the serial number of the aircraft and the total number of operating nours (2) lne appication for the Export Certificate of Airworthiness reflects accumulated. The aircraft engine(s) and propeller(s) should also be identified by serial numbers followed by the total number of operating hours of each and the total elapsed time since the last 100 hour/annual inspection if such inspection has been accomplished; and
(3) The U.S. Export Certificate of Airworthiness reflects the information required by paragraph 14b(2).
controversy or is contrary to existing foreign government special requirements, the exporter should be advised that the issue is to be settled between the c. If for any reason the previously listed information results in a exporter, importer, and the civil air authority of the importing country.
Willem Sullin William J. Sullivan, Acting Director of Airworthiness 8 Par 14
AC 21-2F ฿/7/87 Appendix 1 APPENDIX 1 - SAMPLE FORMS
FORM APPROVED O M.U No. 2120-0018
APPLICATION FOR EXPORT WS 090 or trampartasa CERTIFICATE OF AIRWORTHINESS Export Certilicate No E30016 INSTRUCTIONS — This application is to be submitted to an suthorized FAA representalive (one copy) when the product(s) to be exporied is (are) presented for inspeclion. Use Part I for Class I products and Part Il for Class Il Forcomplele aircrati execule items 1 l through 11, as applicable. For engines and propellers, omit item SA Part Ill is for FAA use only.
Part I - APPLICATION FOR EXPORT CERTIFICATE OF AIRWORTHINESS (Complate llams 1-11).
1. Application la made for an export certificate of airworthiness to cover the produci(a) described below which ta (are):
2. Name and address of exporter LI NEW • USED (Aircraft) 3. Name and address of foreign purchaser • NEWLY OVERHAULED 4. Country of destnation ABC Airplane Corporation Cleveland, Ohio 44111 Tokyo News Service Tokyo, Japan JAPAN $. Description of product(s) Type Make and model (b} Identification No. Serial No$ (C} Spec. No FAA (d) Operating time (Hours) overheul Since (Đ) Total A AIRCRAFT Model C-5 ABC Airplane Corp. I JA-VOX 2468 6A17 51 AIRECO (L/H) 18976 2-88 50
• ENGINES Model 10-470-2 (R/H) 18978 51 Senhatt (L/H) 21375 50 C. PROPELLERS Ulub Model: SC-82XK-2 Blade Model: X8498C-2 (R/H) 21412 P-99 51
6. Does the product comply with all applicable Federal Aviation Regulations,
• YES " NO (Explain in "Remarks")
7. Have applicable special requiremente of the importing country been compiled with?
• YES • NO (Explain in "Romarks")
•. Date thie passed or la expected to pass to foreign purchaser: Apr 11 29; 1986
8. For oversess shipment, preservation and packaging methods used to protect produci(s) agalnal corrosion and damage (List Spec. No. ur Trilar Effecthe duration ofabore methods: Not applicable to Fly-away delivery.
10. Remake The aircraft described above complies with all applicable FAA requirements, except that a temporary auxiliary fuel system has been installed for the delivery flight.
Documenta required by FAR 21.327, as applicable, arc provided herewith.
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 (a) 2 hours (L/H) S/N 21375, 2 hours (R/H) S/N 21412.
11. EXPORTER'S CERTIFICATION - The undorsigned certifies that the above statemenis are true and that tho products) described hersin is (are) airworthy and in condition for safe operation except as may be noted undur item 10 "Ramarks." above Lada pagan grauthorized representativ Tille Dato JOHN D. DOE Sales Munager Apr11 29, 1986 FAA Form 0130-1 (7 eu) Supersedes Previous Edition Figure 1. Completed FAA Form 8130-1, Application for Export Certificate of Airworthiness - For Use with Class I Products
Appendix 1 PART II - APPLICATION FOR APPROVAL OF AERONAUTICAL PARTS (Complete iranis 12-20)
12. Name and address of exporter 12. Name and address of loreign purchaser 14. Country of destination ABC Airplane Corporation Aviation Supplies Ltd.
Cleveland, Ohio 44111 London, England United Kingdom
15. Parta ara eligible for Inatallation on - Make and model Class i product ABC Airplane Model C-5 FAA Sp. No 6A17
16. The parts are (chack one) - → • NEW • NEWLY OVERHAULED
17. The parts are described (Check one) Invoice/packing sheet No.
I Below by name, part number. and quantity • On the attached invoice or packing sheet. by name, part number and quantity - Name • (&) Parl number (b) Quantity (c) Aileron A-456-4 (S/N 113 and 2 ea.
114) Elevator Assy. A-789-2A (S/N 285 and 2 ea.
290)
18. Have applicable special requirements of the importing country been complied with? O YES • NO (Explain in item 10 "Remarks")
18. Preserration and packaging methods used to proteci parts against corrosion and damage (Lis: Spec. No. or Title):
Effecthe duraton ofabove methods: ABC Airplane Corporation Specification 244, (Preservation-corrosion).
20. EXPORTER'S CERTIFICATION-I certily that the foregoing statements are lue and that the parts described harein are airworthy.
conform to FAA approved design data, and are in condition for safe operation except as may be noted in item 10 "Remarks."
" anal po. or authored representatives John D. Due • Part III - APPROVAL (FOR FAA USE ONLY) Sales Manager March 25, 1986
21. II la conaldered that the products) described in Part I or Part Ii Is (are) alrworthy and conform (a) to pertinent requirementa except as noled in Item 10. (Check one) • Part! • Part Il Signature Number Date (Checkone) - * • OMIR O DAR • DELEGATION OPTION MFR. • FAA INSPECTOR
22. Give quantity of approval lags, FAX Form 8130-3, lasued for the parts deacribed in Part II. Quantity
33. 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 inited States of Elmerira Department of a ronsportation Federal Aviation Administration No._E30016 *Dashington, Đ.C.
Export Certificate of Airworthiness Chl STURB that the product identified televand man punticulurly descrited in Specification (s) of theiLalmd taintion Slaministrolion, Aumtered 6A17, E88, and P99.
he hoes coumined and as of the date of this serlifical, is considered virathy in ascertance with a remperhousin and dabailed nievethiness code of the luited Hales: bevenmend, and is in compliancewith these seried requimmerls of the importing sunley filed with the Waited ules Pavemesment, weft as meted tale. This carlificale in me ury allests to creepliance with any agreements on ventrols balucen the vander need purchases, nor shes il coustitule autherity le sperale an airere?.
Pastuct: Airplane Engine Model:
AIRECO 10-470-2 ABC Airplane Corp. Serial Nos. 18976 and 18978 Total Time 50 hrs. and 51 hrs.
• Model: C-5 2468 Propeller Model:
Senhart SC-82XK-2 hub with (8498C-2 blades, Hub Serial los. 21375 and 21412.
Used timeneft Total Time 50 hrs. and 51 hrs.
Gentry be hich cafe stead: Japan carplice: A temporary auxiliary fuel system heatbeens nativery fight. alrigart in conformity with ABC Drawing AF-1 to facilitate its delivery flight.
certificate is valid when the temporary installation is removed.
Total Time since annual/100 hour inspection Enopeffer(s) 2 hours (L/H) S/M 21375, 2 hours (R/H) S/N 21912: Engine(s) CR Smith LA. Smith, FAA Delegation Option Authorization mature of Austenised Representate.
May tri 980 ABC Airplane Corp. (PC7S) Distul Ofee we Designer banker Ipplicable speciation or Type Certifate ala Sheet, if not attached to this report cheflate, wai har been fortarded to it lot altnehed to this export rertifirate, will hair been forwarded to It eppropriale povernmental afire of the importing country.
Pad Form 6120-1 (7-69) Formoit, For PAA 28 -118-967 Figure 3. Completed FAA Form 8130-4, Export Certificate of Airworthiness - Issued for Class I Products
Appendix 1 FAR FORM 0130-3
SUPERSEDES
PREVIOUS EDITION US. Depertment of Transporation Federal Aslation Admintstralion
AIRWORTHINESS APPROVAL TAG
DESCRIPTION OF PARTS
I NEW - NEWLY OVERHAULED
APPROVAL BASIS IC NO. 6A17
QUANTITY, NAME AND PART NUMBER 2 Ailerons P/N A-456-4 S/N 113 S/N 114 2 Elevator Assy's P/N A-789-2A S/N 285 S/N 290
HO PRODUC INSTALLATION ONT ARCH AT VOICE Model C-5 ABC 948690
INSPECTED AND APPROVED
AGENCY HAME AND NUMBER ABC Airplane Corporation
• OF СКА ПЕРПЕВЕНТАТІУ omis Smith
FAR HUMBER March 26. 1986 DOA PC75 Figure 4. Completed FAA Form 8130-3, Airworthiness Approval Tag - Issued for Class Il Products 4
Appendix 2 APPENDIX 2 - SPECIAL REQUIREMENTS OF FOREIGN COUNTRIES
1. This appendix contains special requirements which have been stipulated by a number of foreign governments as being applicable to aeronautical products imported into their countries from the United States.
•ll be made from time to time following receipt of official notification and documentation from the foreign governments concerned.
Aviation Administration. The following governments have filed their requirements with the Federal Appendix 2 Page No.
Argentina, Republic of ... 3 Australia, Commonwealth of * . . 4 Belgium, Kingdom of.... Bolivia, Republic of ... .. ... ... 12 16 Botswana, Republic of .... . . . 18 Brazil, Federative Republic of Brunei Canada, Dominion of France, Republic of Germany, Federal Republic of Honduras, Republic of Guatemala, Republic of 65 Hong Kong • India, Republic of Indonesia, Republic of Ireland ...
Israel, State of Italy, Republic of Japan Korea, Republic of South Labanon, Republic of Malaysia Morocco, Kingdom of Netherlands, Kingdom of the Netherlands Antilles .
New Zealand, Dominion of Pakistan, Islamic Republic of Panama, Republic of Philippines, Republic of the Portugal, Republic of Saudi Arabia, Kingdom of Singapore, Republic of . South Africa, Republic of 116 118 125 127 131 Sweden, Kingdom of Switzerland, Confederation of Syrian Arab Republic 132 139 141 142 Taiwan ..
147 Tunisia, Republic of 148 Yugoslavia, Socialist Federal Republic of Zambia, Republic of Zimbabwe, Republic of United Kingdom 167 171 173 1 (and 2)
Appendix 2
REPUBLIC OF ARGENTINA - SPECIAL REQUIREMENTS (Revised January 30, 1976) 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.
c. 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 Il - 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:
(1) Appendix I - A listing of all engines and propellers and all combinations thereof approved for use on the airplane.
(11) Appendix II - Supplements to Airplane Flight Manual.
(111) Appendix III - A list of manual revisions incorporated.
(iv) Annex - Three (3) 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.
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 SECTION L - INTRODUCTION. A new Dilateral agreement between Australia and the United States (US) 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 certification are dealt with in the current issue of Part 100 of Australian Air Navigation Orders.
(2) A US 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 II 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.
(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 acceptable to Australia in a particular case. The Export Certificate of Airworthiness shall be accompanied by a document (e.g., aircraft logbook), rurnished 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 US Export Certificate of Airworthiness.
(4) The applicant for a US Export Certificate of Airworthiness is also responsible for satisfying all other Australian Special Requirements (identified in Section 2), as appropriate, for the particular product being exported to Australia and all applicable sections of FAR 21, Subpart L, before the US Export Certificate of Airworthiness can be issued.
(5) Copies of Australian Air Navigation Orders may be perused at the various aircraft certification or regional offices of the Federal Aviation Administration or at the office of the Transport Attache, Embassy of Australia, 1601 Massachusetts Avenue, N.N., Washington, D.C. 20036, mail from the Secretary, Department of Transport, Box 1839Q, G.P.O. Melbourne, or may be obtained by Victoria 3001, Australia.
Appendix 2 B. Acceptance of Aircraft
(1) In accordance with paragraph (4) of the Australia/US bilateral agreement, an aircraft exported to Australia must comply with the Section of Air Navigation Orders Part 101 specifies an acceptable basis for type certification against the CAR's or FAR's, lists certain additional validation requirements anc equires compliance to be demonstrated with all applicable Airworthiness Directives issued by the FAA and the Australian Department of Transport. In addition, documentation requirements are specified with respect to first-of-type and subsequent aircraft, with provision for certain additional data relating to service history to be supplied in the case of used aircraft.
Australia will require to become conversant with the design of all fixed wing aircraft in excess of 5700 kg (12,566 lbs.) weight, and all multi-engine rotorcraft offered for Australian certification. Additionally, the Department of Transport may require to evaluate certain other aircraft which have unusual design features. The Department of Transport may then issue special conditions to cover certain features which would otherwise not meet the standards implicit in the Australian Air Navigation Orders.
(3) Once the Australian standard for certification has been determined, and, where necessary, Australian special conditions have been notified, Australia vill in accordance with paragraph 9(h)(ii) of the Australia/US bilateral agreement accept aircraft and rotorcraft to the standard defined in these special conditions, together with the applicable FAR Airworthiness Directives and dustralian Airworthiness Directives while they continue in production.
Modifications to the aircraft may also be made provided the requirements used as the basis of Australian certification are complied with, or alternatively that the Department of Transport otherwise agrees that the modifications made are acceptable.
(4) Aircraft may be issued with Australian certificates of airworthiness in one or more of the following categories:
Transport;
Normal;
Utility;
acrobatic, _ toricultural:
Developmental; and Special.
The Sections of Air Navigation Orders Part 101 relevant to civil aircraft constructed in the United States of America, its territories and possessions and exported to Australia are:
Appendix 2
(i) Iransport Category
(a) A.N.O. Section 101.4, 'Imported Aeroplanes Not Above 5700 kg in the Transport Category."
(b) A.N.O. Section 101.6, Imported Turbine Aeroplanes Above 5700 kg Designed to CAR and FAR.
5700 kg Designed to CAR And FAR.ction 101.8, "Imported Piston Aeroplanes Above CAR and FAR in the Transport Categoro. 101.10, imported Rotorcraft Designed to
(11) Normal, Utility, and Acrobatic Categories
(a) A.N.O. Section 101.22, Imported Aeroplanes in the Normal, Utility and Acrobatic Categories."
(b) A.N.O. Section 101.24, Imported Rotorcraft in the Normal Category.
(111) Agricultural Category. A.N.O. Section 101.17, Imported Aeroplanes Not Above 5700 kg in the Agricultural Category."
(iv) Developmental Category. A.N.O. Section 101.31,Developmental Aircraft."
There are other Sections of Air Navigation Orders relating to aircraft designed against the British Civil Airworthiness Requirements, while the requirements for the Special Category are advised as special conditions to suit individual cases not provided for in the other categories.
C. Acceptance of Engines, Auxiliary Power Units and Propellers (L) Aircraft engines, auxiliary power units and propellers which are exported to Australia as spares - i.e., not as parts of a particular aircraft - to be eligible for use on Australian aircraft must comply with the type design, be new or newly overhauled as defined in Part 21 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 United States Export Certificate of Airworthiness will be accepted as evidence that an engine, auxiliary power unit or propeller conforms with the type design and is either new or newly overhauled as the case may be.
Appendix 2
(3) Engines, auxiliary power units and propeller need not incorporate modifications or manufacturers' service documents made mandatory by Australian rworthiness Directives prior to export of the product to Australia. However, since it may de 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 United States export certificate of airworthiness 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 of a particular aircraft - must conform to the type design and must be new or newly overhauled as defined in FAR 21 in order to be eligible for use on Australia, Such artducts are reguild to inform fith aty apparable 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 Air Navigation Orders Part 100* or otherwise specified or approved by the Department of Transport, will be accepted as evidence that the products conform with the type design and are either new or newly overhauled.
(3) Products need not incorporate modifications or manufacturers' 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.
Restricted and Limited Category Aircraft Aircraft certificated in the United States only in the Restricted Category normally will be eligible for export to and certification in Australia only in the agricultural category in accordance with Section 101.17 of the Air Navigation Orders. Aircraft certificated in the United States only in the Limited Category will not normally be eligible for certification in Australia.
*Documents specified in Air Navigation Orders Part 100 for this purpose are detailed in Section 2 - Special Requirements (paragraph c).
Appendix 2 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 or validation.
A. Aircraft, First of a Particular Type or Model
(1) An Export Certificate of Airworthiness may be issued when it has been demonstrated to the responsible region of the FAA that the aircraft complies with the requirements of the appropriate Section of Part 101 of Air Navigation Orders. Alternatively, such an Export Certificate of Airworthiness may be issued when it has been demonstrated to the Department of Transport that the aircraft complies with the appropriate Section of Part 101 of Air Navigation Orders and the Department of Transport has advised the responsible region of the FAA in writing of its acceptance of the aircraft. The Section against which the aircraft has been demonstrated to comply should be endorsed in the Export Certificate of Afrworthiness. The following guidance is offered:
(i) Export airworthiness approval of aircraft located outside the United States of America, its territories or possessions will be subject to the provisions of subparagraph (b)(2), Section 21.325, Part 21, of the Federal Aviation Regulations.
(11) Compliance with the requirements of Air Navigation Orders may be demonstrated to an authorized officer or officers of the Australian Department of Transport. These officers will normally visit the United States to assess compliance only in the case of aeroplanes of maximum takeoff weight greater than 5700 kg (12,566 1bs.) or multi-engine rotorcraft.
(2) In some circumstances it may be impossible or undesirable to show that an aircraft complies with all the requirements of the appropriate Section of Part 101 of Air Navigation Orders until the aircraft arrives in Australia.
Similarly it may be more appropriate that modification to achieve compliance with the Air Navigation Orders be deferred until the aircraft arrives in Australia.
these circumstances an Export Certificate of Airworthiness may be issued when it has been demonstrated to the responsible region of the FAA that the aircraft complies with much of the requirements of the appropriate Section of Part 101 of the Air Navigation Orders as are desired and the requirements not complied with are clearly established. The Export Certificate of Airworthiness will be endorsed with those exceptions and with the applicable Section of Air Navigation Orders Part 101 against which the demonstration has been made. The following guidance is offered:
(1) Circumstances in which it may not be possible to demonstrate compliance with the requirements before export include the following: