Appendix 2 ENCLOSURE 4
CIVIL AVIATION AUTHORITY
AIRWORTHINESS DIVISION BRABAZON HOUSE REDHILL SURREY RHI ISQ Telephoo: Redhin 65966 Teles 27100 Telegrams & Cables Mordair Redbill
APPLICATION FOR APPROVAL OF, OR MODIFICATION TO, AN ACCESSORY Name and Address of Applicant Name and Address of Manufactures If different from Applicant State abether Initial Full Tille of Accessory Approval or Modification Jocatity or Reference No. - Drawing or Specification No. Declaration of Desigo and Performance No.
Brief Description of Accessory, or of Modification.
INITLAL APPROVAL - State the condition of the Mainteansce, Overhaul and Repair Manuals.
MODIFICATION - Describe briefy any complementary amendment necessury to the Maintenance, Overbaul and Repair Manual: ouberwise state "Not Affected".
FOR CAA USE ONLY Cheque P.O. value f I/we bereby apply for approval of the above Accessory/Modification Cash in accordance with British Civil Airworthiness. Requirements, Cbspier A3-3 or A3-4 (as applicable).
Detacbed by .
Folio _ Date _ Internal Reference No. Sigped Date 139
AC 21-2E Appendix 2 5/18/81
FEDERAL PEOPLE'S REPUBLIC
YUGOSLAVIA - SPECIAL REQUIREMENTS In order to be eligible for certification in SFR Yugoslavia, transport type aircraft must be covered by following documents:
1. DOCUMENTS CONCERNING THE TYPE CERTIFICATE
a. A copy of the type certificate for the aircraft type.
b. A copy of the type certificate data sheet.
c. Summary of flight test reports for aircraft type certification, with expanded flight test list.
d. Three-view drawings of the major assemblies, installations, and primary structure.
e. Summary of stress analysis, for principal structural elements, their design loads, dimensions, materials, stresses, and safety margins, or summary of static test reports, performed for aircrait type certification.
f. Summary of vibration test reports.
g. List of reports and notes prepared for aircraft type certification.
h. A copy of information or instruction necessary for the assembly and rigging of the aircraft, if the aircraft will be exported unassembled.
i. A list of the time limits for first overhaul /TO/ for: engines, propellers, their relevant rotables including the aircraft ones.
j. The aircraft emergency equipment installation bulletin.
k. The passengers' attention and emergency placards bulletin.
1. Manufacturer's maintenance requirements.
m. A list of the necessary special tools and equipment essential to the inspection and maintenance of the aircraft, its engines, propellers, and principal accessories and other equipment items. This should include a list of permissible tolerance limits, maintenance inspection notes due to aircratt structural parts, and complete information on lubricating, fuel and hydraulic systems.
Appendix 2
n. One copy each of maintenance and service, overhaul, and repair manuals applying to the aircraft, engines, propellers, or to the equipment installed on the aircraft.
A separate parts catalog tor the aircrait, the engines, the propellers, and the principal accessories and other equipment items.
p. One copy of the following manuals:
(1) Flight manual which should contain: limitations, normal operations, emergency operations, and performance.
(2) Flight crew operating manual.
(3) Manual wiring diagram.
(4) Weight and balance manual.
g. Complete manufacturer's service bulletins.
I. A statement by an authorized representative of the manufacturer that the Yugoslav D.G.C.A., Brankova 25, Beograd, Yugoslavia, will systematically be furnished with all pertinent information, notification of modifications, service bulletins, etc., and notification of any change in such documents, to quarantee the maintenance of an acceptable airworthiness level for the aircraft.
(1) One copy of above documents must be forwarded to Yugoslav D.G.C.A., in advance or with imported aircraft, if no Yugoslav standard time of aircraft importing, or if Yugoslav standard airworthiness certificate has been issued but abovementioned documents have not been forwarded to Yugoslav D.G.C.A.
2. DOCUMENTS REQUIRED FOR EACH INDIVIDUAL NEW AIRCRAFT
a. An Export Certificate of Airworthiness.
b. Manufacturer's production control and test report for individual aircraft.
c. Manufacturer's production flight test report for the aircraft, including a flight test checklist utilized when testing the aircraft (two copies).
d. A weight and balance report with record containing a complete inventory of all equipment and instruments (two copies).
e. Manufacturer's production test report for the engines and propellers (two copies).
Appendix 2
f. A list of modifications that have been incorporated during production for the aircraft, the engines, and the propellers (two copies).
g. A list of historical records for the aircraft, the engines, and the propellers (summary operating hours).
h. Last engines run-up report, not older than 10 days.
Delivery declaration with aircraft specification containing: data on engines, propellers, their rotables - including the aircraft ones and the equipment installed; flight data recorder, emergency equipment, radio and electrical equipment with following characteristics; model, capacity, frequency, operating instructions, etc. Manufacturer's serial number and summary operating hours must be given for each listed item (two copies).
j. One copy of the documents listed under 1(h) through (g). These documents, which are intended for the purchaser, are required only for first aircraft imported for certain purchaser. For each additional aircraft same type, imported for the same purchaser, all these documents are not required, except flight manual and flight' crew operating manual. For these aircraft, the number of each required manual should be determined through the contract between aircraft exporter and purchaser:
k. Blanket of authorization for ferrying aircraft to make export delivery, issued from airworthiness authority exporter's country, if aircraft will be exported to Yugoslavia via flyaway. The use of aircraft communication transceivers should be also permitted by this document, or by separate ones.
1. Yugoslav certificate of registration and Yugoslav certificate of airworthiness, if aircraft is intended for export to Yugoslavia via flyaway with Yugoslav registration and nationality markings. Mentioned Yugoslav certificates will be issued after basic airworthiness inspection, as defined in Yugoslav law. Yugoslav registration and nationality markings shall be properly displayed on the aircraft before inspection.
3. DOCUMENT REQUIRED IN ADDITION TO THOSE SPECIFIED UNDER ITEM 2, FOR
EACH INDIVIDUAL - USED AIRCRAFT
a. Airworthiness directives status performed on aircraft, list and documents (two copies).
b. A summary of aircraft, engines and propellers modifications, performed during past use.
c. A report of past maintenance and overhaul inspection with a summary of technical data, date and the operating hours since last inspection of each type (two copies).
Appendix 2
d. A report of non-routine work performed on aircraft after failures and damages, list and documents.
e. Aircraft logbook with notified: summary operating hours, number of landings, aircraft historical data concerning technical incidents and accidents, major repairs, periodical inspections and overhuals.
f. Engine and propeller logbooks with notations: summary operating hours, number of cycles and historical data listed above under item 1.e.
g. Acceptance flight test report (two copies).
h. Limitations for next overhaul, or part of overhaul (in-flight hours and in calendar periods) for aircraft, engines and propellers (two copies).
i. Documentation on aircraft system reliability and statistical data on failures, and aircraft technical daily report book, for the past three months of regular use.
j. Previous owner's maintenance manual with current maintenance schedule (two copies).
k. Maintenance and overhaul work cards.
1. Aircraft and powerplants functional test procedures, if not conducted in work cards or in maintenance manual.
m. Maintenance agreement, if aircraft is leased.
n. A copy of radio license.
o. A certificate of deregistration.
NOTE:
Documents listed above, under Items 3.j., k. and 1., required only for first aircraft type imported for each purchaser;
Documents specified under Items 2 and 3 must be furnished with imported aircraft. They are intended for the purpose of both, D.G.C.A. and purchaser; and All documents specified under these requirements must be issued or approved by airworthiness authority of the manufacturer's country.
Appendix 2
REPUBLIC OF ZAMBIA - SPECIAL REQUIREMENIS
1. GENERAL
a. Any aircraft to be eligible for the issue of a Certificate of Registration issued by the Goverment of the Republic of Zambia must qualify for certification in the United States of America in the standard or restricted category, and an Export Certificate of Airworthiness, FAA Form 8130-4, should have been issued in accordance with Part 21 of the
b. Class 2 and Class 3 products should be accompanied by documentation which confirms that the item is in accordance with the relevant section of Part 2l of the United States Federal Aviation Regulations. An Airworthiness Approval Tag, FAA Form 8130-3, is acceptable.
c. If the aircraft is to be entered on the Zambia Register of Civil Aircrait prior to departure from che united states or America, the importer will make application to the Zambian Department of Civil Aviation for the necessary Certificate of Registration, Permit to Fly and Radio Station License, which must be carried during the delivery flight.
d. Inquiries should be addressed to the Director of Civil Aviation, P.O. Box RW 137, Ridgeway, Lusaka, Zambia, marked for the attention of the Chief Aircraft Inspector.
2. AIRCRAFT FIRST OF THE TYPE TO BE REGISTERED IN THE REPUBLIC OF ZAMBIA The following documents and data are required:
a. Complete set of maintenance and overhaul manuals, and parts catalogs, for:
(1) Airplane
(2) Engine(s)
(3) Propeller(s)
(4) Any equipment not already installed in an aircraft on the Zambian Register of Civil Aircraft.
b. Full set of Service Bulletins, Letters, and Modification Leaflets issued by the manufacturers in respect of the airframe, engine(s), propeller(s), and installed equipment.
c. A copy of the Type Certificate, if not already held by the Department.
Appendix 2
d. Three copies of the flight manual for the aircraft.
e. One copy of the production flight test report issued by the manufacturer.
EACH AIRCRAFT FOR WHICH A ZAMBIAN CERTIFICATE OF AIRWOKIHINESS IS TO
BE REQUESTED The following documentation is required:
a. A statement, signed by an official representative of the manufacturers, showing that all mandatory modifications and special inspections have been complied with.
b. The Export Certificate of Airworthiness, FAA Form 8130-4.
c. Two copies of the Approved Flight Manual.
d. Two copies of the Weight & Balance report showing the weights and arms of the main components, and a list of installed equipment.
Appendix 3 APPENDIX 3 FAA Regional Offices Responsible for Civil Aviation Matters in Foreign Countries Country or Area FAA Regional Office Address
a. Canada Federal Aviation Administration Federal Building John F. Kennedy International Airport Jamaica, New York 11430
b. Caribbean Area, Federal Aviation Administration South America, P.O. Box 20636 Central America, Atlanta, Georgia 30320 (excluding Mexico) (Location: 3400 Norman Berry Road Panama, and the East Point, GA 30344) Canal Zone
c. Mexico Federal Aviation Administration P.O. Box 1689 Fort Worth, Texas 76101 (Location: 4400 Blue Mound Rd.)
Fort Worth, Texas 76101
d. Area East of East Pakistan and India, including all free nations south and east of China
e. Europe, Africa, Middle East west of Burma, Iceland, Greenland, and Bermuda Federal Aviation Administration P.O. Box 50109 Honolulu, Hawaii 96850 (Location: 300 Ala Moana Boulevard, Room 7321, Honolulu, Hawaii 96850) Federal Aviation Administration Rue de Loi, 15 B-1000 Brussels, Belgium 1
Appendix 4 APPENDIX 4
COMPOSITE CHARI
BILATERAL AIRWORTHINESS AGREEMENTS REVISED 4/6/81 AGREEMENTS COMPOSITE CHART AND AIRWORTHINESS SCOPE OF BILATERAL AIRCRAFT REPLACEMENT/MODIFICATION PARTS FOR FMPORTED AIRCRAFT ENGINES REPLACEMENT/MODIFICATIO PARTS FOR EXPORTED AIRCRAFT ENGINES PROPELLERS REPLACEMENT/MODIFICATION PARTS FOR EXPORTED PROPELLERS APPLIANCES REPLACEMENT /MODIFICATION PARTS FOR EXPORTED APPLICANCES COMPONENTS MATER TAL PARS SUBASSEMBLIES TREATIES AND OTHER INTERNATIONAL ACT SERIES AGREEMENT Page 1 of 3 DATE
AUSTRALIA (Ref. Note 4 and 7) • Ж _ *2 8126 1975 AUSTRIA × 4219 1959 BELGIUM (Ref. Note 4) 1x2 7292 7675 1973 BRAZIL (Ref. Note 4) *2/×2P2 8384 1976 7091 1971 CANADA * *8 *8 131 1938 CZECHOSLOVAKIA * 6987 1970 DENMARK 3158 1954 EINLAND *5 7795 1974 FRANCE * . (Bef, Note 4) *2×2×2 7728 1973 GERMANY _(Ref. Note 4) * 7965 1974 ISRAEL 7926 1974 6530 1968 ITALY * 7895 1973 (Ref. Note 4) JAPAN (Bef. Note 4) * * * *2172 *2 8934 1977 NETHERLANDS (Ref. Note 4) * * / ×з 7869 1974
NEW ZEALAND *з *З *2 X2 1878 3769 1957 NORWAY * 9141 1978 POLAND *6 *6 *6 X272 X2 8407 9723 1980 1976 ROMANIA ×1 ×1 8440 1976 SOUTH AFRICA * 3200 1955 3906 1978 SPAIN SWEDEN * * *2*2 7611 1973 (Ref. Note 4) SWITZERLAND × *2 S365 1893 UNITED KINGDOH Ref• Note 4) ׄj 7537 1972 1
Appendix 4 APPENDIX 4 - Notes
1. Gliders only.
2. The U. S. has bilateral airworthiness agreements with these cuntries which provides for the reciprocal acceptance of certificates of conformity for components (i.e., materials, parts, and subassemblies). This provision only applies when:
a. An agreement exists between the manufacturers in the importing and exporting countries; and
b. The component is of such complexity that a determination of conformity cannot readily be made by the manufacturer in the importing country; and
c. The airworthiness authorities of the importing country have notified the airworthiness authorities of the exporting country of the applicable design, test, and quality control requirements.
3. The U.S./New Zealand Bilateral is limited as follows:
a. Export from New Zealand to the U.S. is limited to:
(1) Fixed-wing aircraft constructed in New Zealand not exceeding a maximum weight of 12,500 lbs.
(2) Spare (replacement) parts for fixed-wing aircraft constructed in New Zealand which do not exceed a maximum weight of 12,500 pounds.
(3) Appliances for use on civil aircraft.
(4) Spare (replacement) parts for those appliances used on civil aircraft.
(5) Components for fixed-wing aircraft not exceeding 12,500 pounds.
b. Export from U.S. to New Zealand is limited to:
(1) U.S. constructed civil aircraft, in all categories.
(2) U.S. constructed aircraft, engines and propellers.
(3) Spare (replacement) parts for such aircraft, aircraft engines and propellers.
(4) Appliances for use on civil aircraft.
(5) Spare (replacement) parts for those appliances for use on civil aircraft.
Appendix 4
(6) Components for use on civil aircraft.
4. These bilaterals contain a third-party country provision which provides for import/export certification of products/parts thereof by the Civil Air Authorities of a untry other than the country of manufacture.
In these instances, the exporting country must certify that the products/ parts thereof conform to the design covered by the certificate or approval of the importing country (which would be other than country of manufacture) and that the products/parts thereof are in proper state of airworthiness.
5. To be separately determined to be included in the agreement by mutual consent of the competent authorities of the United States and Finland.
(None have been determined to be included as of September 2, 1980).
6. U.S./Polish Bilateral Agreement is limited as follows:
a. Products which may be exported from Poland to U.S. (or U.S.
possession) :
(1) Civil gliders and replacement/modification parts therefor designed and produced in Poland.
(2) Piston engines of 1,000 h.p. or less with associated propellers and accessories and replacement/modification parts therefor produced in Poland.
(3) Small fixed-wing aircraft of 12,500 lbs. or less and replacement/ modification parts therefor.*
(4) Helicopters with associated accessories and replacement/ modification parts therefor.*
(5) Turbine engines and replacement/modification parts therefor.*
(6) Components and appliances for U.S. manufactured products of the types specified in subparagraphs (1), (2), (3), (4), and (5) above.
*Note: Refer to U.S./Poland Bilateral Airworthiness Agreement for applicable design constraints.
Appendix 4
b. Products which may be exported from U.S. to Poland:
(1) U.S. designed and produced aircraft, engines, propellers, components and appliances and replacement/modification parts therefor; and
(2) U.S. produced components and appliances for Polish manufactured products and replacement and spare parts therefor.
The U.S./Australian Bilateral contains a two-party country provision which provides for reciprocal certification whereby Australia can issue an export certificate for a U.S.-manufactured product located in that country which is to be exported to the U.S. Conversely, the U.S. can issue an export certificate for an Australian-manufactured product which is located in the U.S. and which is to be exported to Australia. Such certifications will state that the product conforms to the importing countries type design and is in a proper state of airworthiness.
8. The U.S./Canadian Bilateral (as amended February 18, 1971) does not contain the standard components provision (Rei. Note 2). It does, however, contain a provision which provides for the reciprocal acceptance of materials and parts. Although, the term "subassemblies" is not specifically addressed, Civil Air Authorities of Canada and the U.S. construe the word "parts" as to include subassemblies.