Appendix 2
REPUBLIC OF LEBANON - SPECIAL REQUIREMENTS (New - September 20, 1977)
1. Lebanese acceptance of U.S. aeronautical products.
a. Lebanon's policy is to accept, without modification, aircraft which meet requirements of the competent authority in the country of manufacture. All U.S. equipment meeting Federal Aviation Administration (FAA) requirements are therefore acceptable.
Appendix 2
MALAYSIA, WEST - SPECIAL REQUIREMENTS
1. To be eligible for export to West Malaysia, an aircraft must meet the requirements prescribed in Federal Aviation Regulations Part 2l, Subpart
2. The applicant for certification of the aircraft in West Malaysia must provide the following documents to the Department of Civil Aviation, 3rd Floor, 4th Block, Government Offices, Young Road, Kuala Lumpur, West Malaysia:
a. For each aircraft:
(1) FAA Export Certificate of Airworthiness.
(2) Weight and Balance Report.
(3) Equipment List.
(4) Modification statement and list of FAA Airworthiness Directives complied with.
(5) Copy of Production Flight Test Report related to the specific aircraft.
b. For each model aircraft, one copy of:
(1) FAA approved flight manual.
(2) Weight and Balance manual.
(3) Operating Manual.
(4) Maintenance Planning Data.
(5) Maintenance Manual (Airframe).
(6) Maintenance Manual (Engine).
(7) Overhaul Manual (Airframe).
(8) Overhaul Manual (Engine).
(9) Structural Repair Manual.
(10) Complete set of Service Bulletins (Airframe).
(11) Complete set of Service Bulletins (Engine).
Appendix 2
(12) FAA Aircraft Data Sheet.
(13) FAA Engine Data Sheet.
c. Amendment service tor the above documents must be provided as applicable 74
5/18/81 AC 21-2E Appendix 2
GOVERNMENT OF MOROCCO - SPECIAL REQUIREMENTS (New - August 23, 1977)
1. Import of U.S. Manufactured Aircraft
a. The Government of Morocco accepts for import and registration, without modification, U.S. aircraft manufactured to Federal Aviation Administration (FAA) standards.
Appendix 2
KINGDOM OF THE NETHERLANDS - SPECIAL REQUIREMENIS (ISSUE 2) (Revised August 28, 1978)
1. INTRODUCTION.
a. 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 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.
2. 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 (RID+).
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 RID, 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 RID 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 RID approved maintenance schedule from which this schedule must be followed and the additional maintenance to be performed for this phase of the maintenance schedule.
+ Address: Rijksluchtvaartdienst Directae Luchtvaartinspectie Postbus 7555 1117 ZH Schipol Telephone No.: 020-5163260 The Netherlands 76
Appendix 2
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:
(1) The design and test data specified in Annex A.
NOTE: Annex A is available from the RID(†).
(2) The certificate of airworthiness issued or renewed within a period of 60 days immediately preceding the date of the application for validation of that certificate or the issue of a new certification 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.
(6) 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.
(d) 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.
Appendix 2
(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, to the same make and model as under l.a.
(1) The documents and data listed under a(2), a(4), a(5), a(6), and a(9) unless documentation submitted previously is also applicable to the individual concerned.
(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 RID to determine the deviations.
4. TECHNICAL REQUIREMENIS.
a. 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.
NOTE: Annex B is available from the RID (+).
c. Subsonic jet aircraft, other than aircraft which require a runway with no stopway or clearway of length 600 m or less at maximum certificated weights for airworthiness, which do not comply with Noise Standards at least as severe as the provisions of Chapter 2, par. 2.2 through par. 2.6 of Annex 16, including the Amendments I and II, to the Convention on International Civil Aviation first issue, dated August 1971, are excluded from import to the Netherlands, except on an individual basis after referral to the RID.
d. Propeller-driven aircraft of maximum certificated take-off weight not exceeding 5700 kg, which do not comply with Noise Standards at least as severe as the provisions of Chapter 3, par. 3.2 through par. 3.4 of Annex 16, including the Amendments I and II, to the Convention on International Civil Aviation, first issue, dated August 1971, are excluded from import to the Netherlands, except that aircraft:
(1) With a certification basis older than January 1, 1976, and being of a type which had no Netherlands airworthiness approval before January 1, 1978, are excluded from import to the Netherlands on or after that date;
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