AC 21-2B Appendix 2 10/2/69 Page 15 NOTE: An aircraft having major changes which required approval under Federal Aviation Regulations (FAR) Part Z1, Section
21.97 and/or FAR Part 21, Subpart E 18 not eligible to obtain a French airworthiness certificate under the provisions of paragraph 2a(2), even though an aircraft of the same model may have been issued a French airworthiness certificate prior to October 12, 1968. In order to obtain a French standard airworthiness certificate, the applicant must comply with the procedures outlined under paragraph 2a(1). A French type certificate for import or an extension of a type certificate for import will be issued each time that the FAA issues a new type certificate or an STC for a model based on a model previously imported.
b. Special Airworthiness Certificates. A French special airworthiness certificate may be issued to an aircraft of a model for which application has been made for a French type certificate for import, in order to facilitate its use under the conditions spelled out in Article 5, paragraph 2B of the CNAC, provided that the Secretariat General of Aviation Civil (S.G.A.C.) 1s familiar with the model. In addition, the procedure required for issuance of special airworthiness certificates will be applied in the case of aircraft in the restricted category • Permit. A permit may be issued by the S.G.A.C. to an aircraft which has provisional French registration markings, only to permit the ferrying and tests necessary for aircraft type certification. Normally, the S.G.A.C. will not authorize any private utilization and the permit may, basically, be renewed only for a total period of time not to exceed one year (reference CNAC Articles 13 and 19, and Article 5, paragraph 3).
Requirements for Issuance of French Type Certificates for Import for U.S.
Manufactured Aircraft.
a. Applicant.
(1) The applicant for a French type certificate for import must be the person responsible for maintaining the level of airworthiness for the aircraft. Generally such person would be the manufacturer who originally obtained, and who holds the U.S. type certificate, ir the U.s. type certificate has been transferred by the original holder, the new holder (applicant) must be capable of, and responsible for maintaining the level of airworthiness.
(2) In exceptional cases, it is possible to accept an application for a French type certificate for import from a person who is not the U.S. type certificate holder, provided that the applicant furnishes proof that he has been duly authorized to take over complete responsibility for the type certificate under the licensing provisions of Federal Aviation Regulations Part 21, Section 21,47.
Appendix 2 AC 21-2B CHG 1 Page 16 11/13/70
b. Documents. The required documents are specified in Article ll of the CNAC and under paragraph 5 of these special requirements.
c. Special Conditions. A U.S. applicant for a French type certificate for import must show compliance with the applicable FARS, plus any special conditions imposed by the S.G.A.C. Three types of special conditions are outlined in paragraphs 3c(1), (2), and (3). The primary purpose of the special conditions is to guarantee an airworthiness level equivalent to that of aircraft built and certified in France.
(1) Administrative Special Conditions.
(a) Language. The documents which the S.G.A.C. requires to be furnished may be in English except for the following, which must be provided in French:
1 The type certificate (I.C.), data sheet;
2 The flight manual; and 2 The proposed maintenance guide.
NOTE: The S.G.A.C. will verify the translations of these documents and must approve the IC data sheet and the flight manual.
(b) Document Format. The T.C. data sheet, flight manual, and proposed maintenance guide must be prepared in accordance with the formats specified in the following:
1 I,C. Data Sheet. The SGAC will accept a simple translation into French of the IC data sheets approved by the FAA.
. Flight Manual. The flight manual in French, which must be carried in each aircraft imported into France, must be either a simple translation of the FAA approved flight manual when one exists, or if a flight manual does not exist, a similar document must be established for the purpose of import into France and must contain the following sections:
Limitations.
Normal Operations Emergency Operations.
Performance (Limited to only the approved performance conforming to the requirements of the applicable airworthiness FAR part.)
AC 21-2B CHG 1 Appendix 2 11/13/70 Page 21 * b. The documents listed in paragraph 3c(1) (a)2 and 3, as well as the following documents, will be required for each individual NEW aircraft imported into France.
(1) One copy of a list of radio and electrical equipment items, with their characteristics and their operating instructions.
These equipment items must conform to the applicable categories for which there are French certification requirements.
(2) One copy of the production flight test report for the aircraft involved, including a copy of the flight test checklist utilized when testing the aircraft.
(3) A U.S. Export Certificate of Airworthiness, FAA Form 8130-4, for the aircraft.
(4) A weight and balance record containing a complete inventory of all equipment and instruments.
(5) A list of modifications that have been incorporated, at least those covered by service bulletins, except that, if the manufacturer's information distribution system has been found satisfactory by the S.G.A.C., submittal of such a list is not required.
c. For an individual, USED aircraft, the following documents must be furnished in addition to those specified under paragraph 5b:
(1) A summary of modifications, including:
(a) A summary of mandatory changes made,
(b) A list of modifications recommended by the manufacturer (service bulletins, etc.),
(c) A list and description of modifications made by the previous owners.
(2) A summary and date of past maintenance inspections and the operating hours since the last inspection of each type.
Appendix 2 AC 21-2B Page 22 10/2/69 Example of Standard Application Form for a French Type Certificate for import.
1. a. Application for Type Certificate for Import:
b. Application for Extension of Type Certificate for Import. (Type Certificate No.
2. Name of Applicant:
3. Status of applicant with respect to aircraft to be certificated:
Original Manufacturer: Licensee:
4. Applicant's Complete Address:
5. Address of Production Plant:
6. Aircraft Description:
Make :
Model:
Descriptive Documents (enclose copies with application):
a. FAA Type Certificate No.
b. FAA Type Certificate Data Sheet dated
8. FAA Type Certification Basis (FAR):
9. Date:
10. Applicant's Title and Signature:
AC 21-2B Appendix 2 10/2/69 Page 41
(9) Structural Repair Manual.
(10) Complete set of Service Bulletins (Airframe).
(11) Complete set of Service Bulletins (Engine).
(IZ) FAA. Aircraft Data Sheet.
(13) F.A.A. Engine Data Sheet.
c. Amendment service for the above documents must be provided as applicable.
Appendix 2 AC 21-28 CHG 1 Page 42 11/13/70
KINGDOM OF THE NETHERLANDS - SPECIAL REQUIREMENTS (ISSUE 2) INTRODUCTION. The special requirements associated with the Agreement on the reciprocal validation of export certificates of airworthiness of May 22, 1956, based on the Exchange of Notes between the United States and the Kingdom of the Netherlands of September 19 and November 14, 1955, are prescribed in this document. These requirements are effective from the Ist of July 1967. Issue 2 is effective from the lst of'July 1969.
The requirements specified in this document apply only to aircraft * exported to the Netherlands, and not to those exported to Surinam, GENERAL.
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 Netherlands Department of Civil Aviation, Rijks Luchtvaart Dienst (RLD); (See Note 4a).
b. Aircraft with a certification basis older than March 5, 1952 and being of a type which had no Netherlands airworthiness approval during the last six years, are excluded from import to the Netherlands, except on an individual basis after referral to the RID;
Without prejudice to the foregoing, aircraft types, the United States Export Certificates of Airworthiness of which were validated already by the RLD, 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 specified under paragraph 5.
d. For each used aircraft the RLD will, after inspection of the airthe maintenance records of the aircraft, the phase in the RLD approved maintenance schedule from which this schedule must be phase of the maintenance schedule.
DOCUMENTS AND DATA REQUIRED. The application for the issue or validation of a certificate of airworthiness shall be accompanied by the following documents and data.
a. For the first aircraft of a specific make and model being imported.
(See Note 4c).
(1) The design and test data specified in Annex A. (See Note 4b).
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.