Appendix 2 17 Airworthiness Requirements for non-rigid airship LI/12262 06.08.80 18 Airworthiness LI/11371 10.05.82 Requirements for manned free balloons and Hot Air Ships (FAR 31 and BAR "Manned Free Balloons" as well as BAR Paper 696 "Hot Air Ships") LI/11911 23.06.82 118
Appendix 2
NETHERLANDS
AEROPLANE NOISE CERTIFICATION REQUIREMENTS (effective March 1l, 1987) Subsonic jet aeroplanes and heavy propeller-driven aeroplanes.
Subsonic jet aeroplanes of over 20,000 kg maximum certificated takeoff mass, other than aeroplanes which require a runway length (with no stopway or clearway) of 610 m or less at maximum certificated mass for airworthiness, of a type that has been certificated in the Netherlands before (date of applicability of amendment) are excluded from import into the Netherlands unless they comply with the Standards of Chapter 2 oi ICAO Annex 16, Volume I (Aircrait Noise, First Edition, 1981), on the understanding that only the maximum noise levels of paragraph 2.4.2. apply.
1,2 Two and three engined aeroplanes, covered by paragraph 1.l above, are also eligible for import into the Netherlands if they are "Stage 2" aircraft according to the provisions of FAR Part 36 (Noise Standards: Aircraft Type and Airworthiness Certification), as amended by Amendment 36-12, dated June 29, 1981, effective August 1, 1981.
1.3 Subsonic jet aeroplanes of maximum certificated takeoff mass not exceeding 20,000 kg, propeller-driven aeroplanes of over 5700 kg maximum certificated takeoff mass, and subsonic jet aeroplanes of a type that has not been certificated in the Netherlands before (date of applicability of the amendment), other than aeroplanes which require a runway length (with no stopway of clearway) of 610 m or less at maximum certificated mass for airworthiness, are excluded from import into the Netherlands unless:
they comply either with the Standards of Chapter 3 of ICAO Annex 16 Volume I (Aircraft Noise, Firșt Edition, 1981), provisions of FAR Part 36 (Noise Standards: Aircraft Type and Airworthiness Certification) up to and including Amendment 36-12, dated June 29, 1981, effective August 1, 1981.
1.4 Those propeller-driven aeroplanes, covered by paragraph 1.3 above, which are derived from types that have been certificated at maximum takeoff mass not exceeding 5700 kg and with passenger seating capacity of no more than 19 seats are also eligible for import into the Netherlands if they comply with the provisions of paragraph 2.1 hereunder.
2. Light propeller-driven aeroplanes.
2.1 Propeller-driven aeroplanes of maximum certificated takeoff mass not exceeding 5700 kg other than those covered by 119
Appendix 2 [[paragraph]] 2.2, are excluded from import into the Netherlands unless they comply with the Standards of Chapter 6 of ICAO Annex 16, Volume I, (Aircraft Noise, First Edition, 1981).
2.2 Powered gliders are excluded from import into the Netherlands unless they comply with the Standards of Chapter 6 of ICAO Annex 16, on the understanding that the maximum noise levels of paragraph 6.3 are lowered by 5 dB(A).
2.3 Engine power settings for those aeroplanes, covered by [[paragraphs]] 2.1, and 2.2 above, which are higher than the maximum power in the normal operating range but lower than the maximum takeoff power, have to be indicated on the engine instruments by a yellow arc (cautionary range). The Flight Manual shall contain a note that engine power settings above the maximum power in the normal operating range may only be applied during takeoff and in emergency.
3. Helicopters. Helicopters of a type, that has not been certificated in the Netherlands before, (date of applicability of the amendment) are excluded from import into the Netherlands unless they comply with the Standards of Chapter 8 of ICAO Annex 16, Volume I (Aircraft Noise, First Edition, 1981).
4. Exemptions.
4.1 The Director of the Aeronautical Inspection Directorate, Department of Civil Aviation (RLD) may exempt from the above provisions:
a. Aeroplanes, which are exclusively designed and used for aerobatic purposes or agricultural or fire fighting uses.
b. Aeroplanes not satisfying the applicable requirements for noise certification when they can be equipped to these standards provided that;
suitable conversion equipment exists for the aeroplanes type in question;
aeroplanes fitted with such equipment are capable of achieving the standards required for noise certification;
such equipment is actually available, and the operator has ordered the equipment; and the appropriate equipment must be fitted within not more than two years from the date of registration.
c. Aeroplanes which are temporarily registered into the register of another State than the Netherlands, on account of hire purchase.
Appendix 2
d. Aeroplanes which replace aeroplanes which have been accidentally destroyed and which cannot be replaced by a comparable aeroplane with noise certification available on the market, provided that the recistration of the replacement aeroplane is carried out within one year following the destruction in question; and the replacement aeroplane is removed from the register within two years after registration.
e. Aeroplanes of historic interest.
4.2 In special cases, and under conditions to be defined, the Director of the Aeronautical Inspection Directorate, Department of Civil Aviation (RLD) may allow the application of other noise requirements provided the noise levels are at least equivalent to hose required for the aeroplane according to the ICAO Annex 16.
volume 1, Noise Standards, and on the understanding that subsonic jet aeroplanes and propeller-driven aeroplanes of over 5700 kg maximum certificated takeoff mass have to comply with the provisions of paragraph 1.1 above.
NOTE: At present, no Certificates of Airworthiness are issued for Ultra Light Aeroplanes. However, permission to fly without a Certificate of Airworthiness will only be granted under specified conditions.
As far as the noise emission is concerned, it is not permitted to use ultra light aeroplanes in the Netherlands unless the noise level measured in a full power flyover in 150 meters is below 60 dB(A).
Two-seaters which are used for instruction purposes only are admitted if the noise level does not exceed 63 dB(A).
AC 21-2G . 7/9/92 Appendix 2
NETHERLANDS ANTILLES - SPECIAL REQUIREMENTS [[Reprinted from AC 21-2F dated August 7, 1987]] 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 Aviation, Netherlands Antilles (Department van Luchtvaart Nederlandse Antillen (D.V.L. N.A.)) (See Note 6a).
0. Aircrait 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 exciuded from import into the Netherlands Antilles except on an individual basis after referral tc the D.V.I. 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 l, 1967, may continue tc 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 Mode.. 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 340 122
Appendix 2 Z. DOCUMENIS 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, exemption, or restrictions, which have been rescribed by the FAA, because of design or structural characteristics or features incorporated which are not in coniormity with data forming the basis for the initial type certification of aircraft of this type.
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.I. N.A. will inform on request regarding such of the listed documents and data as may be required in each specific area.)
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 oi 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 [[paragraphs]] (1) and (2) shall be delivered well in advance of the intended delivery date of the aircraft.
Appendix 2 Bulletins. A complete set of service publications including bulletins issued by the manufacturers of the aircraft and by 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. a copy of all new such
(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.
D. 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.I. 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 uthority to cover the use oi radio, vaild ior 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.I. N.A.
Appendix 2
6. NOTES.
a. The address of the Department of Civil Aviation:
Department van Luchtvaart Dr. A. Plesman Luchthaven Curacao, Wederlandse 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
NEW ZEALAND - SPECIAL REQUIREMENTS (Revised February 10, 1992) SECTION 1 - INTRODUCTION.
1.1 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 I.
Special requirements which must be satisfied before the issue of a U.S. Export Certificate of Airworthiness are identified in Section 2. Data shall be forwarded to the Director of Civil Aviation Safety, Civil Aviation Authority, P.O. Box 31441, Lower Hutt, New Zealand (Attention: Controller Aircraft Certification).
1.3 Airworthiness certification procedures of New Zealand aircraft are specified in the New Zealand Civil Airworthiness Requirements Volume 1 Sections A and B. Application for a New Zealand Certificate of Airworthiness is to be made not less than 28 days before the issue of the certificate is desired.
1.4 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 satisfied before export from the United States.
1.5 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.
1.6 If the airworthiness standards which form the certification asis ior the aircraft pre-date the U.S. Civil Airworthiness legulations, the aircraft may be certified in the New Zealanc Restricted Category and ineligible for air transport and aerial work operations.
1.7 Supply of data listed in Section 2.2 and 2.3 may be required in respect of Supplemental Type Certificate (STC) alterations before a New Zealand Certificate of Airworthiness is issued.
1.8 Unless otherwise agreed by the Authority, all data must be supplied in the English language and supplied at no cost to the Authority.
Appendix 2 SECTION 2 - SPECIAL REQUIREMENTS.
2.1 The following data requirements 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 Aircraft Certification Group, Civil Aviation Authority.
(a) A copy of the Export Certificate of Airworthiness.
(b) Statement of Modification, Service Bulletin and Equipment Standard at build.
(c) Summary of Modifications, Repairs, Service Bulletins, Customer Options, and Equipment incorporated since initial build.
(d) Statement of Compliance with FAA Airworthiness Directives for U.S. manufactured aircraft.
(e) Airframe, engine, propeller and APU logbooks (as applicable).
(1) Copies of any applicable Supplemental Type Certificates.
In addition, the following data associated with foreign type certification will be required for first aircraft of a particular type or model exported to New Zealand.
(a) A copy of the type certificate or equivalent document, which certifies compliance with the applicable airworthiness requirements.
(b) Particulars of the airworthiness design requirements with which the aircraft complies including the airworthiness standards, the effective date of the standards, any special conditions applied and any provisions not complied with, together with the associated compensating factors. A copy of a type certificate data sheet or equivalent will provide such data except that, where special conditions or compensating factors are included, the documents detailing them will also be required.
(c) A listing of all the data submitted to the original type certifying Authority for showing compliance with the airworthiness standards. Identified data will include structural load, strength analysis, structural fatigue, aeroelastic, structural test, and flight test reports.
(d) Such of the data listed by 2.2(c) as the Authority requires.
(e) A copy of the flight manual or, if a flight manual is not required by the applicable airworthiness standards, a document defining operating limitations and providing operational data. Also 127
Appendix 2 a weight and balance manual if such information is not contained in the flight manual.
(i) Data to identify the type design such as a parts catalogue or drawings.
(g) Data to identify essential and optional equipment and the location of emergency equipment.
(h) Copies of the instructions for continuing airworthiness, required to be prepared under the airworthiness standards, such as maintenance manuals.
(i) Service documentations issued by the manufacturers of the aircrait, engines, propellers and equipment, such as service bulletins, service letters and equivalent documents.
(j) A statement from the type certificate holder or manufacturer, undertaking to provide the Authority with an ongoing revision service for the operating, maintenance and service documentation.
2.3 It is desirable at the time of export certification to supply additional available data which may subsequently be required for such purposes as the approval of design changes, maintenance and air transport operations. These data may include:
(a) Maintenance, overhaul and repair manuals for airframe, engines, propellers and equipment additional to those required under
2.2.
(b) The manufacturer's detailed specification for the type.
(c) The customer's detailed specification for the type.
(d) The manufacturer's specifications for special processes and materials used in manufacture and maintenance.
(e) Electrical load analysis.
(£) Location drawings for all radio antennas.
(9) Operations manual.
(h) Master minimum equipment list (MMEL).
(i) Maintenance planning document (MPD).
(j) Maintenance review board document (MRB).
(k) Manufacturers Maintenance schedule.
(2) Ground and flight type inspection reports (TIR).
Appendix 2
ISLAMIC REPUBLIC OF PAKISTAN - SPECIAL REQUIREMENTS (Revised February 7, 1991)
REQUIREMENT FOR IMPORTATION OF AIRCRAFT AND ASSOCIATED STORES aircrait into Pakistan, as well as aircrait stores. The requirements shall also be applicable on foreign registered aircraft already in Pakistan which are intended to be transferred on Pakistan Civil Register.
2. IMPORT OF NEW AIRCRAFT. The importer is required to provide the following, to be eligible for issue of Certificate of Airworthiness in the Islamic Republic of Pakistan.
2.1. The Certificate of Airworthiness for Export.
2.2. A complete list of Airworthiness Directives, Service Bulletins or similar documents incorporated during production of aircraft engine(s), propeller (s) and installed equipment.
importer shall supply written confirmation from the relevant manuiacturers that amendments, revision and new issues of Service Bulletins, SIL, and other similar documents will be supplied to the CAA free of cost as soon as they are issued.
2.3. Statement of modification status including customer options incorporated (as applicable).
2.4. Production test flight report for that particular type of aircraft.
2.5. Weight and Balance schedule for that particular type of aircraft.
2.6. List of components installed on the aircraft as per paragraph 2.3.
2.7. The under mentioned manual (s)/documents(s) of aircrait, engine, propellers, component/accessories installed are required as applicable
(i) Two sets of maintenance manuals.
(ii) Two sets of overhaul/shop manuals.
(iii) Two sets of flight manuals.
(iv) Two sets of engine operation manuals.
(V) Two sets of structural repair manuals.