AC 21-2K

Advisory Circular

Subject: EXPORT AIRWORTHINESS

APPROVAL PROCEDURES Date: 9/30/2003 Initiated by: AIR-200 AC No. 21-2K Change:

____________________________________________________________

1. PURPOSE. This advisory circular (AC) contains information and guidance on procedures for exporting aeronautical products and incorporates by reference related special requirements submitted to the Federal Aviation Administration (FAA) by other governments. Additionally, this AC provides general information, guidance and application instructions for issuance of export certificate of airworthiness for Class I products and export airworthiness approvals for Class II and Class III products.

This AC provides an acceptable means, but not the only means, for compliance with Title 14 Code of Federal Regulations (14 CFR) part 21, Certification Procedures for Products and Parts, subpart L, Export Airworthiness Approvals.

2. CANCELLATION. AC 21-2J, Export Airworthiness Approval Procedures, dated June 27, 2000, is canceled.

3. EXPLANATION OF MAJOR CHANGES.

a. Paragraph 11(a)(1) NOTE was added and states that compliance with importing country’s special requirements, e.g., installation of emergency equipment required by the importing country, does not require a document to approve or allow the installation.

b. Paragraph 13(c)(1) is revised to reflect the policy contained in Federal Register Notice Volume 68, Number 48, pages 11759-11760 [03-5326], with respect to work performed on products and/or parts that have left the production approval holder’s quality system.

c. Appendix 1 has been revised to include the current revision of FAA Form 8130-1.

d. Appendix 2, Special Requirements of Importing Countries and Jurisdictions, was removed and relocated to an FAA Internet site upon publication of revision J of this Advisory Circular. The current location of this site is http://www.faa.gov/aircraft/air_cert/international/export_aw_proc/sp_req_import/ Relocating appendix 2 to the Internet provides immediate access to current import requirements.

e. Appendix 3, FAA Aircraft Certification Office and International Flight Standards Field Office Contacts For Other Countries, has been revised to reflect current addresses and phone numbers.

4. FORMAT. This AC has been reformatted to contain only the export airworthiness procedures. The Special Requirements of Importing Countries and Jurisdictions described in paragraph 3b of this AC are provided on the Internet in their original format as submitted by each country or jurisdiction. The FAA

has recently begun a process to review and suggest standardization to special requirements as they are submitted. Format inconsistencies and nonconformance with the United States Government Printing Office Style Manual and FAA directives may be observed. For any assistance with interpretations or to request, a printed copy of the Special Requirements of Importing Countries and Jurisdictions contact the following:

Federal Aviation Administration Production and Airworthiness Division, AIR-200 800 Independence Avenue, SW Washington, DC 20591 Phone Number: 1-202-267-8361 FAX Number: 1-202-267-5580

5. RELATED READING MATERIAL. The latest edition of FAA Order 8130.2, Airworthiness Certification of Aircraft and Related Products, and FAA Order 8130.21, Procedures for Completion and Use of Authorized Release Certificate, FAA Form 8130-3, Airworthiness Approval Tag, should be used when interpreting this AC.

6. DISCUSSION.

a. Persons desiring additional information or guidance on obtaining an export certificate of airworthiness or an export airworthiness approval may contact the nearest FAA Flight Standards District Office (FSDO), Flight Standards Service International Field Office, Aircraft Certification Office, Manufacturing Inspection Office, Manufacturing Inspection District/Satellite Office, or Certificate Management Office/Unit. Persons in other countries or jurisdictions who wish to import aeronautical products from the United States should contact the appropriate FAA Flight Standards Service International Field Office listed in appendix 3.

b. The special requirements of the importing country or jurisdiction referred to in part 21, subpart L, include special conditions and/or additional requirements specified by the Civil Aviation Authority (CAA) of the importing country or jurisdiction. Special conditions and/or additional requirements may be found at http://www.faa.gov/aircraft/air_cert/international/export_aw_proc/sp_req_import/ . When importing countries or jurisdictions impose special conditions or additional requirements, the FAA must certify the exporter’s compliance except as noted below:

(1) Special requirements are administrative requirements that must be satisfied as a condition of shipment at the time of export. For example, they may involve the requirement for a United States Export Certificate of Airworthiness, copies of logbooks, flight manuals, etc. When a product does not meet the special requirements of an importing country or jurisdiction, the exporter must obtain a written statement from the CAA of the importing country or jurisdiction indicating the CAA will accept the deviation. This statement must accompany FAA Form 8130-1, Application for Export Certificate of Airworthiness.

(2) Additional requirements are those deemed necessary by the importing country or jurisdiction, in addition to the exporting country’s or jurisdiction’s certification or approval basis, to provide a level of safety and environmental quality equivalent to the importing country’s or jurisdiction’s certification basis. When these requirements cannot or will not be satisfied, the exporter must obtain a written statement from the CAA of the importing country or jurisdiction indicating acceptance of the deviation.

This statement must accompany the Form 8130-1. Exporters are encouraged to obtain information on additional requirements from the importing country’s or jurisdiction’s CAA. Additional requirements by the importing country or jurisdiction should be documented on Form 8130-1, block 10, when they constitute a difference to the type design.

(3) Special conditions are airworthiness standards issued to cover unique and/or unusual design features that are not adequately covered by a country’s or jurisdiction’s applicable laws, regulations, or requirements. These special conditions should be included in the Type Certificate Data Sheets (TCDS) or Supplemental Type Certificates, as applicable. Special conditions for U.S. type certifications are issued in accordance with § 21.16. Exporters are encouraged to obtain information on special conditions from the importing country’s or jurisdiction’s CAA.

NOTE: The Special Requirements of Importing Countries and Jurisdictions as described in paragraph 3a of this AC refer to various importing countries’ and jurisdictions’ internal technical documents. These documents are not normally available in FAA offices. In such cases, it will be necessary for interested person(s) to obtain those documents directly from the importing country’s or jurisdiction’s embassy.

c. FAA Form 8130-4, Export Certificate of Airworthiness, certifies compliance with applicable airworthiness requirements but DOES NOT CONSTITUTE AUTHORITY TO OPERATE AN AIRCRAFT. Information and guidance concerning appropriate airworthiness certificates, flight permits, and special flight authorizations are contained in AC 20-65, U.S. Airworthiness Certificates and Authorizations for Operation of Domestic and Foreign Aircraft.

7. TITLE 14 CFR § 21.323, ELIGIBILITY. Person(s) engaged in exporting civil aircraft and related products, including aircraft owners and their representatives, are eligible for an export airworthiness approval for a Class I or Class II product provided all pertinent requirements are met. A Class III product export airworthiness approval may only be issued by manufacturers (or their authorized suppliers) who have in their employ a designated representative of the Administrator authorized to issue that specific approval. The manufacturer must be a production approval holder (PAH) for that specific Class III product, (i.e., hold a Production Certificate (PC), an Approved Production Inspection System, a Parts Manufacturer Approval, or Technical Standard Order (TSO) authorization). Class III products, including standard parts as defined in § 21.321(b)(3), not produced under an FAA production approval are not eligible for issuance of Form 8130-3 for export.

8. TITLE 14 CFR § 21.325, EXPORT AIRWORTHINESS APPROVALS. In general, an export airworthiness approval means that at the time and date signed, the product covered was found airworthy by the FAA and to be in compliance with the applicable CAA requirements.

a. Export airworthiness approvals for Class I products are documented by issuance of Form 8130-4, Export Certificate of Airworthiness. Procedures for completion and use of Form 8130-4 may be found in Order 8130.2. The FAA or authorized designee will complete Form 8130-4 upon receipt of Form 8130-1 completed by the applicant. Procedures for completion of Form 8130-1 are found in paragraph 9 of this AC.

b. Export airworthiness approvals for Class II or Class III products are documented by issuance of an Authorized Release Certificate, FAA Form 8130-3, Airworthiness Approval Tag. Procedures for completion and use of Form 8130-3 may be found in Order 8130.21.

9. TITLE 14 CFR § 21.327, APPLICATION. A separate application must be made for each aircraft, aircraft engine, or propeller EXCEPT that one application may be made for more than one engine or propeller, if all are of the same type and model and are exported to the same purchaser and country or jurisdiction. One application may be submitted for more than one type of Class II product when the products are separated and identified in the application as to the type and model of the related Class I product and they are exported to the same purchaser and country or jurisdiction. Class II products manufactured by a PC holder and Class III products produced by any PAH do not require a written application. In these cases, an oral application or request may be made to the FAA as specified in § 21.327. A sample of Form 8130-1 is shown in appendix 1. Part I of the application should be completed for Class I products and Part II should be completed for Class II products.

NOTE: A Class I product is defined as a complete aircraft, aircraft engine, or propeller. A Class II product is a major component of an aircraft, aircraft engine, or propeller, the failure of which would jeopardize the safety of a Class I product;

or any part, material, or appliance, approved and manufactured under the TSO system in the “C” series. A Class III product is any part or component that is not a Class I or Class II product and includes standard parts (Reference § 21.321).

a. Guidance for completion of Part I of Form 8130-1 (for Class I products).

(1) Export Certificate No. Leave blank.

(2) Items 1 and 2. Self-explanatory.

(3) Item 3. Self-explanatory, except for aircraft owned by a U.S. company being leased to a company in another country or jurisdiction. Under these circumstances, strike-thru the word “purchaser” and insert “lessee.”

(4) Item 4. Self-explanatory.

(5) Item 5. Description of product(s). Self-explanatory, except as follows:

(a) For an aircraft not under U.S. registry, in the Identification No. Block insert the nationality and registration marks supplied by the country or jurisdiction of registry or intended registry that are displayed on the aircraft. For U.S.-registered aircraft, insert the identification marks as assigned under 14 CFR part 47, Aircraft Registration. Any questions concerning the marking requirements of the importing country or jurisdiction should be resolved between the exporter/importer and the CAA of that country or jurisdiction.

(b) Under FAA Spec No., insert the pertinent specification number or TCDS number, whichever is applicable.

(c) For used aircraft, insert the operating hours since the annual type inspection required Page 4

by § 21.329(c) and total time in service. Except as provided in § 21.329(g), because used aircraft engines and propellers (which are not being exported as part of a certificated aircraft) must have been newly overhauled in accordance with § 21.329(e) to be eligible for export, the operating time since overhaul would reflect only run-in time as required to complete the overhaul process.

(d) For aircraft, the blocks for engine (5B) and propeller (5C) should be completed to reflect the applicable information.

(6) Items 6 and 7. These items are self-explanatory; however, if the Item 6 NO box is checked, explain the deviations in Item 10. If the Item 7 NO box is checked, attach the written confirmation of deviation acceptance from the CAA of the importing country or jurisdiction.

(7) Item 8. This item provides a means of establishing a date the ownership of the Class I product is expected to pass to the purchaser. For leased aircraft, enter N/A in this block and explain in Item 10.

(8) Item 9. This item provides a means of documenting the status of preservation and damage treatment, as required by the type certificate holder’s approved procedures or other procedures acceptable to the Administrator.

(9) Item 10. This space is used to explain or clarify the information required under Items 6 and

7. This space may also be used by the exporter to convey any other information necessary to facilitate issuance of the export airworthiness approval. Documentation that must be submitted with the application should be listed and additional sheets may be attached and cross-referenced as necessary.

After review by the FAA representative, documents required to be furnished to the importing country or jurisdiction under § 21.335 will be returned to the applicant.

(10) Item 11. This certification is to be dated and signed in a permanent-type ink by the exporter, with the name of the person signing the application typed or printed below. If the person signing the application is an authorized representative of the exporter, insert that person’s title in the space provided.

A notarized statement authorizing the individual to represent the exporter in this transaction should be attached to the application and referenced in Item 10.

b. Guidance for completion of Part II of Form 8130-1 (for Class II products).

(1) Items 12 through 14. Self-explanatory.

(2) Item 15. The instructions contained in Order 8130.21 for entering eligibility information should be used for item 15.

NOTE: No entry is required in the “FAA Spec No.” box.

(3) Item 16. Self-explanatory.

(4) Item 17. This space provides for a description and listing of the Class II products being exported. If the quantity and variety of the parts are too numerous to list in the space provided, check the second 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 first block and list the parts in Page 5

the space provided. In either case, if more than one type of Class II products is involved, they are to be listed according to the Class I product to which they pertain. List serial numbers or equivalent means of identifying each physical product.

(5) Item 18. This item is self-explanatory; however, if the NO box is checked, explain the noncompliance in Item 10, and attach the written confirmation of deviation acceptance from the CAA of the importing country or jurisdiction.

(6) Item 19. This item provides a means of documenting the status of preservation and damage treatment as required by the manufacturer’s approved procedures or other procedures acceptable to the Administrator. It is recommended that all products be appropriately treated for corrosion and damage prevention.

(7) Item 20. This certification is to be dated and signed in permanent-type ink by the exporter with the name of the person signing the application typed or printed below. If the person signing the application is the exporter’s authorized representative, insert that person’s title in the space provided. If the person signing the application is the exporter’s authorized representative, a notarized statement authorizing that individual to represent the exporter in this transaction should be attached to the application and referenced in Item 10.

10. TITLE 14 CFR § 21.329, ISSUANCE OF FAA FORM 8130-4, EXPORT CERTIFICATE OF AIRWORTHINESS, FOR CLASS I PRODUCTS. Under this section, an aircraft of U.S.

manufacture need not possess a standard or restricted airworthiness certificate; but it must meet the airworthiness requirements for such a certificate. Conversely, non-U.S. manufactured aircraft are required to be U.S.- registered and possess a valid U.S. Standard Airworthiness Certificate.

11. TITLE 14 CFR § 21.335, RESPONSIBILITIES OF EXPORTERS.

a. Show that a product meets the requirements of §§ 21.329, 21.331, and 21.333.

(1) Ensure the product meets its type design, is in a condition for safe operation, and meets the importing country’s or jurisdiction’s CAA requirements.

NOTE: Importing country’s special requirements are not considered exceptions to 14 CFR that require written acceptance as defined in paragraph (2).

(2) Make the product available to the FAA representative for any inspection considered necessary.

NOTE: A product not meeting the requirements of §§ 21.329, 21.331, or 21.333 may be exported if the importing country’s or jurisdiction’s CAA indicates acceptance in writing. Requirements that are not met shall be listed or referenced on Form 8130-4 in the Exceptions block, or referenced in the Remarks block on Form 8130-3, as applicable.

b. When title to a U.S.-registered and certificated aircraft passes to a purchaser in another country or jurisdiction, § 21.335 requires the exporter to:

(1) Request cancellation of the United States registration and airworthiness certificate, give the date of title transfer, and the name and address of the new owner.

(2) Return the registration certificate, AC Form 8050-3, Certificate of Registration;

FAA Form 8100-2, Standard Airworthiness Certificate; or FAA Form 8130-7, Special Airworthiness Certificate; as applicable, to the FAA Aircraft Registry.

(3) Submit a statement certifying the U.S. registration marks have been removed from the aircraft in compliance with 14 CFR part 45, Identification and Registration Marking, § 45.33.

NOTE: The above information should be submitted to the following address:

Federal Aviation Administration Aircraft Registration Branch, AFS-750 P.O. Box 25504 Oklahoma City, OK 73125

c. If an importing country or jurisdiction requires design approval of a product prior to its export, then any application for type certification should be forwarded to the responsible ACO for transmittal to the appropriate aviation authority.

12. TITLE 14 CFR § 21.339, SPECIAL EXPORT AIRWORTHINESS APPROVAL FOR AIRCRAFT. When an aircraft is exported under the provision of § 21.339, and title of the aircraft has passed to a purchaser from another country or jurisdiction, the exporter is to comply with § 21.335(e) (reference paragraphs 11a and 11b of this AC).

13. DETERMINATION OF NEW, NEWLY OVERHAULED, AND USED PRODUCTS.

a. Title 14 CFR does not define NEW or USED products. However, there are requirements that are pertinent to both new and used products in 14 CFR and in the special requirements of certain countries or jurisdictions.

b. Aircraft engines, propellers, or Class II or III products that are removed for any reason and remain under the control of the PAH, and are then exported without any previous TIME IN SERVICE are considered NEW, since any time in service makes them used products.

c. An aircraft may be considered NEW as long as the manufacturer or dealer retains its ownership and there is no intervening private owner, lease, or time-sharing arrangements, and the aircraft has not been used in any pilot training school and/or air taxi operation. An aircraft is still considered NEW regardless of the amount of operating time logged by the manufacturer or dealer when:

(1) Any work performed on the aircraft while under the control of the PAH’s quality system is accomplished in accordance with that system.

(2) The application for the Export Certificate of Airworthiness reflects the serial number of the aircraft and the total number of operating hours 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 an inspection has been accomplished.

(3) The Export Certificate of Airworthiness reflects the information required by paragraph 13(c)(2) of this AC.

(4) The aircraft has not been used in any revenue flights.

d. Under § 21.321, the words NEWLY OVERHAULED (when used to describe a product) mean the product has not been operated or placed into service, except for functional testing, since having been overhauled, inspected, and approved for return to service in accordance with the applicable regulations.

Class II products eligible for export approval may only be new or newly overhauled and conform to the requirements of 14 CFR part 43, Maintenance, Preventive Maintenance, Rebuilding and Alteration, § 43.2(a); be in a condition for safe operation; be identified with at least the manufacturer’s name, part number, model designation (when applicable), and serial number(s) or equivalent (when applicable), and meet the special or additional requirements of the importing country or jurisdiction. Serial number or equivalent includes but is not limited to batch numbers, lot numbers, work order numbers, or any sequence of letters or combination of numbers and letters established by the manufacturer or repair station to maintain traceability of their products.

e. Class II products not meeting these requirements may be exported if the CAA of the importing country or jurisdiction provides written confirmation stating acceptance under § 21.327(e)(4). Class III products are eligible for export when the applicant shows the product conforms to the approved design data applicable to the Class I or Class II product of which it is a part; the product is in a condition for safe operation; and the product meets the special or additional requirements of the importing country or jurisdiction. A Class III product that is not NEW may be exported only when the CAA of the importing country or jurisdiction provides written confirmation stating acceptance of the product under §§ 21.333(b) and 21.327(e)(4).

NOTE: Although newly overhauled products technically are used products, the terms new and newly overhauled are prescribed in part 21, subpart L, in order to distinguish between products eligible for Form 8130-3. Any products that are not NEW or NEWLY OVERHAULED are considered USED. Flight Standards Information Bulletin for Airworthiness, Bulletin Number FSAW 94-04, provides additional guidance when exporting used avionics. Contact your local FSDO for current information.

f. If for any reason the previously listed information results in controversy or is contrary to existing special or additional requirements, the issue should be settled between the exporter, importer, and the CAA of the importing country or jurisdiction.

9/30/2003 AC21-2K

14. RESPONSIBILITY FOR ISSUANCE AND REVISION.

a. The issuance, revision, or cancellation of material in this AC is the responsibility of AIR-200.

Future changes will be issued as required to carry out the responsibility of the FAA. Interested persons are invited to submit recommendations for revisions or new material to keep this AC current. Proposed material for inclusion in this AC should be forwarded to:

Federal Aviation Administration Production and Airworthiness Division, AIR-200 800 Independence Avenue, SW.

Washington, DC 20591 Phone Number 1-202-267-8361 FAX Number 1-202-267-5580

b. Revisions to the Special Requirements of Importing Countries and Jurisdictions are updated on a continuing basis, as received from the country. Revisions are posted on an FAA Internet site:

http://www.airweb.faa.gov/AC. Changes should be forwarded to the address identified in paragraph 14(a).

c. The CAAs of other countries or jurisdictions should submit new material or revisions to special requirements in English and are requested to use a format suitable for publication to meet the intent of their requirements. Special requirements received in other than English will not be accepted or published.

/s/

Frank P. Paskiewicz Manager, Production and Airworthiness Division, AIR-200

Page 9 (and 10)

9/30/2003 AC21-2K

APPENDIX 1. SAMPLE FORMS Figure 1. Completed FAA Form 8130-1, Application for Export Certificate of Airworthiness (Front Side) OMB NO. 2120-0018

Application for Export Certificate of Airworthiness

Export Certificate No.

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 1 products and Part II for Class II. For complete aircraft execute items 1 through 11, as applicable.

For engines and propellers, omit item 5A. Part III is for FAA use only.

Part I — Application for Export Certificate of Airworthiness (Complete items 1-11)

1. Application is made for an export certificate of airworthiness to cover the product(s) described below which is (are):

NEW USED (Aircraft) NEWLY OVERHAULED

2. Name and address of exporter ABC Airplane Corporation 121 Lake Avenue Cleveland, OH 44111

3. Name and address of foreign purchaser Tokyo News Service Tokyo, Japan

4. Country of destination Japan

5. Description of product(s) Type

(a) Make and Model

(b) Identification No.

Serial Nos.

(c) FAA T.C.

or Spec. No.

(d) Operating time (Hours)

(e) Since Overhaul

Total A. AIRCRAFT ABC Airplane Corp Model C-5 JA-VOX 2468 6A17 51 B. ENGINES (L/H) AIRCO Model IO-470-2 (R/H) 18976

18978

E-88

51 C. PROPELLERS Senhart (L/H) Hub Model: SC-82XK-2 Blade Model: X8497C-2 (R/H) 21375

21412

P-99

6. Does the product comply with all applicable Federal Aviation Regulations, Airworthiness Directives, and other FAA requirements?

YES NO (Explain in “Remarks”)

7. Have applicable special requirements of the importing country been complied with?

YES NO (Explain in “Remarks”)

8. Date title passed or is expected to pass to foreign purchaser: 01/09/2003

9. For overseas shipment, preservation and packaging methods used to protect product(s) against corrosion and damage (List Spec. No. or Title):

Not applicable to Fly-away delivery.

Effective duration of above methods:

10. Remarks The aircraft described above complies with all FAA requirements for export, except that a temporary auxiliary fuel system has been installed IAW ABC drawing, Rev.1. Upon the removal of the auxiliary fuel system, the aircraft will be returned to its approved configuration.

Documents required by 14 CFR section 21.327 are included with this application.

Total time since annual inspection IAW 14 CFR part 43: Aircraft 2 hours Engine(s) 2 hours (L/H) S/N 18976, 2 hours (R/H) S/N 18978.

Propeller(s) 2 hours (L/H) S/H 21375, 2 hours (R/H) S/N 21412.

11. EXPORTER’S CERTIFICATION — The undersigned certifies that the above statements are true and that the product(s) described herein is (are) airworthy and in condition for safe operation except as may be noted under item 10 “Remarks” above.

Signature of applicant or authorized representative

J.R.Smith Title

Sales Manager Date

12/18/2003 Agency Display of Estimated Burden: T he FAA estimates that the average burden f or this report form is 12 minutes per response . Y ou may submit any comments concerning the accuracy of this bur den estimate or an y suggestions for reducing the burden to the Office of Mana gement and Budget. Y ou ma y al so send comments to the Federal Aviation Administration, Production and Airworthiness Certification Division, AIR-200, 800 Independence Avenue, SW, Washington, DC 20591, Attention: OMB number 2120-0018.

FAA Form 8130-1 (11-95) Supersedes Previous Edition NSN: 0052-00-024-9005 Page 1

AC21-2K 9/30/2003 APPENDIX 1. SAMPLE FORMS (CONTINUED) Figure 2. Completed FAA Form 8130-1, Application for Export Certificate of Airworthiness (Reverse Side)

Part II — Application for Approval of Aeronautical Parts (Complete items 12-20)

12. Name and address of exporter ABC Airplane Corporation 121 Lake Avenue Cleveland, OH 44111

13. Name and address of foreign purchaser Aviation Supplies Ltd.

London, England

14. Country of destination

United Kingdom

15. Parts are eligible for installation on Make and model Class I product ABC Airplane Model C5 FAA Spec. No. or T.C

16. The parts are (Check One) NEW NEWLY OVERHAULED

17. The parts are described (Check One) Below by name, part number and quantity On the attached invoice or packing sheet, by name, part number and quantity Invoice/packing sheet No.

Name

(a) Part number

(b) Quantity

(c)

Aileron Assembly

Elevator Assembly

A-456-4 (S/N 113 and 114)

A-789-2A (S/N 285 and 290)

2 each

2 each

18. Have applicable special requirements of the importing country been complies with? YES NO (Explain in item 10 “Remarks”)

19. Preservation and packaging methods used to protect parts against corrosion and damage (List Spec. No. or Title):

ABC Airplane Corporation Specification #44 Preservation and Corrosion Effective duration of above methods: 12/16/2002

20. Exporter’s Certification — I certify that the foregoing statements are true and that the parts described herein are airworthy, conform to FAA approved design data, are in condition for safe operation except as may be noted in item 10 “Remarks”.

Signature of applicant or authorized representative

J.R. Smith Title

Sales Manager Date

12/16/2003 Part III — Approval (FOR FAA USE ONLY)

21. It is considered that the product(s) described in Part I or Part II is (are) airworthy and conform(s) to pertinent requirements except as noted in Item 10. (Check one) Part I Part II Signature

Number

Date

(Check one) DMIR DAR DOA ODAR FAA Inspector

22. Give quantity of approval tags, FAA Form 8130-3, issued for the parts described in Part II. Quantity

23. EXPORT FILE SPOT-CHECKED BY:

FAA Supervising Inspector

D.O. No.

Date

FAA Form 8130-1 (11-95) Supersedes Previous Edition *U.S. Government Printing Office: 1996 - 405-552/45303 NSN: 0052-00-024-9005