(2) Item 16 - Parts are Eligible For Installation on: Insert the make and model of the aircraft, engine, or propeller on which the Class II products (parts) are eligible for installation, and the FAA specifications or type certificate data sheets applicable to such aircraft, engine, or propeller.
(3) Item 17. Self-explanatory.
(4) Item 18. This item provides for the description and listing of the Class II products (parts) being exported. If the quantity and variety of parts are too voluminous to list in the space provided, check the first block and, on the line provided, specifically identify (and attach) a copy of the exporter's shipping document covering the parts concerned.
Otherwise, check the second block and list the parts in the space provided.
In either case, if more than one type of Class II product is involved, they are to be listed according to the Class I product to which they pertain.
Also list serial numbers or equivalent means of identifying each physical product.
(5) Item 19 - Exporter's Certification. This certification is to be dated and signed in ink by the exporter. The name of the person signing the application is to be typed or printed on the form. If the person signing the application is the exporter's representative, insert the representative's title in the space provided.
5. FAR 21.329 ISSUE OF EXPORT CERTIFICATES OF AIRWORTHINESS, FAA FORM 8130-4, FOR CLASS I PRODUCTS. Under the provisions of this Section, an aircraft of U.S. manufacture need not already possess a standard or restricted airworthiness certificate, but it is required to meet the requirements for such a certiticate, as applicable. On the other hand, an aircrait of foreign manufacture is required to possess a valid U.S.
standard airworthiness certificate issued under the provisions of FAR
21.183(c).
6. FAR 21.331 ISSUE OF AIRWORTHINESS APPROVAL TAGS, FAA FORM 8130-3, FOR CLASS II PRODUCTS. Among other things, Class II products are required to be identified by means of serial numbers or equivalent. This requirement is to provide for positive identification of each product covered by the export airworthiness approval similar to that provided for Class I products. This should be of benefit both to the exporter and the FAA since otherwise when complaints are received from foreign countries, there would often be no way to determine whether the parts in question are actually those covered by an export airworthiness approval or if they have ever been issued such an approval.
7. FAR 21.335 RESPONSIBILITIES OF EXPORTERS.
a. Regarding paragraph (e) of FAR 21.335, when title to a U.S.-registered and certificated aircraft passes to the foreign buyer, the certificate Par 4 5
cancellation request, the certification regarding removal of the U.S.
markings, and the registration and airworthiness certificated being returned for cancellation should be transmitted to the following address by the exporter:
Department of Transportation matrat tor-250 Federal Aviation Administration Airman & Aircraft Registry, AAC-250 Aircraft Records Building, P.O. Box 25082 oklahoma City, Oklahoma
b. The act of showing that products meet the pertinent requirements, as required by Sections 21.329, 21.331, and 21.333 carries with it the responsibility for making the products available to the FAA representative for whatever inspection he considers necessary and appropriate in each case.
Normally, his inspection will consist of a review of the application (when applicable), a review of all related documents, and an inspection of the finished product or products to determine their eligibility, proper identification and configuration, condition for safe operation, and compliance with special requirements (if any) of the importing country.
A product not meeting the requirements of FAR 21.329, 21.331, and 21.333 may be exported, if the importing's cuntry civil air authority indicates its acceptance in writing. The requirements that are not met should be listed or referenced on FAA Form 8130-4 in the exceptions block, and referenced on FAA Form 8130-3, as applicable.
8. FAR 21.339 SPECIAL EXPORT AIRWORTHINESS APPROVAL FOR AIRCRAFT. In the case of aircraft exported under the provisions of FAR 21.339, when title to the aircraft has passed to a foreign purchaser, the exporter should comply with FAR 21.335(e) (reference paragraph 7a of this AC).
9. RESPONSIBILITY FOR ISSUANCE AND REVISION.
The issuance, revision, or cancellation of material in this AC is the responsibility of the FAA Aircraft Manufacturing Division, AWS-200. All changes will be accomplished as required to carry out the responsibility of the agency. Interested personnel are invited to submit recommendations for revisions or new material, as applicable, to keep this document updated.
b. Material for inclusion should be forwarded to FAA Aircraft Manufacturing Division, AWS-200.
c. Information submitten should clearly identify the substance of the material. Air authorities of foreign countries should submit new material or revisions to special requirements in the wording and format in English to meet the intent of their requirements.
6 Par 7
AC 21-2E 5/18/81 Appendix 1 APPENDIX - 1 SAMPLE FORMS
UNITED STATES OF AMERICA DEPARTMENT OF TRAHSPORTATION - • FEDERAL AVIATION ADNUMISTRATION Ho.0470019 Application for Export Certificate of Airworthiness EXPORT CERTIFICATE NO. E30016 JASTRICTION. -This application is lu be aubmined to an authorized FAA repre calive (our capy) when ibe prodors (a) to be exporred is la . 'presend for inspection. Liar Part 1 for Class I producia and Pan Il for Ciano II. For complete aircrafi esecate irents | chrough Il an applicable For engines and propellere, cair inese SA and 6. Par II is for FAA one oaly PART I IN INADE FOR AN EXPORT CERTIFICATE OF AIRBORTMINEESTO COVER THE PRODUCTIŞIDESCRIBEDBELOR, EMICH
1) -11 WHEELY OVE HANE AND ADDRESS OF EXFORTEN NAME ADADORESS OF FOREIER MASER 4. COUNTAY OF DESTMATIOA ABC Airplane Corporation Jokyo Hews Service Cleveland, Ohio Tokyo, Japan Japan
DESCRIFTION OF PRODUCTISI TYPE MAKE AND MODEL PATION IDENTIFNO SERIAL NUMBERS SEC. NO OPERATING TIME (Haurs) artist & AIRCRAFT ABC Airplane Corp.
Model C-5 ¡JA-VOX 2468 6A17 51 AIRECO 18976 I-80
• ENGINES Model 10-470-2 18978 Senhart Hub Nos. P-99
r. PROPELLERS Hub model: SC-B2XK-2 21375 Blade model: X8498C-2 21412 SATISFACTORY FLIGHT TEST ON ART22 28 g1926
BITHALL ARPLICABLE FEDENAL AVIATION MEGULATIONS, AIRRORTMINESS DIRECTIVES, AND LE SPECIAL REGUIRELENTS OF THE IMPER FINE COUNTRY BEEN COMPLIED WITH?
• MAI PEOPRA PARVEMTATIVE TRI ITHENT BEEN APPLIED TO PRODUCTE SUSCERTIBLE TO RAPID CORNOSION EMEN DEINO DrES Dmo Not applicable to Fly-away delivery The el temptaty attary to pite has ole hitled fot the drivery, ice.
Documents required by FAR 21.327, , as applicable, re provided herewith.
I EXPORTER'S CERTIPICATION condition los dele esperation escapi ex April 29, 2926 (Dern! Signs of hoplicans or Auster John D. Do ried Regrasantative) Sales Hanage: Thie FAA Foom $130. | 10-00:
Figure 1 Completed Application for Export Certificate of Airworthiness, FAA Form 8130-1 For Use with Class I Products 1
Appendix 1
PART II 13 MAME AND ADDRESS OF EXPONTER 12 APPLICATION IS MADE FOR APPROVAL OF AERONAUTICAL PARTS FOR EXPORT AS INDRA AD BELOW COUNTRY OF DESTINATION 14 NAME ANDADORESS OF FOREIGN PURCHASER ABC Airplane Crp. Aviation Supplies Ltd.
Cleveland, Ohio London, England England
• PARTSARE ELGIBLE FOR INSTALLATIONO ALL ALIPLADE NOdEL, CES mate and mandal Ciese | Produci! ¡FAA SpaS No.) 6A17
1) THE PARTS ARE (chuchomat. • MEaLY OvERHAULeD ID THE PANTE ARE DESCRIBED (Chuck and):
• Br Home, Part Numbar, and Quantiry or , do atroched loo • Parting Shaul Mo I balan by Mama, Pars Mum and Oramlily Name BA 2 570285 6 29 Part Number Aileron P/N A-456-4 Elevator Assy.
I certity that the loregoing et described hertin are airworthy and confore to FAA approved design : 4. Doi Harch 25. 1976 John D. Doe Sales Manager (Signature of Applicon or Autherised Represemorive) ¡Title!
PART III-APPROVAL (FOR FAA USE ONLY)
20. 17 15 CONSIDERED TH. THE PRODUCTIS; DESCRIBED IN 15 (ARE) AIRWORTHY AND COMFORMIS
TO PERTI (Signores ¡Humber! IDote.
Check Ons • SMIR • DELEGATION OPTION MFR • FAN INSPECTOR
11. _ _ APPROVAL TAGS, FORMS FAABI30-3, WERE ISSUED FOR THE PARTS DESCRIBED IN PART IJ.
22 EXPORT FILE SPOT-CHECKEC BY:
(FAR Supervising Insperior) (D. O. No.) (Date:
Figure 2 Completed Application for Export Certificate of Airworthiness, FAA Form 8130-1, (Reverse Side) for Use with Class 11 Products
Appendix 1 The Bladeed States of America Department of Transportation Fedcral Aviation Administration No. E30016 Contagina, D.C.
Expor: Certificate of Airborchiness Eat tes shal th pendurl identified baler and ever particularly desvited in fpecificatin (s) of the Federo/Soriadon Stateinistratin, Nschoco 6817; TE6, and P-234 has hear soomined and as of the dals of this contificals, is considered ainerathy in accordance with a compressin and delailed amoothiness ande of the United hates Fevermond, and is in compliance with these special seguirements of the importing country filed with the Uniled Hales Ferovemenl, sacep?
as nded below. This contipeate in a way attests to complance with any agrement oo contrart baten the sander and purchases, non does it sealiluls authority to operale an aircraft Tour: Airplane Engine Model:
AIRECO 10-170-2 Manufariume: ABC AIrplane COrP. Serial Nos. 18976 and 18978 Total time 50 bre. and 51 bre.
Alodel: 6-5 Propeller Model:
taviah A 2468 Senhart SC-82XK-7 hub with X84980-2 blades Hub Serial Noa, 21375 and 21412 Total time 50 hrs. and 51 hrs.
Weed Demonap D finghins: A temporary auxiliary fuel oysten has been installed in this aircraft in conformity with ABC Drawing AF-1 to facilitate Its delivery flight.
This certifloate is valid when the temporary installation is removed.
Desmith * Total time on airoraft: 51 hours; 10 hours since annual insp.
J. A. Smith, PAA Delegation Option Authorization Liganion of Anitaried Angersemiarro Marob 1, 1976 ABC Airplane Corp. (PC75) Chate Desires Offer as Desi peer Number 110751 9604-815-067 Figure 3 Export Certificate of Airworthiness, FAA Form 8130-4, Issued for Class I Products 3
5/18/81 AC 21-2E Appendix 1
UNITED STATES OF AMERICA
DEPARTMENT OF TRANSPOF CATION
FEDERAL AVIATION ADMINISTRATION
AIRWORTHINESS APPROVAL TAG
DESCRIPTION OF PARTS
IS NEW - NEWLY OVERHAULED
APPROVAL FASIS IC No. 6A17
OUANTITY, NAME AND PART NUMBER 2 Ailerons P/N A-456-4 S/No. 113 S/No. 114 2 Elevator Assy's A-789-2A S/No. 285 S/No. 290 ELL. IPO FOR INSTALLATION ON:
Airplane Model C-5
SEE SHIPPER'S INVOICE NUMBER ABC 948690
INSPECTED AND APPROVED
AGENCY NAME AND NUMBER ABC Airplane Corp.
DATE PAA NUMBER July 28, 1976 DOA PC 75 Figure 4 Airworthiness Approval Tag, PAA Form 1830-3, Issued for Class II 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. Revisions of the appendix will be made from time to time following receipt of official notification and documentation from the foreign governments concerned.
2. The following governments have filed their requirements with the Federal Aviation Administration.
Appendix 2 Page No.
Argentina, Republic of ... 3 Australia, Commonwealth of 4 Belgium, Kingdom of... 12 Bolivia, Republic of 16 Botswana, Republic of Brazil, Federative Republic of .
Canada, Dominion or France, Republic of Germany, Federal Republic of Hong Kong India, Republic of Indonesia, Republic of Ireland, Republic of Israel, State of Italy, Republic of Japan Korea, Republic of Lebanon, Republic of Malaysia, West Morocco, Government of Netherlands, Kingdom of Netherlands Antilles New Zealand, Dominion of Pakistan, Republic of Panama, Republic of Philippines, Republic of Portugal, Republic of
Rhodesia96
Saudi Arabia, Kingdom of. 98 Singapore 100 South Africa, Republic of 104 Sweden, Kingdom of .. 105 Switzerland, Confederation of. 112 Syrian Arab Republic 14 Taiwan .. 115 Tunisia, Republic of . 120
United Kingdom121
Yugoslavia, Federal People's Republic of . 140 Zambia, Republic of 144 pages 1 (and 2)
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 2l 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 Aiworthiness, 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 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 Engiish 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 (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.
2. Class II and Class III products shall be exported in accordance with the provisions prescribed in Part 2l of the United States Federal Aviation Regulations.
Appendix 2
COMMONWEALTH OF AUSTRALIA - SPECIAL REQUIREMENTS SECTION 1 - INTRODUCTION. A new bilateral 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 2l 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), furnished by the applicant, which contains entrie:
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 satistying 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 regional offices of the Federal Aviation Administration or at the office of the Transport Attache, Embassy of Australia, 1601 Massachusetts Avenue, N.W., Washington, D.C. 20036, or may be obtained by mail from the Secretary, Department of Transport, Box 18390, G.P.O. Melbourne, 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 and requires 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.
determined, and, where necessary, Australian special conditions have been notified, Australia will 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 602220 FAA Airworthiness Directives and Australian 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;
otılity;
Acrobatic;
Agricultural;
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) Transport 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."
(c) A.N.O. Section 101.8, Imported Piston Aeroplanes Above 5700 kg Designed to CAR and FAR.
(d) A.N.O. Section 101.10, 'Imported Rotorcraft Designed to CAR and FAR in the Transport Category.
(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."
(1v) Developmental Category. A.N.O. Section 101.3-, "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
(1) 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 Engines, auxiliary power units and propeller need not incorporate modifications or manufacturers' service documents made mandatory by Australian Airworthiness Directives 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 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 2l 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 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, intormation 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.
e. 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).