUIREMENTS
1. Aircraft to be eligible for export to New Zealand, in addition to the requirements prescribed in Part 21 of the United States Federal Aviation Regulations, must comply with these special requirements.
2. Aircraft which are certificated only in the restricted category will not be considered as eligible for registration or airworthiness certification in New Zealand, and export certificates of airworthiness issued to such aircraft will not be validated by that Government. Any modifications to aircraft initially designed to comply with requirements for type certification in the normal, utility, acrobatic or transport categories must be approved on the basis of requirements contained in the regulations for those categories, as applicable, to be eligible for certification in New Zealand.
3. Export certificates of airworthiness and other forms and supporting data relating to aeronautical products exported to New Zealand shall be forwarded to the Director of Civil Aviation, Air Department, Civil Aviation Branch, Wellington C.l, New Zealand. This material shall include logbooks or other historical records relating to aircraft or engines exported.
4. An export certificate of airworthiness is required in connection with any Class 1 product exported from the U.S. to New Zealand. Class Il and Class Ill products to be eligible for approval and installation on certificated civil aircraft of New Zealand registry, should be exported in accordance with the applicable provisions of Part 2l of the United States Federal Aviation Regulations.
5. If an aircraft is the first- of a model to be exported to New Zealand, the following material will be furnished:
a. An export certificate of airworthiness (required with all Class I products).
b. A three-view general arrangement drawing of the aircraft.
c. A certified copy of the complete drawing list (quoting latest issue numbers issued by the manufacturer).
d. A basic load report giving a summary of the design loads, materials, and reserve factors for each member of the primary structure.
e. Evidence of strength of primary structure as ascertained by physical tests of calculations (stress analysis or static test reports acceptable) 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 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