Appendix 2 With a certification basis older than January 1, 1976, 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
TABLE I Manufacturer Model Manufacturer Model G. AGUSTA - BELL AB.206 A ERCOUPE 415-D BEECH FAIRCHILD 24R 46 A 23 GRUMMAN AGCAT G 164 A 65 P&W R 985-An-I (450 hp) Ham. Std. 6101- A-12 BELL 47G N.A. AVIATION AT-6 47G-2A-1 47J HUGHES 269B 47J-2A LOCKHEED L~188C BOBING 707-355C Ir1049G CESSNA L~1049H M-20A J3C-65(I-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 79
Appendix 2 Manufacturer Model Manufacturer Model CONVAIR 640 PIPER PA-28-180 DOUGLAS DC-3C-S1C-3G PA-30 C54B-DC DC-6 SIKORSKY S-61 N DC-6A S-62A DC-6B DC-7C DC-8-33 SIINSON L~5B DC-8-53 DC-8-55 DC-8F-55 DC-8-63 DC-9-15 DC-9-32 DC-9-33F 80
5/18/81 AC 21-2F Appendix 2
NETHERLANDS ANTILLES - SPECIAL REQUIREMENTS
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.
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 Luchtvarrt 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 trom 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 validated 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.I. 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, 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 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 82
5/18/81 AC 21-2E Appendix 2 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. 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.
b. 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. FLYAWAY 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.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. 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.
a. The address of the Department of Civil Aviation:
Department van Luchtvaart Dr. A. Plesman Luchthaven Curacao, Nederlandse Antillen 83
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 aircrait is the first of a type to be exported to the Netherlands Antilles.
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 II 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 befort 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, Wellington, New Zealand.
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 1 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.
G. Supply of data listed in Section 2 D through G may be required in respect of SIC alterations before a New Zealand Certificate of Airworthiness is issued.
H. Copies of MOI 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 - SPECTAL REQUIREMEVIS 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:
A. 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.
C. Copies of any applicable supplemental type certificates (see Section 1 G).
+ D. Three copies of all current service information for the aircraft, its engine(s) and propeller(s), i.e., Service Bulletins, Service Letters and equivalent documents.
+ E. Two copies of each of the following manufacturer's manuals:
(1) Flight manual (when required by the U.S. regulations for the aircraft type);
(2) Operations (or owners) manual;
(3) Maintenance;
(4) Overhaul;
) In addition to any ) required to be ) supplied for each ) aircraft under U.S.
) airworthiness ) regulations.
(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 MOI 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 equigment list.
Required only with first aircraft of a particular type and model exported to New Zealand.
Appendix 2
REPUBLIC OF PAKISTAN - SPECIAL REQUIREMENIS
1. Aircraft and other Class I products, to be eligible for registration and airworthiness certification by the Government 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 Pakistan registry, should be exported in accordance with the applicable provision of Part 2l of the United States Federal Aviation Regulations.
2. 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, Pakistan.
3. Upon application by the prospective purchaser (citizen of Pakistan), the Department of Civil Aviation of the Government of Pakistan:
a. Will assign Pakistan registration letters,
b. Will issue a certificate of registration endorsed: "Valid only until first landing at customs aerodrome in Pakistan."
c. Will issue a Pakistan short-term certificate of airworthiness.
NOTE: To preclude delay in initiating the delivery flight, the temporary registration and airworthiness certificates referred to above will be forwarded by the Department of Civil Aviation of Pakistan or by the foreign purchaser direct to the exporter, or to the point from which delivery of the aircraft is to be initiated.
AC 21-2E 5/18/81 Appendix 2
REPUBLIC OF PANAMA - SPECIAL REQUIREMENTS 10 GENERAL In order to be eligible for certification by the Panama Government the following documents and data shall be submitted to the Direccion de Aeronautica Civil.
(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 Regulations. Complete aircraft, new or used, will require the following documents:
(i) Export Certificate of Airworthiness - FAA Form 8130-4.
(ii) FAA-Approved Airplane Flight Manual and Weight and Balance Report with Equipment List.
(iii) 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
1. In order to be eligible for certification by the Philippine Government, Class I, II and III products should be covered by export airworthiness approvals in accordance with the applicable provision of Part 21 of the United States Federal Aviation Regulations.
2. In addition to the data required to be furished to the purchaser, an aircraft, when a NEW aircraft is the first I of a model to be exported to the Philippines, the following data will be forwarded direct by the exporter to the Administrator, Civil Aeronautics Administration, Manila, Philippines:
a. One copy of the weight and balance report pertaining to the particular aircraft including a loading schedule or chart, if applicable, and an equipment list.
b. One copy of the Approved Aircraft Flight Manual, if applicable, to the particular type of aircraft.
c. One copy of the assembly and rigging instructions, if the aircraft is to be assembled at the point of destination.
d. One copy of the pertinent maintenance manual and service bulletins.
e. The Export Certificate of Airworthiness, FAA Form 8130-4.
I/ When in doubt as to whether an aircraft is the first of a model, contact the air authority of the importing country.