Appendix 2 AC 21-2B 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 lst of July 1967. Issue 2 is effective from the Ist 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;
c. 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 aircraft, establish on the basis of their findings and on the basis of the maintenance records of the aircraft, the phase in the RLD approved maintenance schedule from which this schedule must be followed and the additional maintenance to be performed for this phase of the maintenance schedule.
3. 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 43
(2) The certificate of airworthiness issued or renewed within a period of sixty days immediately preceding the date of the application for validation of that certificate or the issue of a new certificate of airworthiness.
(3) A statement specifying the applicable airworthiness requirements and indicating that these requirements were complied with.
(4) The manufacturer's specification and, if available, a type specification issued by the Contracting State, containing basic data concerning performance, dimensions, weights and required equipment.
(5) The weight and balance report, including equipment list, showing all removable items of equipment that are included in the empty weight.
The aircraft flight manual, approved by the contracting State, issued in the English language.
(7) The manufacturer's maintenance manual, containing at least the following information:
(a) Engineering description of the aircraft.
(b) Instructions for ground handling.
(c) Assembly and disassembly instructions for the various aircraft parts and assemblies.
(a) Description of the powerplants, propellers and the various systems.
(e) Maintenance repair and overhaul instructions and the associated inspection items and schedule.
(8) Aircraft, engine and propeller parts lists.
(9) For used aircraft the historical records, such as aircraft and engine logbooks and records regarding maintenance, repairs, modifications, mandatory service bulletins and airworthiness directives.
b. For subsequent import aircraft of the same make and model as under paragraph 3а:
(1) The documents and data listed under 3a(2), (4), (5), (6), and (9% unless the documentation submitted previously is also applicable to the individual aircraft concerned.
Appendix 2 AC 21-2B Page 44 10/2/69
(2) A list of deviations from the first aircraft. If the applicant is unable to provide such a list additional data may be required to enable the RLD to determine the deviations.
3. TECHNICAL REQUIREMENTS Special conditions of a particular nature. The aircraft shall to the extent deemed essential by the RID, comply with such additional requirements as may be specified in writing. These additional requirements will be prescribed if the aircraft has special features or characteristics the safety of which has not been guaranteed adequately by the existing requirements.
b. Special conditions of a general nature. The special conditions of a general nature are listed in Annex B. (See note 4b.)
4. NOTES
a. The address of the RLD is: Rijksluchtvaartdienst Afd. Luchtvaartinspectie Hangaar 5, tel (020) 798451 Schiphol - Oost Postbus 7555 The Netherlands
b. Annex A and Annex B are available from the RLD.
c. The RLD will inform on request whether an aircraft is the first of a type to be exported to the Netherlands.
5. AIRCRAFT TYPES WHICH HAVE HAD EXPORT CERTIFICATES OF AIRWORTHINESS VALIDATED BY THE RID.
Manufacturer Model Manufacturer Model GAGUSTA - BELL AB. 206 A BELL 47G BEECH D18 S 47G-2A-1 23 473 65 473-2A 65-80A 65-90 BOEING 707-355C 95-A55
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 AI-6 172B 172E HUGHES 269B 172F LOCKHEED L-188C 182B 182F 172G L-1049G L-1049H A188 MOONEY M-20A P206 U206A PIPER J3C-65 (I-4J) CONVAIR 640 PA-18-125 PA-18A-135 DOUGLAS DC-3C-S1C-3G PA-18-150 C54B-DC PA-18A-150 PA-19 DC-6A PA-22-108 DC-6B PA-22-150 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 FAIRCHILD 24R 46 A NOSNIIS L-5B S-62 A
Appendix 2 AC 21-2B CHG 1 Page 46 11/13/70
KINGDOM OF THE NETHERLANDS - SPECIAL REOUTREMENTS 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 2l 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.
Without prejudice to the foregoing, aircraft types, the United States Export Certificates of Airworthiness of which were validated by the 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 DOCUMENTS AND DATA REQUIRED. The following documents and data shall be submitted to the D.V.I. 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,
(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, 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.
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. wi11 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 oi the customer's specification for the aircrait, together with a specimen copy of the approved Airplane Flight Manual. A copy of information or instructions essential to the assembly and
(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 equipment
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.
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. FLY-AWAY AIRCRAFT.
a. 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.
AC 21-2Г 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.
a. 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.
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 21-28 Page 46-4 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 2l 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 I product exported from the U.S. to New Zealand. Class II and Class III 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 21 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- 2 B Appendix 2 10/2/69 Page 47
f. A report on the flight characteristics of the aircraft which shall be specified in a manner convenient for calculating the aircrafts performance over a reasonable range of weights, altitudes, and atmospheric conditions. Type flight test reports should be obtained from the FAA Regional Office responsible for the type certification of the aircraft in question. The purpose of this requirement is to verify that the aircraft can be operated in such a manner as to leave a satisfactory margin between the scheduled characteristics of the aircraft, and those of New Zealand airdromes, and surroundings, and the routes operated upon.
Performance figures, as referred to in paragraph I., above, shall have been corrected to standard atmospheric conditions, and a statement to this effect shall be made a part of the report on the flight performance characteristics of the aircraft.
h. One extra set of the pertinent service bulletins, assembly instructions, and operation manuals, etc.
1. Copies of supplements, amendments, modifications, or other changes to type certification data, as required in 5b. through 5h.
6. Information contained in paragraphs 5d, e., f., and g., (i.e., structural and performance data), to be acceptable to the Director of Civil Aviation in New Zealand, must be certliled by the FAA, or by a designated representative approved for this purpose by the FAA. This certification may be an endorsement of the actual documents, or in the form of a covering letter attached to the documents provided they are adequately identified in the covering letter. In a case where the information is furnished by different sources, separate certification with respect to each set of documents is required.
7. In lieu of the "certificate of type design" normally required in connection with the first aircraft of a model exported to New Zealand, the Export Certificate of Airworthiness, FAA Form 8130-4, issued to cover such an aircraft, shall indicate the following information in addition to other entries provided for or required under special circumstances or conditions:
a. Specification Number:
(List the covering aircraft spcc. or IC Data Sheet No.)
b. Type Certificate Number:
(List aircraft type certificate number) Aircraft Classification:
(Example: Single engine land plane)
Appendix 2 AC 21-2B Page 48 10/2/69
d. Category:
(Example: Normal category)
e. Subdivision(s) :
(Example: Personal aircraft)
8. In addition to the data to be forwarded to the Director of Civil Aviation in accordance with instructions contained in paragraph 3 above, the following material should accompany the aircraft, or otherwise be delivered to the purchaser:
a. One copy of the weight and balance report.
b. One copy of the aircraft flight manual and of the loading chart when such material would be required if the aircraft were certificated in the "standard" classification as an aircraft of U.S. registry.
c. One copy of the manufacturer's production flight test report with respect to new aircraft which are exported by the manufacturer.
AC 21- 2 B Appendix 2 10/2/69 Page 49
PAKISTAN - SPECIAL REQUIREMENTS
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 Il 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 provisions of Part 21 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
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.