Appendix 2
(2) with a certification basis older than January l, 19/6, and being of a type which had a Netherlands airworthiness approval before January 1, 1978, are excluded from import to the Netherlands on or after January 1, 1980, and except on an individual basis after referral to the RLD.
TABLE I Manufacturer Model Manufacturer Model G. AGUSTA - BELL AB.206A ERCOUPE 415-D BEECH D18S FAIRCHILD 24R 46 A 23 GRUMMAN AGCAT G 164 A 65 P&W R 985-An-1 65-80 (450 hp) 65-90 Ham. Std. 6101- 95-A55 A-12 BELL 47G N.A. AVIATION AT-6 47G-2A-1 47J HUGHES 2698 47J-2A LOCKHEED L-1880 BOEING 707-355C L-1049C CESSNA L-1049H MOONEY M-20A PIPER J3C-65(L-4J) PA-18-125 PA-18A-135 PA-18-150 PA-18A-150 PA-19 PA-22-108 PA-22-150 PA-22-160 PA-23-160 PA-23-235 PA-24-250 PA-25-235 PA-28-140 PA-28-160 105
Appendix 2 Manufacturer Model Manufacturer Model CONVAIR 640 PA-28-180 DOUGLAS DC-3C-S1C-3G PA-30 C54B-DC DC-6 SIKORSKY 5-61 N DC -6A S-62A DC-6B DC-7C STINSON L-5B DC-8-33 DC-8-53 DC-8-55 DC-8F-55 DC-8-63 DC-9-15 DC-9-32 DC-9-33F 106
8/7187 AC 21-2F Appendix 2
NETHERLANDS ANTILLES - SPECIAL REQUIREMENTS 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.
a. 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 6а).
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.
c. without prejudice to the foregoing, aircraft types, the United States Export Certificates of Airworthiness of which were valicated by the D.V.L. N.A.
prior to July 1, 1967, may continue to be imported on 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 MCDONNELL 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 28-180 182 M PA 22-150 J-3 CONVAIR 340
2. DOCUMENTS AND DATA REQUIRED. The following documents and data shall be submitted to the D.V.L. N.A.
Appendix 2
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.
(3) Certificated aircraft and engine logbooks, and when available propeller logbooks, or other equivalent historical records showing total operating time.
(4) A certified statement regarding any flight or operational limitations, exemption, or restrictions, which 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, FAA Form 337, or equivalent, 1f repairs and/or alterations have been accomplished on the exported aircraft.
b. For aircraft being the first of a type exported to the Netherlands Anties (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. wil] inform on request regarding such of the listed documents and data as may be required in each specific area.)
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 auxiliary equipment fitted to the aircraft. A list of communications equipment 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 manufacturers 108
Appendix 2 of engines, propellers and other type certificated equipment installed thereon, and a statement by an authorized representative of the aircraft manufacturer to bulletins. the effect that he will undertake to supply the D.V.L. N.A. a copy of all new such
(4) Design and test data. The design data and test data listed in Annex A (see Note 60.).
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 between the relevant airworthiness codes of the United States and the Netherlands, additional requirements will be determined having regard to the differences in the Netherlands. and to any additional requirements as would be prescribed for comparable aircraft
b. Unless otherwise stated the conditions listed in Annex B apply (See Note 6b.).
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. FLYAWAY AIRCRAFI.
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.L. N.A. on arrival in the Netherlands Antilles.
b. If delivery of an aircraft is via flyaway 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.
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.
NOTES.
a. The address of the Department of Civil Aviation:
Department van Luchtvaart Dr. A. Plesman Luchthaven Curacao, Nederlandse Antillen 109
Appendix 2
b. Annexes A and B are available form 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.
8/7/87 AC 21-2F Appendix 2
DOMINION OF
NEW ZEALAND - SPECIAL REQUIREMENTS (Revised January 6, 1976) SECTION 1 - INTRODUCTION.
An Export Certificate of Airworthiness with pertinent data attached will be required for each Class I product exported from the United States to New Zealand. To be eligible for installation in New Zealand aircraft, Class Il and Class III products must be processed in accordance with the applicable provisions of FAR 21 Subpart L.
B. Special requirements which must be satisfied before the issue of a U.S.
Export Certificate of Airworthiness are identified in Section 2. The Director of Civil Aviation (Attention: Airworthiness), Ministry of Transport, Private Bag, C. Airworthiness certification procedures of New Zealand aircraft are specified in the New Zealand Civil Airworthiness Requirements Volume I Sections A and B. Application for a New Zealand Certificate of Airworthiness is to be made not later than 28 days before the issue of the certificate is desired.
D. Additional requirements which must be satisfied for the issue of a New Zealand Certificate of Airworthiness, are specified in New Zealand Civil Airworthiness Requirements Volume l Section C and Volume 2. It is not necessary for these additional requirements to be complied with before export from the United States.
E. Aircraft which are certificated only in the United States Restricted Category will not be eligible for registration or airworthiness certification in New Zealand unless special conditions are met.
F. If the airworthiness standards which form the certification basis for the aircraft pre-date the U.S. Civil Air Regulations, the aircraft may be certified in the New Zealand Restricted Category and be ineligible for air transport and aerial work operations.
Supply of data listed in Section 2 D through G may be required in respect alterations before a New Zealand Certificate of Airworthiness is issued.
Copies of MOT 2171 (see Section 2 F) are obtainable from the New Zealand Embassy, 19 Observatory Circle, N.W. Washington, D.C. 20008.
Appendix 2 SECTION 2 - SPECIAL REQUIREMENTS The following identifies those special requirements which must be satisfied at the time of export for an aircraft to be eligible for New Zealand airworthiness certification. The listed data must be supplied to the Director of Civil Aviation:
Statement of Build, Modification and Equipment Standard. To include list of Service Bulletins incorporated in production or subsequently, alterations, customer options, and equipment incorporated including items not necessarily installed by the manufacturer.
B. Engine/airframe log books.
Section 1'opies of any applicable supplemental type certificates (see + D. Three copies of all current service information for the aircraft, its engine(s) and propeller(s), f.e., Service Bulletins, Service Letters and equivalent documents.
+ E. Two copies of each of the following manufacturer's manuals:
(1) Flight manual (when required ) In addition to any by the U.S. regulations for )required to be the aircraft type); ) supplied for each J aircraft under U.S.
(2) Operations (or owners) manual; airworthiness )regulations.
(3) Maintenance;
(4) Overhaul;
(5) Structural repair;
(6) Parts;
(7) Engine operation;
(8) Engine maintenance;
(9) Engine overhaul;
(10) Engine parts;
(11) Propeller maintenance;
(12) Propeller overhaul;
(13) Propeller parts.
Appendix 2 + F. A New Zealand Ministry of Transport form MOT 2171 completed by the aircraft manufacturer. This constitutes an agreement to supply amendments and reissues of the data required under items D and E above.
+ G. One copy of:
(1) Type Certificate Data Sheet;
(2) Basic loads report;
(3) Structural substantiation report;
(4) Structural fatigue substantiation (if required for U.S. type certification);
(5) Type flight test report;
(6) Drawings of major assemblies, installations, and primary structure;
(7) Electrical load analysis;
(8) Minimum equipment list.
Required only with first aircraft of a particular type and model exported to New Zealand.
Appendix 2
ISLAMIC REPUBLIC OF PAKISTAN - SPECIAL REQUIREMENTS Aircraft and other Class I products, to be eligible for registration and airworthiness certification by the Government of the Islamic Republic of Pakistan, should be covered by Export Certificates of Airworthiness as provided in Part 21 of the United States Federal Aviation Regulations. Class II and Class III products, to be eligible for approval and installation on certificated civil aircraft of the Islamic Republic of Pakistan registry, should be exported in accordance with the applicable provision of Part 21 of the United States Federal Aviation Regulations.
Export Certificates of Airworthiness and other related data, as provided for in Part 21, should be forwarded to the Director-General of Civil Aviation, Karachi, the Islamic Republic of Pakistan.
3. Upon application by the prospective purchaser (citizen of the Islamic Republic of Pakistan), the Department of Civil Aviation of the Government of che Islamic Republic of Pakistan:
a. Will assign the Islamic Republic of Pakistan registration letters,
b. Will issue a certificate of registration endorsed: 'Valid only until first landing at customs aerodrome in the Islamic Republic of Pakistan."
c. Will issue an Islamic Republic of Pakistan short-term certificate of airworthiness.
NOTE: To preclude delay in initiating the delivery Tight, the temporary registration and airworthiness certificates referred to above will be forwarded by the Department of Civil Aviation of the Islamic Republic of Pakistan or by the foreign purchaser direct to the exporter, or to the point from which delivery is to be initiated.
Appendix 2
REPUBLIC OF PANAMA - SPECIAL REQUIREMENTS
1. GENERAL following documents and data shall be submitted to the Direccion de Aeronautica Civil. In order to be eligible for certification by the Panama Government the
(1) Class I aeronautical products must be covered by Export Certificates of Airworthiness as provided for in Part 21 of the United States Federal Aviation documents: Regulations. Complete aircraft, new or used, will require the following
(1) Export Certificate of Airworthiness - FAA Form 8130-4.
(11) FAA-Approved Airplane Flight Manual and Weight and Balance Report with Equipment List.
(111) Aircraft and Powerplant(s) Log Books and when applicable propeller Log Books with certified annual inspection (large aircraft will require annual inspection certified by an FAA-approved repair station).
(iv) Major Repair and Alteration Form 337, if repairs and/or alterations have been accomplished on the exported aircraft.
(v) A certified statement that all the airworthiness directives or changes prescribed by the FAA are up-to-date on the exported aircraft.
(vi) A bill of sale notarized by a Panamanian Consul or by one of a friendly nation.
(2) Class II and Class III products shall be exported in accordance with the provisions prescribed in Part 21 of the United States Federal Aviation Regulations.
Appendix 2
REPUBLIC OF THE PHILIPPINES - SPECIAL REQUIREMENTS (Revised - July 1, 1981) The following data shall be forwarded direct by the exporter to the Director of Air Transportation, Manila International Airport, Philippines: antional air bort, I. First of a Model In order to be eligible for certification and registration by the Philippine government, Aircraft and other Class I, II and III products shall be covered by:
a. Applicable provisions of Part 21 of the USFAA regulations, f.e. Export Certificate of Airworthiness.
b. Basis for type certification.
c. Properly certified aircraft, engine and propeller logbooks or equivalent historical records indicating total time operated.
d. A certified statement that all mandatory FAA directives have been complied with.
e. Copy of the manufacturer's production flight test report for the aircraft to be exported.
f. One copy of the weight and balance report pertaining to the particular aircraft including loading schedule or chart, if applicable, and Master Equipment List.
g. One copy of the Approved Flight Manual of the particular type of aircraft.
h. One copy of the assembly and rigging instructions if aircraft is to be assembled at the point of destination.
1. One copy of the pertinent maintenance/service manuals and service bulletins.
j. General arrangement drawing of aircraft.
k. Aircraft design specification.
1. Sale Documents.