Appendix 2 4• SPECIAL REQUIREMENTS
4.1 This subject identifies those special administrative requirements which must be satisfied for particular products to be eligible for Brunefan Certification or use on Brunei civil registered aircraft.
APPLICABILITY CODE:
+ Required only with first of type and model exported to Brunef.
* Required only for aircraft with a maximum authorised 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 Brunel Additional Requirements and a list of Service Bulletins incorporated during manufacture. The list of Service Bulletin incorporation must identify :-
(1) Production versions of the Service Bulletins Service Bulletins
(111) 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 :-
(1) Customer options and equipment incorporated including items of equipment not necessarily installed by the manufacturer of the aircraft.
(11) 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.
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 Brunei Certificate of Airworthiness is issued.
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(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 Bruneian operator.
The FAA Approved Flight Manual or Pilots Operating Handbook for the individual aircraft concerned, for approval by the
(1) Airframe/engine/propeller/auxilliary 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 supply of electrical energy to essential services.
+ (n) FAA approved Master Minimum Equipment List, where applicable.
(o) Weighing report and associated weight schedule.
+ (p) Manuals required by the DCA :- NO: REQUIRED
1) The FAA approved Flight Manual 2 (but see or Pilots Operating Handbook also 4.2(h) ii) Airframe Maintenance including wiring diagrams 1 ii1) Operations 1 iv) Weight and Balance/Loading Procedures 1
v) Overhaul 1 vi) Structural Repair 1 34
Appendix 2 vf1) Engine maintenance and overhaul 1 vif1) Standard practices 1 †x) Non-destructive testing 1
x) Structurally significant items 1 ×1) Maintenance planning guide including manufacturers recommended component overhaul lives 1 ×11) Parts Catalogue 1 xi11) Set of Service Bulletins and Service Letters or equivalent documents 1 NOTE: A condition for first of a type certification in Brunel is the provision by the applicant for certification of a continuing amendment service for the required manuals.
(q) 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.
* (u) List of Serial Numbers of significant component parts.
+ (v) Noise Type Certificate.
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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 :- previous check cycle.
11) future check cycle.
* (b) 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 must include details of any structural sampling program in which these aircraft have been included, together with details of their position in this program.
NOTE: All used afrcraft will be subject to a physical condition survey and review of the associated records to the satisfaction of the DCA before the issue of a Brunei Certificate of Afrworthiness is considered. In addition, approval must be obtained from the DCA for the applicants proposals for integration of the aircraft into a maintenance programme approved by the DCA. Prospective purchasers of used aircraft are encouraged to discuss their proposals with the DCA before arranging
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 exported from the United States to Brunei.
NOTE: In the case of aircraft, the Certificate shall not have been issued more than sixty days prior to the date of presentation for certification in Brunei 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 Certificate, as Brunei is principally concerned with establishing the status of compliance at the time of export from the United States.
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(c) The Certificate shall be accompanied by a document furnished by the applicant (eg. a log book) which contains entries identifying those applicable Airworthiness Directives (ADs) with which compliance has been achieved. This document shall also identify those ADs 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.
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 :- The appliance has been accepted by the FAA as complying with the Minimum Performance Standards of the applicable Technical Standard Order published in FAR 21 or,
(11) 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.
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4.7 PRODUCTS OTHER THAN AIRCRAFT OR APPLIANCES
(a) Engines and propellers:- Export Certificate of Airworthiness (refer to paragraph 4.4).
(11) Service Bulletin compliance statement.
(b) Class Il as defined in sub-part L of FAR Part 21 :-
(1) FAA Airworthiness Approval Tag.
(c) Class III as defined in sub-part L of FAR Part 21 :-
(1) FAA Airworthiness Approval Tag, or A certification by the manufacturer of the product that the product concerned was manufactured under a Production Certificate granted under sub-part G of FAR Part 21, a Parts Manufacturing Approval granted under sub-part K of FAR Part 21, or a Technical Standard Order authorisation granted under sub-part 0 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. Applications for Bruneian certification are advised to give early notification to the DCA of any aircraft type in this classification.
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DOMINION OF CANADA - SPECIAL REQUIREMENTS (Revised February 7, 1979) Aircratt and aeronautical products, to be eiigible for export to canada, must in addition to requirements prescribed in Part 21 of the United States Federal Aviation Regulations (FAR), comply with applicable special requirements prescribed below. It should be noted that the Canadian Department of Transport (DOT) will accept for certification in Canada only those aircraft which are eligible for U.S.
certification as "standard" aircraft and have been manufactured in the United States under a Type Certificate currently issued in accordance with FAR Z1.21.
Thque lutes "raitation i spect tol"by De "etment of tr" sport it accichance with Part I, Chapter II, Section 2.10.2.4 of the Engineering and Inspection Manual.
Persons wishing to export transport category aircraft to Canada shall contact the DOT for policies and procedures governing such export.
a. An export certificate of airworthiness will be required by the DOT for products exported to Canada will be processed in accordance with the provisions contained in FAR Part 21, Subpart L.
b. An aircraft exported to Canada, except as indicated in paragraph c below, shall not have been flown for any purpose other than that required to accomplish the manufacturer's production flight test, flight tests for modifications, crew training flights for Canadian purchaser, and such time as may be involved in effecting delivery.
c. Used aircraft may be exported to Canada, provided that such aircraft comply with the export certification requirements in FAR Part 21, are certificated in the "standard classification", and are accompanied by records or logbooks applying to the aircraft and engine(s).
NOTE: Used aircraft exported from the United States without an Export Certificate of Airworthiness are eligible for a Canadian Certificate of Airworthiness when the ITRAN requirements of Part 1, Chapter Il, Section 2.9, of the Canadian Department of Transport Engineering and Inspection Manual have been complied
d. Ski and ski installations must be designed to meet the requirements of the DOT Engineering and Inspection Manual Part II, Chapter I, Sections 1.1.39 and
1.1.40.
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e. When the first aircraft of a type is exported to Canada, the exporter is required to provide the Canadian Department of Transport at no charge, seven copies of the Flight Manual, Maintenance Manual, Structural Repair Manual, illustrated parts catalog, and service bulletins and subsequent amendments chereto. When a model - of an aircraft type not previously registered in Canada is exported to Canada, seven copies of the new Manuals or appropriate amendments and Service Bulletins must be provided. In the case of transport category aircraft, the required number of copies of manuals may be negotiated with the Canadian Department of Transport when the aircraft are exported to Canada.
f. United States exporters of aircraft and aeronautical products manufactured in a country other than the United States should contact the Department of Transport for certification policies and procedures.
Airworthiness issued on or after July 1, 1981, U.S. exporters of aircraft must comply with the Flight Manual Requirements as specified in Transport of Canada regulation "Engineering and Inspection Manual" (Part II, Chapter 1, Sections 1.12 and 1.13). This regulation is on file at all FAA aircraft certification and regional offices and must be complied with before an FAA export approval can be issued, when applicable to the particular aircraft being exported.
To facilitate the licensing of aircraft, the following documentation should be forwarded to the Regional Administrator of the Region in which the purchaser resides (address of the six Regional Offices of the Canadian Department of Transport may be found in paragraph 4):
a. Export Certificate of Airworthiness;
b. Evidence of transfer of ownership to the Canadian purchaser from the last U.S. recorded owner, or the manufacturer in the case of a new aircraft; and,
c. The appropriate Canadian Regional Administrator should be informed by telegram or telex of the issuance of an Export Certificate of Airworthiness for an aircraft being exported via flyaway to Canada.
(1) The following is an example of the telegram referred to above:
Regional Administrator Canadian Air Transportation Administration Transport of Canada 739 West Hastings Street Vancouver, British Columbia V6C 1A2
Export Certificate of Airworthiness E-covering
(Make and Model of Aircraft) Department of Trans tre, other, ontario, lata, RiA One a model, contact the 40
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SERIAL NUMBER ASSIGNED
CANADIAN IDENTIFICATION MARKINGS PURCHASED BY BEING PREPARED.
(Canadian Purchaser)
JOHN DOE
FAA INSPECTOR or
JOHN DOE DMIR No. 6666
JOHN DOE
FAA DELEGATION OPTION MANUFACTURER (NAME OF COMPANY).
(11) The responsibility for having the telegram forwarded and any expense involved lies with the exporter.
3. Flyaway aircraft exported to Canada:
Aircraft being exported to Canada via flyaway must display Canadian nationality and registration marks.
b. Registration marks will be issued by a Regional Office on Application by the Canadian purchaser.
4. Listed below are the addresses (and the geographical boundaries) of the six Regional Offices of the Canadian Department of Transport:
a. Pacific Region Regional Administrator Canadian Air Transportation Administration Transport Canada 739 West Hastings Street Vancouver, British Columbia, Canada Note: (British Columbia, excluding the area North and east of a line ten miles west of the Alaska Highway) 41
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b. western Region Regional Administrator Canadian Air Transportation Administration Transport Canada Federal Building 9820 - 107th Street Edmonton, Alberta, Canada T5K 1G3 NOTE: (Alberta, the Northwest Territories west of the 1l0th meridian, Yukon Territory and that part of British Columbia north and east of a line ten miles west of the Alaska highway, Including Deace Lake, British Columbia).
C. Central Region Regional Administrator Canadian Air Transportation Administration Transport Canada P.O. Box 8550 Winnipeg, Manitoba, Canada R3C OP6 Nolt: (manitoba, Saskatchewan, western Ontario as far east as the 88th meridian and the Northwest Territories lying to the north, more particularly described as follows: That part of Canada bounded by the meridian of 110°W, the Canada - United States border between 110°W, and 88°W, the meridian of 88°W, the meridian of 88°W between the Canada - United States border and latitude 60°N, the parallel of 60° North latitude between 88°W and 80°W and the meridian of 80° West, north of 60°N but not including Mansel Island).
d. Ontario Region Regional Administrator Canadian Air Transportation Administration Transport Canada 4900 Young Street Suite 300 Willowdale, Ontario, Canada M2N 6A5 NOTE: (Ontario east of the 88th meridian).
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e. QUEBEC REGION Regional Administrator Canadian Air Transportation Administration Transport Canada P. O. BOx 5000 Montreal International Airport Dorval, Quebec, Canada H4Y 1B9 NOTE: (Quebec and those parts of the Northwest Territories to the north and east of the Central Region, not including the Magdalen Islands and Labrador).
Atlantic Region Regional Administrator Canadian Air Transportation Administration Transport Canada P. 0. Box 42 Moncton, New Brunswick, Canada EIC 8K6 NOTE: (New Brunswick, Nova Scotia, Prince Edward Island, Newfoundland, including Labrador, and the Magdalen Islands).
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REPUBLIC OF FRANCE - SPECIAL REQUIREMENTS (Revised June 1, 1978) INTRODUCTION.
Effective October 12, 1968, to be eligible for a French standard airworthiness certificate, an aircraft imported into France must be of a type which has been issued a French type certificate for import, except as provided in paragraph 2.a.(2) of these special requirements. In addition, U.S. manutactured aircraft must meet the export rules in Federal Aviation Regulations (FAR) Part 21, subpart L. The requtrements for issuance of French type certificates are contained in Conditions de Navigabilite des Aeronefs CivileArrete of September 1967," (for convenience, referred to hereinafter as the "CNAC") and in French Circular No. 5403 DIA/M, S.G.A.C. dated November 13, 1968. Other French documents and circulars also apply, as referred to in the text that follows.
Copies of French documents and circulars can be obtained from the French Embassy or the Ministere des Transports Aeirens, Secretariat General a l'Aviation Civile, 3 Boulevard de Montparnasse, Paris be, France. Since a French type certificate for import is a prerequisite to issuance of a french airworthiness certiticate, these special requirements include an outline of the general requirements for obtaining such type certificates.
b. Class II and III products will be exported in accordance with the provisions prescribed in Part 21, Subpart L of the united States Federal Aviation Regulations. In particular, each class II and III product will be exported with an Airworthiness Approval Tag. Aeronautical authorities of the importing country (S.G.A.C.) shall promptly advise the aeronautical authorities of the exporting country of any additional requirements which the importing country finds necessary to insure that the products meet a level of safety equivalent to that which be effective for a similar product produced on the importing state. This will be confirmed by the importing agent on his orders.
2. REQUIREMENTS FOR ISSUANCE OF FRENCH AIRWORTHINESS CERTIFICATES AND PERMITS.
d• Standard Airworthiness Certificates.
(1) Except as provided in paragraph 2.a. (2), a U.S. Export Certificate of Airworthiness, FAA Form 8130-4, may be exchanged against a French airworthiness certificate only if the following requirements have been met.
(a) The aircraft type must have a French type certificate for import.
(b) The requirements of Article 11B of the CNAC must be complied with.