Appendix 1 PART I) ~ APPLICATION FOR APPROVAL OF AERONAUTICAL PARTS (Complete items 12-20)
12. Neme and address of exporter 13. Name and address of loreign purchaser 14. Country of destination ABC Airplane Corporation Aviation Supplies Led.
Cleveland, Ohio 44111 London, England United Kingdom
15. Parta are eligible for installation on Make and model Class | produci FAGAT*C No.
ABC Airplane Model C-5
15. The parts are (check one) iS NEW • NEWLY OVERMAULED
17. The parts are described (Check ones Invoice/packing sheet No.
D: Below by name. part number. • On the attached invoice or packing sheel.
and quantity by name, part number and quantry Name Pan number Quantity (a] IDI Aileron A-456-4 (S/N 113 and 2 ва.
114) Elevatory Assy. 4-789-2A (S/N 285 and 2 ea.
290)
18. Have applicable special requirements of the importing country been compiled with? IS YES • NO (Explain in ler 10 "Aemarks")
19. Preservation and packaging meinods used to protect parts agsinst corrosion and damage I List Spec. No. or Tille.
Ellecive duration olabove melhods: ABC Airplane Corporation Specificacion $44, (Preservation-corrosion).
20. EXPORTER'S CERTIFICATION-I certily that ina foregoing statements are true and that ine paris described hereir. are sivorny.
conform to FAA approved design data. and are in condition for sale operation excadi as may be noted in item 10 • Remarks Signaturg of applicant or authorized representative Title Dale initi Smith Sales Manager October 30, 1991 Part III - APPROVAL (FOR FAA USE ONLY)
21. Il is considered that the products) described in Part i or Part il ta (are) airworthy and conform (s) to pertinent requirements except as noted in ilem 10. (Check oner • Part • Part II Sıgnature Number Dale (Check one) - • • OMIR • DAR • DELEGATION OPTION MFR. • FAA INSPECTOR
22. Give quantity of approval tags, FAA For 8130-3, Issued for the parts described in Part II. - Quantily
23. EXPORT FILE SPOT-CHECKED BY:
FAA Supertaing Inspector D.O. No. Date Figure 2. Completed FAA Form 8130-1, Application for Export Certificate of Airworthiness - (Reverse Side) For Use with Class II Products 2
Appendix 1 The niced States of America Department of Transportation Federal Aviation Administration No. E30016 20ashtngcon, 29.C.
Export Certificate of Airtuorchiness This ties that the product ide nified dalene and mum particularly deviled in. Specification (s) of the Fedoral Aviation: Idministration, Numbored 6A17, E88, and P99 has been scamined and as of the date of this sortificole, is considoned airenthy in accordance with a comprehensive and detailed airunthiness code of the United Sales Govemment, and is in compliance with those special requivements of the importing country filed with the United Plates Invernment, arepl as nded below. This contificate in no sony attests to compliance with any agreements on contracks belveen the vender and purchaser, men does it constitute autherity le sporale an sincreft.
Preduct: Airplane Engine Model AIRECO I0-470-2 Manufacturer: ABC AIrplane COIP. Serial Nos. 18976 and 18978 Total Time 50 hrs. and 51 hrs.
Model: C-5 terial Ar.: 2468 Propeller Model:
Senhart SC-82XK-2 hub with Ace I Acudy Prentrated • X8498C-2 blades, Hub Serial Nos. 21375 and 21412.
Used Slincrap D Total Time 50 hrs. and 51 hrs.
Gruntry lewhich saported: JaPBN Cace/lions: A temporary auxiliary fuel system has been installed in this aircraft In conformity with ABC Drawing AF-1 to facilitate its delivery flight. This certificate is valid when the temporary installation is removed.
Total Time since annual/100 hour inspection Aircraft 2 hours Engine (s) 2 hours (L/H) S/N 18976, 2 hours (R/H) S/N 18978.
Propeller (s) 2 hours (L/H) S/N 21375, 2 hours (R/H) S/N 21412.
Smith R. Smith: FAA Delegation Option Authorization Signature of Authorized Represeniattre October 1, 1991 ABC Airplane Corp. (PC75) Date District Offue or Designer Aumber Applice spectate of type entice at she Type Caritar to this on set for, tinath een jorand ped to l appropriale governmental ofice of the importing country, FAA Form B130-1 (7-6B) Formerty Fom FAA 20 $ U.8. GOVERNMENT PRINTINO OFFICE: 1974 - 779-238/138/7 Figure 3. Completed FAA Form 8130-4, Export Certificate of Airworthiness - Issued for Class I Products
Appendix 1
3. Certificate Rof. No. 5. Work Order/Contract/Invoice W.O. # 108432 12. Status/Wrk 11. Serial/Batch No. NEW S/N 64532 NEWLY OVERHAULED S/N 3867 NEW S/N 87-1603 Certifies that the work specified above except as olherwise specified in block 13 was cared out in accordance with the airworthiness regulations of the stated country and the notified special requirements of the importing country and in respect to that work, the parts) is (are) in condition for safe operation and considered ready for release (over) 19. Issued by or on behalf of the Federal Aviation Administration. CE FSDO 03 Cross-check eligibility for more details with parts catalog
10. aty.
AIRWORTHINESS APPROVAL TAG 9. Eligibility* a. Part No. G159 159AV10170-1 G-159 159H1305-1 TSO-C62 6.50X8 ITEM 2 - A.D. 88-XX-XX C/W T.S.O. -0 T.S.N.-1345 SEE ATTACHED MAINTENANCE 15. Used Parts: Certifies that the parts) identified above except as otherwise specified in block 13 was (were) manufactured/inspected in accordanca with the airworthiness regulations ot the staled country andror in the case of pars to be exponed with the approved design data and with the notified special requirements of the importing country. to service. 18. Dale 10/1/91
1. Country UNITED STATES US Deporment of transportoson Federal Antation Administrution ABC MANUFACTURING CO. 4. Organization 13976 WEST 47ch ST. SAINT LOUIS, MO 31400 7. Description 6. Item NOSE WHEEL WELL, JUNCTION BOX ASSY. MAIN GEAR DOWNLOCK CYLINDER ASSY. TIRE TYPE III, 8 PLY RATING 13. Remarks RELEASE 14. New Parts: 16. Signatur mitt 17. Name (typed or printed) J. R. SMITH A.S.I. FAA Form 8130-3(9-88) Figure 4. Completed FAA Form 8130-3, Airworthiness Approval Tag - Issued for Class II Products 4
Appendix 2 APPENDIX 2 - SPECIAL REQUIREMENTS OF IMPORTING COUNTRIES This appendix contains special requirements which have been stipulated by a number of governments as being applicable to aeronautical products imported into their countries from the United States. Revisions of the appendix will be made from time to time following receipt of official notification and documentation from the governments concerned.
The material in appendix 2 is quoted from the requirements submitted by import countries, therefore, changes were not made to conform to the Government Printing Office Style Manual or FAA directives. where the FAA added information for clarification, the information is enclosed in double brackets.
The following governments have filed their requirements with the Federal Aviation Administration.
Appendix 2 Page No.
Argentina Australia..
Bangladesh Belgium 13 Bolivia 17 Botswana 19 Brazil 21 Brunei Darussalam 30 Canada 37 France 47 Germany, Federal Republic of 56 Guatemala 68 Honduras 69 Hong Kong • 70 India Indonesia Ireland Israel Italy Japan • Korea, Republic of 7 Lebanon Malaysia MorOcco Netherlands, The Netherlands Antilles 122 New Zealand 126 Pakistan Panama, Republic of Philippines.
Portugal Saudi Arabia
Appendix 2 Appendix 2 Page No.
Singapore 147 South Africa, Republic of 151 Spain 153 Sweden 157 Switzerland 162 Syrian Arab Republic 166 Taiwan 167 Tunisia 173 United Kingdom 174 Yugoslavia 192 Zambia 196
zimbabwe .......198
Appendix 2
REPUBLIC OF ARGENTINA - SPECIAL REQUIREMENTS (Revised January 30, 1976)
1. In order to be eligible for certification by the Argentine Government, Class I aeronautical products must be covered by Export Certificates of Airworthiness as provided for in Part 21 of the United States Federal Aviation Regulations. Complete aircraft (new or used) to be registered in the Argentine Republic will require the following documents:
a. Export Certificate of Airworthiness, FAA Form 8130-4.
b. Record of aircraft and engines, including logbooks.
Copy of the Airplane Flight Manual (AFM) approved by the Federal Aviation Administration written in accordance with the guidelines contained in International Civil Aviation Organization Circular 65-AN/59. The basic sections of the manual may include I - General, and must include II - Operations Limitations, III - Normal Operating Procedures, IV - Emergency Procedures, V - Performance, and VI - Weight and Balance.
(1) In the case of airplanes certificated in the transport category, this flight manual may be in either English or Spanish.
(2) In the case of airplanes certificated in the normal utility, acrobatic and restricted categories, this flight manual must be written in Spanish, and in addition, must include the following:
(i) Appendix I. A listing of all engines and propellers and all combinations thereof approved for use on the airplane.
(ii) Appendix II. Supplements to Airplane Flight Manual.
(iii) Appendix III. A list of manual revisions incorporated.
(iv) Annex. Three blank pages labeled Reserved for Aircraft Inspector.
d. Copy of the weight and balance report and equipment list.
e. Major Repair and Alteration Form, FAA Form 337, or equivalent, if repairs and/or alterations have been accomplished on the exported aircraft.
2. Class II and Class III products shall be exported in accordance with the provisions prescribed in Part 21 of the United States Federal Aviation Regulations.
Appendix 2
COMMONWEALTH OF AUSTRALIA - SPECIAL REQUIREMENTS (Revised March 1991) SECTION 1 - INTRODUCTION. A bilateral agreement between Australia and the United States (U.S.) came into effect by the Exchange of Notes in December 1974 and June 1975 and superseded the agreement of 1959 relating to the reciprocal acceptance of aeronautical products.
The manner in which this agreement will be implemented is described below.
A. Administration and Procedures.
(1) The procedures which must be followed to obtain Australian import certification are dealt with in the current issue of Part 100 of Australian Civil Aviation Orders (CAO's).
(2) A U.S. Export Certificate of Airworthiness for export to Australia (or agreed alternative) with pertinent data will be required in connection with any Class I product and engine modules exported from the United States to Australia. Class Il and Class III products to be eligible for installation on certificated civil aircraft registered in Australia must be processed in accordance with the applicable provisions of Part 21 of the United States Federal Aviation Regulations. The requirement for an Export Certificate of Airworthiness for an aircraft exported to Australia may be waived on production, to the Australian CAA delegate, of:
(i) documentary evidence that the aircraft was registered in a Contracting State and that a standard Certificate of Airworthiness in accordance with ICAO Annex 8 was in force in respect of the aircraft at the time of export from the Contracting State;
(ii) certification by the holder of an appropriately rated Certificate of Approval that the aircraft has been inspected in accordance with manufacturer's instructions for continued airworthiness to the extent necessary to establish that the aircraft is satisfactory for the issue of an Australian Certificate of Airworthiness; and
(111) certification, made in relevant log books by the Certificate of Approval holder that, following an inspection of the WeEd with the relevant type certifiese Doc Sheet and apsicable suppiemental lype Certiricates and all modiiications comply with the applicable design standards.
(3) Where the issue of an Export Certificate of Airworthiness is relevant, the certificate shall be issued within a period of 90 days or 50 operating hours, whichever is the lesser period, immediately preceding the date of application for Australian certification or validation, as appropriate, except as otherwise 4
Appendix 2 acceptable to Australia in a particular case. The Export Certificate of Airworthiness shall be accompanied by a document (e.g•, aircrait logbook), furnished by the applicant, which contains entries identifying those applicable FAA Airworthiness Directives (AD's) with which compliance has been achieved. This document shall also identify those AD's containing repetitive compliance requirements, and when compliance is next due to be satisfied. All applicable FAA AD's must have been complied with prior to issuance of the U.S.
Export Certificate of Airworthiness.
The applicant for a U.S. Export Certificate of Airworthiness is also responsible for satisfying all other Australian Special Requirements (identified in Section 2), as appropriate, ior the particular product being exported to Australia and all applicable sections of FAR 21, Subpart L, before the U.S. Export Certificate of Airworthiness can be issued.
(5) Copies of CAO's may be perused at the various aircraft certification or regional offices of the Federal Aviation Administration, or may be obtained by mail from the Civil Aviation Authority Publication Centre, P.O. Box 1986, Carlton South, Victoria, 3053, Australia, Facsimile No. 61-3-3474407.
B. Acceptance of Aircraft.
(1) Prior to issue of a Certificate of Airworthiness to an aircraft exported to Australia, the aircraft must be of a type and model as defined on the FAA Type Certificate Data Sheet or Specification that either:
(a) has previously been issued with a Certificate of Airworthiness by the Australian authority; or
(b) is the subject of a Certificate of Type Approval issued by the Civil Aviation Authority of Australia.
(2) The Civil Aviation Authority may require documents other than the FAA Type Certificate and Type Certificate Data Sheet to be supplied for continuing airworthiness control purposes prior to issue of the first Australian Certificate of Airworthiness on a new type or model. Design familiarization for technical specialists may also be required for the same reason.
Compliance with Australian Air Navigation (Aircraft Noise) Regulations is required. Subsonic jet aircraft added to the Australian register after January 1, 1991, will not be permitted to operate unless they meet ICAO Chapter 3 noise standards.
C. Acceptance of Engines, Auxiliary Power Units, and Propellers.
(1) Aircraft engines, auxiliary power units, and propellers which are exported to Australia as spares, i.e., not as parts oi e particular aircraft, to be eligible for use on Australian aircraft 5
Appendix 2 must comply with the type design, be new or newly overhauled as defined in Part 2l of the United States FAR's and have a relevant logbook. Before installation in, or fitment to, an aircraft in Australia, such products are required to conform with any applicable Australian Airworthiness Directives.
(2) A U.S. Export Certificate of Airworthiness will be accepted as evidence that an engine or propeller conforms with the type design and is either new or newly overhauled as the case may be.
(3) Engines and propellers need not incorporate modifications or manufacturers service documents made mandatory by Australian AD's prior to export of the product to Australia.
However, since it may be difficult to determine in Australia whether the product complies with the mandatory documents, information as to the modification status of a particular product would be of help to the Australian user. An appropriate statement, either in a logbook or separately issued by the person or organization issuing the U.s.
Export Certificate of Airworthiness or appropriate certification document, will be accepted as evidence of the modification status.
D. Acceptance of Appliances and Components.
(1) Items classified as Class II and Class III products by FAR 21 (Subpart L, Section 21.321) and which are exported to Australia as spares, i.e., not as parts oi a particular aircrait, nust conform to the type design and must be new or newly overhaulec as defined in FAR 21 in order to be eligible for use on Australian aircraft. Before installation in, or fitment to, an aircraft in Australia, such products are required to conform with any applicable Australian Airworthiness Directives.
(2) An Airworthiness Approval Tag, FAA Form 8130-3, issued in accordance with the requirements of FAR 21, or other document specified in CAO's Part 100* or otherwise specified or approved by the CAA, will be accepted as evidence that the products conform with the type design and are either new or newly overhauled.
Products need not incorporate modifications or manufacturer's service documents made mandatory by Australian Airworthiness Directives. However, since it may be difficult to determine in Australia whether the product complies with the mandatory documents, information as to the modification status of a product would be of help to the Australian user. A statement by the person issuing the airworthiness approval tag or alternative document will be accepted as evidence of the modification status of the products.
*Documents specified in CAO's Part 100 for this purpose are detailed in Section 2, Special Requirements (paragraph c).
Appendix 2 E. Restricted and Limited Category Aircraft. Aircraft certificated in the United States only in the Restricted Category could be eligible for export to and certification in Australia in the Agricultural Category in accordance with Section 101.17 of the CAO's.
Aircraft certificated in the United States only in the Limited Category will not normally be eligible for certification in Australia.
SECTION 2 - SPECIAL REQUIREMENTS. The following identifies those special administrative requirements which must be satisfied at the time of export, for a particular product to be eligible for Australian airworthiness acceptance.
A. Aircraft, First of a Particular Type or Model.
(1) An Export Certificate of Airworthiness may be issued when the aircraft complies with FAA requirements.
(2) An Australian Certificate of Airworthiness will, however, only be issued after issue of an Australian Certificate of Type Approval, flight manuals have been submitted and approved, all maintenance publications have been received and compliance with Civil Aviation Order Section 100.2 established.
FAA approved Supplemental Type Certificates (STC) are now automatically acceptable in Australia. STC's must be listed on the Export Certificate of Airworthiness and any required Flight Manual Supplements will be required to comply with Australian requirements and be approved by the Australian CAA prior to issue of an Australian Certificate of Airworthiness.
(4) Applicants for first-of-type acceptance of aircraft in the Transport Category should anticipate being expected to comply with an Australian Maintenance Requirements Document.
B. Aircraft Not First of a Particular Type or Model.
(1) An Export Certificate of Airworthiness may be issued when the aircraft complies with FAA requirements.
Australian Certificate of Airworthiness.
C. Aircraft Products and Components.
(1) In the case of FAA Class I products. A United States of America, Federal Aviation Administration Form 8130-4 (Export Certificate of Airworthiness);
Appendix 2
(2) In the case of FAA Class II products. A United States of America, Federal Aviation Administration Form 8130-3 (Airworthiness Approval Tag) ;
(3) In the case of FAA Class III products.
(i) A United States of America, Federal Aviation Administration Form 8130-3 (Airworthiness Approval Tag); or
(ii) A Technical Standard Order (TSO) authorization granted under United States of America, Federal Aviation Regulations Part 21, Subpart 0; or
(iii) A document issued by the manufacturer of the component and which contains a certification to the effect that the component was manufactured under;
(a) A Production Certificate granted under United States of America, Federal Aviation Regulations Part 21, Subpart G;
or
(b) An FAA Parts Manufacturing Approval (PMA) granted under United States of America, Federal Aviation Regulations Part 21, Subpart K.
(4) In the case of any aircraft component. A document issued by an FAA Certificated Repair Station and which quotes the certificate number issued to that Repair Station under United States of America, Federal Aviation Regulations, Part 145.
NOTE: Class I, II, and III are defined in United States of America, Federal Aviation Regulations, Part 21, Subpart L, Section 21.321.
SECTION 3.- VALIDATION. The CAA has the facility to validate a U.S.
Certificate of Airworthiness or Export Certificate of Airworthiness, for the purposes of aircraft delivery to Australia, if the applicant wishes to place the aircraft on the Australian Register of Aircraft, but does not wish that an Australian Certificate of Airworthiness be issued for such delivery. A Flight Manual validation certificate will normally be processed at the time of validation certificate processing. Particular restrictions are applied to flight on a validated foreign Certificate of Airworthiness.
• 8
Appendix 2
PEOPLE'S REPUBLIC OF BANGLADESH - SPECIAL REQUIREMENTS (Revised July 6, 1989)
1. INTRODUCTION.
1.1 To be eligible for certification by the Government of the People's Republic of Bangladesh, all Class I, II, and III products should be issued export Certificate of Airworthiness or Export Airworthiness Approvals in accordance with the provisions of Subpart L of Part 21 of the Federal Aviation Regulations.
1.2 All correspondence regarding Registration and Certification of civil aircrafts should be address to:
AIRWORTHINESS & ENGINEERING LICENSING DIVISION
CIVIL AVIATION AUTHORITY OF BANGLADESH
HEADQUARTERS
ZIA INTERNATIONAL AIRPORT
KURMITOLA DHAKA-1206 BANGLADESH AFTN: VGHQYAYL
2. DOCUMENTS AND ADDITIONAL REQUIREMENTS.
2.1 In addition to the foregoing, one copy of the following documents/materials shall be furnished by the Manufacturer to the Chairman CAAB and also the subsequent revisions.
A. NEW AIRCRAFT. (DOCUMENTS AND RECORDS).
(a) Type Certificate.
(b) Type Certificate Data Sheet.
(c) Supplemental Type Certificate (if any).
(d) Complete list of Service Bulletins incorporated in the production version of the aircraft.
(e) List of Customer requested modifications incorporated.
(f) Aircraft, Engine, Propeller, and APU log book with total time in service.
(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 Operator.
(h) List of all service bulletins incorporated on the aircraft, engine, propeller, and appliances as applicable.