Appendix 2
2.2 In addition, aircraft must be eligible for the issue of a standard airworthiness certificate as prescribed in Subpart H of FAR Part 21 unless otherwise agreed by the DA.
3. ADDITIONAL REQUIREMENTS.
3.1 This subject identifies those design requirements additional to the FAR certification basis which must be satisfied for a particular aircraft type to be eligible for Malaysian certification.
3.2 Additional Requirements for Malaysian certification are not specified for fixed wing aircraft:-
(a) below a maximum authorized weight of 2730 kg (6000 1bs).
(b) below a maximum authorized weight of 5700 kg (12500 lbs) when certification will not be applied for in the Malaysian Transport or Aerial Work Categories.
NOTE: Malaysian air navigation legislation requires the carriage of equipment on scales related to the purpose for which the aircraft is being flown. The aircraft commander is responsible for determining that an aircrait is properly equipped for any proposed flight.
3.3 For all aircraft other than those defined in paragraph 3.2 DCA may prescribe Additional Requirements. Details for any individual aircraft type will be supplied on written application; a limited type evaluation by the DCA may be required when no previous example has been certificated in Malaysia. Equipment required to be carried on flights for the purpose of public transport, to satisiy Malaysian air navigation legislation, will also be specified.
Additional Requirements need not necessarily be complied with before the Export Certificate of Airworthiness (FAA Form 8130-4) is issued. However, if the applicant for certification in Malaysia elects to satisfy any or all of the relevant Additional Requirements before the Certificate is issued, the Certificate must be endorsed in accordance with paragraph 4.4(b) of this document. In such cases the applicant shall notify the DCA to enable details of the Additional Requirements to be provided to the FAA or appropriate designee.
4. SPECIAL REQUIREMENTS.
4.1 This subject identifies those special administrative requirements which must be satisfied for particular products to be eligible for Malaysian certification or use on Malaysian registered aircraft.
Appendix 2 APPLICABILITY CODE:
+ Required only with first of type and model exported to Malaysia.
* Required only for aircraft with a maximum authorized weight greater than 5700 kg (12500 1bs).
4.2 All aircraft.
* (a) Statement of build standard. This statement must include the aircraft specification, changes in design to satisfy Malaysian Additional Requirements and a list of Service Bulletins incorporated during manufacture. The list of Service Bulletin incorporation must identify:
i) Production versions of the Service Bulletins.
ii) Service Bulletins.
ii) Alert Service Bulletins.
(b) Copy of the production flight test report or a statement that no flight test has been completed.
(c) Modification standard. This must include:
i) Customer options and equipment incorporated including items of equipment not necessarily installed by the manufacturer of the aircraft.
ii) Service Bulletins compliance.
(d) Export Certificate of Airworthiness (see paragraph 4.4 of this document).
+ (e) A copy of the aircraft Type Certificate Data Sheet.
(f) Details of any alterations which may have been embodied under the Supplemental Type Certificate procedure (STC).
NOTE: Any STC which has been embodied but not previously investigated by the DCA will be subject to evaluation before a Malaysian Certificate of Airworthiness is issued.
(g) A list of the defects, if any, at the time of issue of the Export Certificate of Airworthiness which will require rectification by the Malaysian operator.
(h) The FAA Approved Flight Manual or Pilot's Operating Handbook for the individual aircraft concerned, for approval by the 104
Appendix 2
(i) Airframe/engine/propeller/auxiliary power unit log books.
(j) Seating configuration approval document, where relevant.
+ (k) Maintenance Review Board document, where relevant.
+ (1) A summary of FAA approved retirement life limitations.
* (m) Electrical load analysis.
NOTE: For aircraft other than first of type, the DCA requires sufficient information to be available to determine the effect of customer options, etc., on the suppiy of electrical energy to essential services.
+ (n) FAA Approved Master Minimum Equipment List, where applicable
(o) Weighing report and associated weight schedule.
Appendix 2 + (P) Manuals required by the DCA:
NO. REQUIRED
1) The FAA approved Flight Manual or 2 (but see Pilot's Operating Handbook. also
4.2 (h)) ii) Airframe Maintenance including wiring diagrams. 1 iii) Operations. 1 iv) Weight and Balance/Loading Procedures. 1
v) Overhaul. 1 vi) Structural repair. 1 vii) Engine maintenance and overhaul. 1 viii) Standard practices. 1 ix) Non-destructive testing. 1 × ) Structurally significant items.
xi) Maintenance planning guide including manufacturers recommended component overhaul lives. 1 xii) Parts Catalogue. 1 xiii) Set of Service Bulletins and Service Letters or equivalent documents. 1 Cort ication. NOTE: A condition of Malaysian certification of the first of a type is the provision by the Malaysian applicant for certification of a continuing amendment service for the required manuals.
(g) Record of compass system and magnetic compass swings.
(r) Record of rigging checks.
(s) A statement that suitable tests and measurements have been made and recorded to establish the satisfactory performance of the installed radio/radar apparatus and their associated antennae. A list of antennae positions must be provided.
(t) Detailed list of equipment constituting the navigation and communications installation.
Appendix 2 * (u) List of Serial Numbers of significant component parts.
+ (v) Noise Type Certificate.
4.3 Used aircraft. In addition to the requirements specified in paragraph 4.2 (but (b) need not necessarily be complied with) the following information is required for used aircraft:
* (a) Maintenance program to which these aircraft have previously been maintained including:
(i) previous check cycle; and
(ii) future check cycle.
D) Component overhaul life summary, including details of service life remaining and modification standards.
(c) Component and structure retirement life summary where applicable, including details of service life remaining.
* (d) Compliance with structural inspection program. This nust include details of any structural sampling program in which these aircraft have been included, together with details of their position in this program.
condition survey and review of the associated records to the satisfaction of the DCA before the issue of a Malaysian All used aircraft will be subject to a physical Certificate of Airworthiness is considered. In addition, approval must be obtained from the DCA for the applicants proposals for integration of the aircraft into a maintenance program approved by the DCA. Prospective purchasers of used aircraft are encouraged to discuss their proposals with the DCA before arranging import into Malaysia.
4.4 Requirement for Export Certificates of Airworthiness (FAA Form 8130-4) to be issued.
An Export Certificate of Airworthiness (FAA Form 8130-4) is required for any Class I product or engine module exported from the United States to Malaysia.
NOTE: In the case of aircraft, the Certificate shall not have been issued more than sixty days prior to the date of presentation for Malaysian certification, unless otherwise agreed by the DCA.
(b) When Additional Requirements have been notified to the FAA or FAA designee in accordance with paragraph 3.4 of this document, the Certificate shall be so endorsed as to provide a detailed status of compliance. Items of non-compliance do not require a waiver from the DCA providing they are so endorsed on the 107
Appendix 2 Certificate, as Malaysia is principally concerned with establishing the status of compliance at the time of export from the United States.
(c) The Certificate shall be accompanied by a document furnished by the applicant (e.g., a log book) which contains entries identifying those applicable Airworthiness Directives (AD's) with which compliance has been achieved. This document shall also identify those AD's containing a repetitive compliance requirement and when compliance is next due to be satisfied. All ADs shall be complied with prior to the issue of the Certificate unless a waiver has been issued by the DCA.
4.5 Appliances - general.
(a) For the purpose of this procedure, "appliance" has the meaning assigned to it in FAR Part 1 and includes associated replacement and modification parts.
(b) The DCA will accept that an appliance has those characteristics vouched for on an FAA Airworthiness Approval Tag (FAA Form 8130-3). The procedures given in the following sub-paragraphs provide acceptable alternative means of compliance for appliances other than radio:
i) The appliance has been accepted by the FAA as complying with the Minimum Performance Standards of the applicable Technical Standard Order or, ii) In lieu of approval under a Technical Standard Order, the appliance has been accepted by the FAA as meeting the applicable FAR's and the terms of the applicant's specifications.
(c) An FAA Airworthiness Approval Tag must be supplied with all appliances.
4.6 Radio appliances. The DCA may require a declaration of design and performance in the format specified in the current issue of British Standard Specification G.100. Details for any individual type of radio appliance will be supplied on written request.
NOTE: Where a radio appliance has been approved by the United Kingdom Civil Aviation Authority, the item will be accepted by the DCA without further investigation. The relevant CAA approval number must be quoted on the FAA Airworthiness Approval Tag.
Appendix 2
4.7 Products other than aircraft or appliances.
(a) Engines (including APU's), engine modules, and propellers:
Export Certificate of Airworthiness (refer to paragraph 4.4).
ii) Service Bulletin compliance; statement.
(b) Class II as defined in Subpart I of FAR Part 21:
i) FAA Airworthiness Approval Tag.
(c) Class III as defined in Subpart L of FAR Part 21:
1) FAA Airworthiness Approval Tag or, ii) A certification by the manufacturer of the product that the product concerned was manufactured under a Production Certificate granted under Subpart G of FAR Part 21, a Parts Manufacturing Approval granted under Subpart K of FAR Part 21, or a Technical Standard Order authorization granted under Subpart O of FAR Part 21, as appropriate.
5. SPECIAL CONDITIONS.
Where an aircraft is of unusual or novel design, the DCA reserves , the right to prescribe Special Conditions or refuse certification.
Applicants for Malaysian certification are advised to give early notification to the DCA of any aircraft type in this classification.
Appendix 2
KINGDOM OF MOROCCO - SPECIAL REQUIREMENT (New - August 23, 1977)
1. Import of U.S. Manufactured Aircraft.
a. The Kingdom 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 REQUIREMENTS (ISSUE 2) (Revised December 10, 1980)
1. 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 I and November 14, 1955, are prescribed in this document.
equirements 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.
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+).
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 be imported identical 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 111
Appendix 2 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:
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 RLD(+).
(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 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.
(9) For used aircraft, the historical records, such as aircraft and engine logbooks and records regarding maintenance, 112
Appendix 2 repairs, modifications, mandatory service bulletins, and airworthiness directives.
For subsequent import aircraft, to the same make and model as under 1.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 RLD to determine the deviations.
4. TECHNICAL REQUIREMENTS.
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 RLD(+).
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, paragraph 2.2 through paragraph 2.6 oi 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 RLD.
d. Propeller-driven aircraft of maximum certificated takeoff weight not exceeding 5700 kg, which do not comply with Noise Standards at least as severe as the provisions of Chapter 3, paragraph 3.2 through paragraph 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 certiiication basis oider 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
(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 RLD.
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