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 Respons1b1lities 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 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 repone i Hey for mith the producer vat lab to the hi te 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.
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:
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.
*
b. 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 DEPARTMENT OF TRANSPORTATION - FEDERAL AVIATION ADNINISTRATION UNITED STATES OF AMERICA Fuda Braved No. 04.00059 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(s) to be exported is (are) presented for inspection. Use Part I for Class I products and Part Il for Class II. For complete aircraft execute items 1 through I1 as applicable. For engines and propellers, omit items 5A and 6. Part Ill is for FAA use only.
PART I
• APPLICATION IS MADE FOR AN EXPORT CERTIFICATE OF AIRWORTHINESS TO COVER THE PRODUCTISIDESCRIBED BELOW, WHICH IS (ARE): I NEW • UsED (Alraat) • NEWLY OvERHAULED NAME AND ADORESS OF EXPORTER NAME AND ADDRESS OF FOREIGN PURCHASER 4. COUNTRY OF DESTINATION ABC Airplane Corporation Tokyo Newa Service Cleveland, Ohio Tokyo, Japan Japan
5. DESCRIPTION OF PRODUCTS) DENTIFI OPERATING TIME (Hours) TYPE MAKE AND MODEL CATION NO SERIAL NUMBERS SPEC. NO. TOTAL & AIRCRAFT ABC Airplane Corp.
Model C-5 JA-VOX 2468 6A17 7.5 AIRECO 18976 E-88-8 & ENGINES Model 10-470-2 18978 Senhart Hub No. 's
c. PROPELLERS Hub model: SC-82XK-2 21375 P-99-9 7.5 Blade model: X8498C-2 21412 7,5
8. THE AIRCRAFT WAS GIVEN A SATISFACTORY FLIGHT TEST ON ADI 11. 20001962
DOES THE PRODUCT COMPL Y WITH ALL APPLICABLE FEDERAL AVIATION REGULATIONS, AIRMORTHINESS DIRECTIVES, AND OTHER FAA REQUIREMENTS? DYES [X] NO (Explain In "Remarks"")
HAVE APPLICABLE SPECIAL REQUIREMENTS OF THE IMPORTING COUNTRY BEEN COMPLIED WITHT E Yes • NO (Explain in "Remarke"")
9. HAS PROPER PREVENTATIVE TREATMENT BEEN APPLIED TO PRODUCTS SUSCEPTIBLE TO RAPID CORROSION WHEN BEING SHIPPED! O YES DNO Not applicable. Fiy-away delivery
10. REMARKS 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, are provided herewith.
11. EXPORTER'S CERTIFICATION condition for safe operation except as may be noted under item 10 "Remarks,' The sadernigned ceritica that the above statements are true and that the products) descibed herein is (are) nisworthy and in Apr11 29, 1969 John D. Doe Sales Manager (Dote) (Signature of Applicont or Authorised 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 L 10/2/69
PART II
2. APPLICATION IS MADE FOR APPROVAL OF AERONAUTICAL PARTS FOR EXPORT AS INDICATED DELOWI
9. HAME AND ADDRESS OF EXPORTER 14. NAME ANDADDRESS OF POREION PURCHASER 15. COUNTRY OF DESTINATION ABC Airplane Corp. Aviation Supplies Ltd, England Cleveland, Ohio London, England &. PARTS ARE ELIGIBLE FOR INSTALLATION ON ABO ALIPLanE COIP. MOdEL CES 6A17 Make and Hodel Close I Product) (FAA Spac No.)
17. THE PARTS ARE (chack onah & NEW O NEWLY OVERHAULED
•. THE PARTS ARE DESCRIBED (check ond)
• By Heme, Part Number, and Quantily on the attached Involce or Packing Sheat Ho.
(X) Balam by Heme, Part Humber, and Quantity.
Name Part Number Quantity 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 paa described herela are sirworthy and conforn to FAA approved design date.
John M. Woe March 25, 1969 John D Doe Sales Manager (Signature of Applicont or Authorlsed Representative) PART Ili-APPROVAL (FOR FAA USE ONLY)
20. IT IS CONSIDERED THAT THE PRODUCT (5) DESCRIBED IN ..._ IS (ARE) AIRWORTHY AND CONFORMS) TO PERTINENT REQUIREMENTS EXCEPT AS NOTED IN ITEM 10. (Pon i or lit (Signature) (Number) (Date) Check One • DELEGATION OPTION MFR. L FAA INSPECTOR
21. _ APPROVAL TAGS, FORMS FAA-T86, WERE ISSUED FOR THE PARTS DESCRIBED IN PART II.
(QuantIty)
22. EXPORT FILE SPOT-CHECKED BY:
(FAA Supervising Inspecter) 10.0 N61 Completed Application for Export Certificate of Airworthiness, FAA Form 8130-1, (Reverse Side) for Use with Class II Products
AC 21-2B Appendix 1 10/2/69 Page 3 Che niced States of Samerica Depertment of Cransportation Federal Aviation Administration No. 30016 Washington, Đ.C.
Export Certificate of Airborthiness This Attles that the product identified belu and more particularly described in Specification (s) ' of thr Fedoral SIviation IIdministration, Numbered 6A17; 786; and P-234 has been samined and as of the dote of this certificate, is considered airwasthy in accordance with a comporchensive and delailed aincorthiness code of the Uniled Flates Govornment, and is in compliance with those special requirements of the imporling sountry filed with the United tales Government, sacept as noled below. This corlificate in no way attests to compliance with any agreement's on contradds beluren the vendon and purchaser, nor does it conslitule authority to sporale an aivoraf?.
Produch: Airplane Engine Model:
Manufactures: ABC Airplane COIP. AIRECO I0-470-Z Serial No. 's 18976 and 18978 Model: 6-5 Propeller Model:
toriah Na: 2468 hub with X8498C-2 blades Senhart SC-82XK-2 New 6) Newty Preshauted D Hub Serial No.'s 21375 and 21412 Used Slincraß? D Country lo schich sported: Japan In conformity with ABC Drawing AF-l to facilitate its delivery flight. Exceplind: A temporary auxiliary fuel system has been installed in this aircraft This certificate is valid when the temporary installation is removed.
signature of Autharized Represeniati March Dải 1969 ABC Airplane Corp. (PC75) District Offar or Designer Number For complete aircraft, list applicable specifiration or Type Certificate Data Sheet numbers for the aircrafi, engine, and propelle Applicable specifications or Type Certificate Data Sheel, i nol allached to this export cerlificale, will have been fararded to the appropriale povertmental ofice of the importing country.
PAN Form #130-4 (7-69) Formerty Fom FAA 20 U.B. BOYERMMENT PRINTING OFPICK: 1948 0-718-967 Export Certificate of Airworthiness, FAA Form 8130-4, Issued for Class I Products
Appendix 1 AC 21- 2B Page 4 10/2/69 FAX FORM 8132J (501)
FORMERLY
FRA FORM DE
UNITED STATES OF AMERICA
DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
AIRWORTHINESS APPROVAL TAG
DESCRIPTION OF PARTS IX NEW • NEWLY OVERHAULED
APPROVAL BASIS TC No. 6A17
QUANTITY, NAME AND PART NUMBER 2 Ailerons P/N A-456-4 2 Elevator Assy's A-789-2A ELIGIBLE FOR INSTALLATION ON: (T. C. PRODUCT) ABC Airplane Model C-5
SEE SHIPPER'S INVOICE NUMBER ARC 948690
INSPECTED AND APPROVED
AGENCY NAME AND NUMBER ABC Airplane Corp.
Jane a smith PATEUly 28, 1969 FAA NUDA PC 75 Airworthiness Approval Tag, FAA Form 8130-3, Issued for Class II Products
AC 21-2B CHG 1 Appendix 11/13/70 Page 1 APPENDIX 2 - SPECIAL REQUIREMENTS OF FOREIGN COUNTRIES 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 2
b. Australia, Commonwealth of...
Brazil, Republic of the United States of
d. Canada.
e. France, Republic of..
India..
Indonesia, Republic of.
h. Ireland. , 28
i. Israel, State of..
Italy, Republic of.
к. Japan.
Korea..
Malaysia, West.
n. Netherlands, Kingdom of.
o. Netherlands Antilles.
New Zealand. ›-4 Pakistan.
Philippines, Republic of.
S • Rhodesia..
t. Singapore, Republic of.
u. South Africa, Republic of...
v. Sweden...
w. Switzerland..
United Kingdom..............
У • Zambia. 65
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 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 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 2l of the United States Federal Aviation Regulations.
AC 21-2B CHG 1 Appendix 2 11/13/70 Page 3
AUSTRALIA, COMMONWEALTH OF --SPECIAL REQUIREMENTS
1. Aircraft, 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.
b. The appropriate Section of the Australian Air Navigation Orders Part 10l 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.
c. 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.
d. 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.
(c) 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.i
(0) A Vego Section 101.24, imported Rotorcraft in the Normal
(3) Agricultural Category. A.N.O. Section 101.17, "Imported Aeroplanes Not Above 12,500 lb. 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.
Copies of Air Navigation Orders may be perused at the various regional offices of the Federal Aviation Administration 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.
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;
a. 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.
b. 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 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, 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 is 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 compllance.
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 21 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: * 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 Depart- пера вне ment of Civil Aviation, as to whether an eircraft is the first of its type or model to be imported into Australia.
* C. 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, i.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.