AC 21-2B CHG 1 Page 5 11/13/70
(8) Item Il 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.
b. PART II - (For Class II products)
(1) Items 12 through 15, are self explanatory.
Item 16 Parts are Eligible 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) 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 torm. 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 certificate, as applicable. On the other hand, an aircraft of foreign manufacture is required to possess a valid U.S.
STANDARD airworthiness certificate issued under the provisions of FAR 21.183 (c).
Page 6 AC 21-2B CHG 1 11/13/70
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 because, in the past, when complaints have been received from foreign countries, there was no way to determine, in some cases, whether the parts in question were actually those covered by an export airworthiness approval or had ever been issued such an approval.
7. FAR 21.335 Responsibilities of Exporters.
Regarding paragraph (e) of FAR 21.335, when title to a U.S. registered and certificated aircraft passes to the foreign buyer, the certificate cancellation request, the certification regarding removal of the U.S. markings, and the registration and airworthiness certificates being returned for cancellation, should be transmitted to the following address by the exporter:
Federal Aviation Administration Aircraft Registration Branch, AC-250 Aircraft Records Building, P.O. Box 1082 oklahoma City, Oklahoma 73101
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.
8. PAR L1.339 Special Export Airworthiness Approval for Aircrait. in che case or aircrait exported under the provisions of FAR 21.339, when title to the aircraft has passed to a foreign purchaser, the exporter should:
a. Ensure that all countries except the country in which the aircraft is sold are deleted by use of ink or typewriter from the original Export C of A which was carried in the aircraft, * Comply with FAR 21.335(e) (reference paragraph 7a of this Advisory Circular)
AC 21-2B CHG 1 Appendix 1 11/13/70 Page 1 APPENDIX 1 - SAMPLE FORMS UNITED STATES OF AMERICA Form approved.
DEPARTMENT OF TRANSPORTATION - FEDERAL AVIATION ADMINISTRATION Budget Burgou No. 04-R0059 EXPORT CERTIFICATE NO.
Application for Export Certificate of Airworthiness INSTRUCTIONS. -This application is to be submitted to an authorized FAA representative (one copy) when the product(a) to be exported is (are) presented for inspection. Use Part I for Class 1 produces and Part Il for Class II. For complete aircraft execute items I through 11 as applicable. For engines and propellers, omit items 5A and 6. Part II1 is for FAA use only.
PART J
1. APPLICATION IS MADE FOR AN EXPORT CERTIFICATE OF AIRWORTHINESS TO COVER THE PRODUCTISI DESCRIBED BELOW, WHICH 15 (ARE):
• USED (Aireraft) • NEMLY OVERMAULED
2. NAME AND ADORESS OF EXPORTER 3. NAME ANDADDRESS OF FOREIGN PURCHASER TO COUNTRY OF DESTINATION AFC Airplane Corporation Tokyo News Service Cleveland, Ohio Tokyo, Japan Japan
15. DESCRIPTION OF PRODUCT(S) TYPE MAKE AND MODEL CATION NO. IDENTIFI SERIAL NUMBERS SPEC. NO. FAA EVENATUL OPERATING TIME (Hows) TOTAL & AIRCRAFT ABC Airplane Corp.
Model C-5 JA -VOX 2468 6A17 7.5 AIRECO 18976 E-88-8 10.5
6. ENGINES Model I0-470-2 18978 9.2 Senhart Hub No. 's
c. PROPELLERS Hub model: SC-82XK-Z 21375 P-99-9 7.5 Blade model: X8498C-2 21412 7.5
8. THE AIRCRAFT WAS GIVEN A SATISFACTORY FLIGHT TEST ON ARE 11.280 1969
7. DOES THE PROOUCT COMPL Y WITH ALL APPLICABLE FEDERAL AVIATION REGULATIONS, AIRMORTHINESS DIRECTIVES, AND OTHER FAA REQUIREMENTS? DYES [X) NO (Explain in '*Remarke"") HAVE APPLICABLE SPECIAL REQUIREMENTS OF THE IMPORTING COUNTRY BEEN COMPLIED WITH?
• NO (Explain in "Remarks"") S. SAI PEOPER PREVENTATIVE TREATMENT BEEN APPLIED TO PRODUCTS SUSCEPTIBLE TO RAPID CORROSION WHEN BEING Q YES Not applicable. Fly-away delivery
10.
The aircraft described above complies with all applicable FAA requirements, except that a temporary auxiliary fuel system has been installed for the delivery flight.
Documents required by FAR 21.327 as applicable, are provided herewith.
11. EXPORTER'S CERTIFICATION The undersigned certilies that the above statements are true and that the product(s) desctibed herein is (are i airworthy and in condition for safe operation except as may be noted under item 10 "Remarks " abouc.
John D Doe April 29, 1969 John D. Doe Sales Manager (Dote) (SIgnature of Applicant or Authorized Representative) (Title) FAA Form 8130-1 (6-69) Completed Application for Export Certificate of Airworthiness, FAA Form 8130-1 For Use with Class I Products
Appendix 1 AC 21-2B Page 2 10/2/69
PART II
12. APPLICATION 15 MADE FOR APPROVAL OF AERONAUTICAL PARTS FOR EXPORT AS INDICATED BELOWI
13. NAME AND ADDRESS OF EXPORTER 14. NAME AND ADDRESS OF FOREION PURCHASER 19. COUNTRY OF DESTINATION ABC Airplane Corp. Aviation Supplies Ltd, England Cleveland, Ohio London, England
1. PARTS ARE ELIGIBLE FOR INSTALLATION ON ABC ALIplane COrP: Model C-5 6A17 (Make and Model Class I Product) (FAA Spac. No.)
17. THE PARTS ARE (check onel • NEW - NEWLY OVERHAULED
8. THE PARTS ARE DESCRIBED (check one):
• By Name, Part Number, and Quantity on the attached Inveice or Packing Sheat No..
i Balam by Name, Part Number, and Quentlty.
Name Part Number Quent y Aileron P/N A-456-4 Elevator Assy. P/N A-789-2A
19. EXPORTER'S CERTIFICATION I certify that the foregoing statements are true and that the parts deacribed heteln are airworthy and conform to FAA apptored deaian data.
John d. Woe sarch 25, 190 10h0 1 Doe Sales Manager Date Signature of Applicant or Authorized Representalve
PART III-APPROVAL (FOR FAA USE ONLY) 20, IT 15 CONSIDERED THAT THE PRODUCT (S) DESCRIBED IN - - IS (ARE) AIRWORTHY AND CONFORMS) ¡Por ¡ or !!)
TO PERTINENT REQUIREMENTS EXCEPT AS NOTED IN ITEM 10.
(Signature) (Number) (Dote) Check One: O DHIR • DELEGATION OPTION MFR • FAA INSPECTOR
- APPROVAL TAOS, FORMS FAA -186, WERE ISSUED FOR THE PARTS DESCRIBED IN PART II.
(Quantity)
22. EXPORT FILE SPOT-CHECKED BY:
іла бора vising Inspector Completed Application for Export Certificate of Airworthiness, FAA Form 8130-1, (Reverse Side) for Use with Class II Products
AC 21-2B CHG 1 Appendix 2 11/13/70 Page 1 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 to this 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:
Page No.
a. Argentina, Republic of
b. Australia, Commonwealth of...
Brazil, Republic of the United States of.
d. Canada.
e. France, Republic of.
f. India.
Indonesia, Republic of
h. Ireland.
i. Israel, State of.
Italy, Republic of. 34 K. Japan. 3
1. Korea. 38
m. Malaysia, West..
n. Netherlands, Kingdom of
o. Netherlands Antilles P• New Zealand. -4 9 • Pakistan.
Philippines, Republic of.
S • Rhodesia.
t. Singapore, Republic of..
South Africa, Republic of..
V . Sweden..
w. Switzerland.
x. United Kingdom..
* У • Zambia.
Appendix 2 AC 21-2B Page 2 10/2/69
ARGENTINA, REPUBLIC OF - SPECIAL REQUIREMENTS
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 Airworthiness, FAA Form 8130-4.
b. Record of aircraft and engines, including logbooks.
c. Copy of the Federal Aviation Administration Approved Flight Manual, if applicable.
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.
AC 21-2B CHG 1 Appendix 11/13/70 Page 3
AUSTRALIA, COMMONWEALTH OF--SPECIAL REQUIREMENTS Aircrait, to be eligible for certification in Australia, in addition to the requirements prescribed in Part 21 of the United States Federal Aviation Regulations, must be demonstrated to comply with the requirements of the appropriate Section of Part 101 of the Air Navigation Orders issued by the Director General of Civil Aviation in Australia. The following guidance is offered:
A United States Export Certificate of Airworthiness for export to Australia without exceptions will be considered as evidence that an aircraft complies with the requirements for the issue of an Australian Certificate of Airworthiness provided the Export Certificate has been issued for no longer than 90 days or 50 operating hours.
The appropriate Section of the Australian Air Navigation Orders Part 101 will be that appropriate to the category of certification required and the class of aircraft concerned. The Section against which the aircraft has been demonstrated to comply should be endorsed on the Export Certificate of Airworthiness.
Aircraft may be issued with Australian certificates of airworthiness in one or more of the following categories;
(1) Transport;
(2) Normal;
(3) Utility;
(4) Acrobatic;
(5) Agricultural;
(6) Developmental; and
(7) 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:
(1) Transport Category.
(a) A.N.O. Section 101.4, Imported Aeroplanes Not Above 12,500 1b. in the Transport Category."
(b) A.N.O. Section 101.6, "Imported Turbine Aeroplanes Above 12,500 1b. Designed to CAR and FAR.
A.N.O. Section 101.8, Imported Piston Aeroplanes Above 12,500 1b. Designed to CAR and FAR."
410-605 0 - 70 - 3
Appendix 2 AC 21-2B CHG 1 Page 4 11/13/70
(d) A.N.O. Section 101.10, "Imported Rotorcraft Designed to CAR and FAR in the Transport Category.
(2) 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."
Agricultural Category. A.N.O. Section 101.17, "Imported Aeroplanes Not Above 12,500 1b. in the Agricultural Category."
(4) Developmental Category. A.N.O. Section 101.31, "Developmental Aircraft."
(5) 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.
e. 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.
The procedures to be followed for the issue of an Australian certificate of airworthiness are specified in the Australian Air Navigation Orders Section 100,2.
8 • Copies of Air Navigation Orders may be perused at the various regional offices of the Federal Aviation Admínistration or at the office of the Civil Air Attache, Embassy of Australia, 1601 Massachusetts Avenue N. W., Washington, D. C. 20036, or may be obtained by mail from The Director General, Department of Civil Aviation, Box 18390, G.P.O., Melbourne, Vic. 3001, Australia.
2. An Export Certificate of Airworthiness, for export to Australia, in accordance with the requirements prescribed in Part 21 of the Federal Aviation Regulations 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 Civil Aviation that the
AC 21-2B CHG 1 Appendix 2 11/13/70 Page 5 aircraft complies with the appropriate Section of Part 101 of Air Navigation Orders and the Director General of Civil Aviation has advised the responsible region of the FAA in writing of its acceptance of the aircraft. The following guidance is offered:
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.
Compliance with the requirements of Air Navigation Orders may be demonstrated to an authorized officer or officers of the Australian Department of Civil Aviation. These officers will normally visit the United States to assess compliance only in the case of transport category aircraft of maximum take-off weight greater than 12,500 1b.
3. In some circumstances it may be impossible or undesirable to show thet an aircraft complies with all thé 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. In these circumstances an Export Certificate of Airworthiness for export to Australia may be issued in accordance with the requirements prescribed in Part 21 of the Federal Aviation Regulations when it has been demonstrated to the responsible region of the FAA that the aircraft complies with such 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:
a. Circumstances in which it may not be possible to demonstrate compliance with the requirements before export include the following:
(1) Those where interpretations or assessments have to be given by the Department of Civil Aviation and where an authorized officer 16 not available in the U.S. to perform these functions; and
(2) Those where demonstrations of radio communication/navigation and other electronic equipment need to be given using Australian ground aids.
b. There are some circumstances where compliance can only be demonstrated or modification can only be performed by the manufacturer in which cases the applicant should note the possibility of difficulties developing later, should he proceed without that compliance.
Appendix 2 AC 21-2B CHG 1 Page 6 11/13/70 C. In the circumstances concerned, the U.S. Export Certificate of Airworthiness, if it has been issued for no longer than 90 days or 50 operating hours, will be validated, if so requested, to permit the aircraft to be flown to Australia. An Australian Certificate of Airworthiness will be issued for the aircraft only when it has been demonstrated to the Department of Civil Aviation that the previously unfulfilled requirements have been complied with or agreement has been reached with the Australian applicant as to a program of compliance. *
4. In some cases it may not be possible, before export of an aircraft to Australia, to provide all the documents and data required by the relevant * Section of Part 101 of Air Navigation Orders. In these cases an Export Certificate of Airworthiness for export to Australia may be issued in accordance with the requirements prescribed in Part 2l of the Federal Aviation Regulations when as many of the documents and data as possible are supplied to the responsible region of the FAA and documents and data not supplied are clearly defined. 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 supply of documents and data has been assessed. The following guidance is offered:
a. The documents and data required, by the Air Navigation Orders, to be supplied to the Director General of Civil Aviation, include data on each aircraft as well as on the aircraft type. These latter documents are only required when the aircraft is the first of its type to be imported into Australia. Subsequent aircraft of the same type and model are only required to be supported by documents appropriate to the individual aircraft.
b. The vendor or exporter should obtain advice from the purchaser (on the basis of information furnished to the purchaser by the Australian Department of Civil Aviation), or from a representative of the Department of Civil Aviation, as to whether an aircraft is the first of its type or model to be imported into Australia.
* Practically all of the documents and data concerned can only be supplied by the manufacturer and therefore, the applicant should note the possibility of difficulties developing later should he proceed without that material.
d. In the circumstances concerned, the United States Export Certificate of Airworthiness may be validated, if so requested, to permit the aircraft to be flown to Australia. An Australian Certificate of Airworthiness will be issued for the aircraft only when the remaining documents and data have been supplied to the Department of Civil Aviation or agreement has been reached with the Australian applicant as to a program for supply of the material.
AC 21-2B CHG 1 Appendix 2 11/13/70 Page 7
5. Aircraft engines 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, must be new or newly overhauled as defined in Part 21 of the United States FARs and must have a log book. In addition, such engines and propellers are required to conform with modifications and specified manufacturers' service documents which are made mandatory by Air Navigation Orders.
The following guidance is offered:
a. A United States Export Certificate of Airworthiness for export to Australia will be considered as evidence that an aircraft engine or propeller conforms with the type design and is either new or newly overhauled.
b. Engines and propellers need not incorporate modifications or manufacturers' service documents made mandatory by the Director-General prior to export 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 product would be of help to the Australian user. An appropriate statement either in a log book or separately issued by the person or organization issuing the United States Export Certificate of Airworthiness will be considered as evidence of the modification status.
6 - Class II and Class III products which are exported to Australia as spares, 1.e., not as parts of a particular aircraft, to be eligible for use on Australian aircraft must conform with the type design and must be new or newly overhauled as defined in Part 21 of the United States FARs. In addition, such products are required to conform with modifications and specified manufacturers' service documents which are made mandatory by Air Navigation Orders. The following guidance is offered:
a. An Airworthiness Approval Tag, FAA Form 8130-3, issued in accordance with the requirements of Part 2l of the United States FARS will be considered as evidence that the products conform with the type design and are either new or newly overhauled.
b. Products need not incorporate modification or manufacturers' service documents made mandatory by the Director General prior to export 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 product would be of help to the Australian user. A statement by the person issuing the airworthiness approval tag will be considered as evidence of the modification status of the products.
Appendix 2 AC 21-2B Page 8 10/2/69
BRAZIL, REPUBLIC OF THE UNITED STATES OF - SPECIAL REQUIREMENTS
1. To be eligible for registration and airworthiness certification by the Government of Brazil, Class I, II, and III products will be processed in accordance with the instructions contained in paragraphs a., b., and
c., below.
a. The manufacturer or supplier must hold or obtain one or more of the following FAA approvals, unless otherwise approved by a Brazilian Governmental agency, e.g., Brazilian Air Force, etc.:
(1) A current valid FAA production certificate for the product involved, as outlined in Federal Aviation Regulations Part 21.
(2) An FAA Approved Production Inspection System (FAA-APIS), as provided in Federal Aviation Regulations Part 21, Subpart F.
(3) An FAA replacement and modification parts manufacturer approval FAA-PMA as provided in Federal Aviation Regulations Part 21.
subpart K. in this case, parts, containers, and invoices wil] bear evidence of the manufacturer's name, address, the part number registered trademark, when described in FAA approval letter, and the symbol "FAA-IMA."
(4) Technical Standard Order (ISO) letter of acceptance, or authorization issued by the FAA per Federal Aviation Regulatione Part 37.
b. Reconditioned, used, or surplus parts, must be accompanied by a certification statement signed by an FAA certified repair station holding a currently valid certificate, or by a certified aircrait und powerp-ant mechanic, as provided for under FAR Parts 145 and 65, respectively. The return to service maintenance records required by Federal Aviation Regulations 43 shall accompany the parts.
NOTE: The provisions of the above paragraphs are not applicable to standard parts (such as nuts and bolts) conforming to established industry or Government specifications, e.g., Standard Aircraft Equipment (SAE), and Military Specifications (MIL Spec.).
c. In all instances, suppliers must certify on the face of their invoice that the product involved was manufactured under one or more of the above procedures; 1.e., FAA PC No. _; FAA-APIS letter dated FAA-PMA letter dated _: ISO NO. _; SAE NO._ _; MIL Spec.
_; other Government or Industry Specifications