Appendix 2 ENCLOSURE 2 - STATEMENT OF CONFORMANCE
FIRM'S NAME AND ADDRESS I certify that:
Nomenclature of appliance. This must include identifying part number which will mean that this particular part number will always conform to the declared state at time of registration.
I certify that (1) the above-named appliance meets the requirements of:
either the requirements of FAR Part 37 T.S.0. • . ... • or, Specification No. ......, with the following exceptions (if any);
(2) The appliance has been accepted by the FAA as meeting the relevant airworthiness requirements of FAR. • • or
(3) The Additional Requirements of CAA letter dated. • • •, have been met and that*
(4) The appliance will be manufactured under the quality control system specified in FAR 21.143, and
(5) the CAA will continue to be advised of any modifications affecting the airworthiness of the appliance.
Signed. ... .......
For . ... ..... • (name of firm) * Not required at initial submission. Only required when the applicant has been notified of any Additional Requirements in accordance with Section 3, par. B(2).
Appendix 2 ENCLOSURE 3 Department of Transportation Federal Aviation Administration In Reply Refer to Airworthiness Division Civil Aviation Authority Brabazon House Redh111 Surrey RH1 1SQ
ENGLAND Dear Mr. Connery The Bennett Corporation has requested our assistance in obtaining United Kingdom import acceptance of their Altimeter Model #7, Series 725 under the terms of the agreement between the United States of America and the United Kingdom of Great Britain and Northern Ireland relating to the reciprocal acceptance of airworthiness certifications.
We would advise you that we have accepted The Bennett Corpoation certification that their Altimeter Model #7, Series 725 complies with the periormance standards of FAR 37, TSO 737b.
Products of this approved design will be manufactured under Federal Aviation Administration (FAA) quality control surveillance in accordance with our Technical Standard Order (TSO) authorizations granted on June 26, 1979, and, July 8, 1979. A copy of each TSO authorization is enclosed for your information. Articles manufactured under these TSO authorizations will be marked in accordance with FAR 37.7(d) and paragraph (b) of TSO 737b.
In addition, articles exported will be accompanied by an FAA airworthiness approval which will be 1ssued by a representative of the FAA in the form of an Airworthiness Approval Tag, FAA Form 8130-3 (formerly FAA Forn
186) in accordance with FAR 21.325(a)(2).
Copies of the technical data required and accepted by the FAA in granting the above TSO authorizations are being forwarded under separate cover.
The data being forwarded are the same as itemized in the enclosed letters of TSO authorization, or later drawing revisions reflecting product improvement and minor changes to these instruments. Your office will continue to be advised of any modifications affecting the airworthiness of these items.
Please advise if any additional requirements must be met and if any additional data are needed for your acceptance. Otherwise, if you find this information sufficient, we would appreciate your confirmation that the subject products will be accepted when accompanied by an appropriate FAA export airworthiness approval.
Appendix 2 ENCLOSURE 4
CIVIL AVIATION AUTHORITY AIRWORTHINESS DIVISION BRABAZON HOUSE REDHILL SURREY RH1 1SQ Telephone Redhill 65966 Telex 27100 Telegrams & Cables Bordair Redbil!
APPLICATION FOR APPROVAL OF, OR MODIFICATION TO, AN ACCESSORY Name and Address of Applicant Name and Address of Manufacturer if different from Applicant State whether Initial Full Title of Accessory Approval or Modification Identity or Reference No. - Drawing or Specification No. Declaration of Design and Performance No.
Brief Description of Accessory, or of Modification.
INITIAL APPROVAL - State the condition of the Maintenance, Overhaul and Repair Manuals.
MODIFICATION - Describe briey any complementary amendment necessary to the Maintenance, Overhaul and Repair Manual: otherwise state "'Not Affected".
FOR CAA USE ONLY Cheque P.O. value f I/we hereby apply for approval of the above Accessory/Modification Cash in accordance with British Civil Airworthiness. Requirements, Chapter A3-3 or A3-4 (as applicable). The rum of £5-00 is enclosed Detached by in payment of deposit on the statutory charge.
Folio.. Date.
Internal Reference No. Signed Date 132
Appendix 2
FEDERAL PEOPLE'S REPUBLIC OF
YUGOSLAVIA - SPECIAL REQUIREMENIS 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 ortification, 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 aircraft 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 /IBO/ 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 to aircraft structural parts, and complete information on lubricating, fuel and hydraulic systems.
Appendix 2
n. One copy each or maintenance and service, overnaul, and repair manuals appiying to the aircraft, engines, propellers, or to the equipment installed on the aircraft.
o. A separate parts catalog for the aircraft, 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.
q. Complete manufacturer's service bulletins.
r. 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 guarantee 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 airworthiness certificate was issued for aircraft of that type prior the 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 aircrait, including a flight test checklist utilized when testing the aircraft (tw 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.
i. 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, trequency, 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 flyaway with Yugoslav registration and nationality markings. Mentioned Yugoslav certificates will be issued after basic airworthiness inspection, 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).
1. 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 REQUIREMENTS
1. GENERAL
a. Any aircraft to be eligible for the issue of a Certificate of BESSE Registration issued by the Government 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 Class 2 and Ciass 3 products should be accompanied by documentation which confirms that the item is in accordance with the relevant section of Part 21 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 Aircraft prior to departure from the United States of 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.
3. EACH AIRCRAFT FOR WHICH A ZAMBIAN CERTIFICATE OF AIRNORTHINESS 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. Iwo 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 Whipple Street Panama, and the East Point, GA) Canal Zone
c. Mexico Federal Aviation Administration P.O. Box 1689 Fort Worth, Texas 76101 (Location: 4400 Blue Mound Rd.)
d. Area East of East Federal Aviation Administration Pakistan and India, P.O. Box 4009 including all free Honolulu, Hawaii 96813 nations south and (Location: 1833 Kalakaua Ave.
east of China Honolulu, Hawaii 96815
e. Europe, Africa, Federal Aviation Administration Middle East west Tour-Madou Building of Burma, Iceland, 1 Place Madou Greenland, and 1030 Brussels, Belgium Bermuda 1
1/15/80 AC 21-2D Appendix 4 APPENDIX 4
BILATERAL AIRWORTHINESS AGREEMENTS REPLACEMENT/MODIFICATION REPLACEMENT/MODIFICATION REPLACEMENT/MODIFICATION REPLACEMENT/MODIFICATION COMPONENTS Page COMPOSITE CHART AND AIRWORTHINESS AGREEMENTS SCOPE OF BILATERAL AIRCRAFT PARTS FREEMPORTED AIRCRAFT ENGINES PARTS FOR EXPORTED AIRCRAFT ENGINES PROPELLERS PARTS FOR EXPORTED PROPELLERS APPLIANCES PARTS POR EXPORTED APPLICANCES MATERIAL PARTS SUBASSEMBLIES TREATIES AND OTHER INTERNATIONAL ACT of REVISED 10/5/79 AGREEMENT
SERIES DATE
AUSTRALIA (Ref. Note 4 and 7) ×2 *2 8126 1975 AUSTRIA * 4219 1959 BELGIUM * * ×2 ×2 7675 1973 (Ref. Note 4) BRAZIL (Ref. Note 4) * *2 ×2 p*2 8384 1976 7091 1971 CANADA 131 1938 CZECHOSLOVAKIA 6987 1970 DENMARK 3158 1954 FINLAND *5 7795 1974 FRANCE (Ref, Note 4) * 1×2 ×2 7728 1973 GERMANY _(Ref. Note 4) * * ·2·2 *2 7965 1974 ISRAEL * * 72172 - ×2 7926 1974 6530 1968_ ITALY *2172 7895 1973 (Ref. Note 4) JAPAN * * ×2172 *2 8934 1977 (Bef. Note 4).
NETHERLANDS (Ref. Note 4) * ×2×2 *2 7869 1974 NEW ZEALAND ×3 x2×2 ×2 6857 1878 3769 1957 NORWAY 9141 1978 8407 1976 POLAND ×6 ROMANIA ×1 8440 1976 SOUTH AFRICA 3200 1955 3906 1978 SPAIN SWEDEN *2*21*2 7611 1973 (Ref. Note 4) SWITZERLAND * * * * *2 721 *2 33Ł5 1897 UNITED KINGDOM * * × 7537 1972 (Ret• Note 4) 1
Appendix 4 APPENDIX 4 - Notes
1. Gliders only.
2. Applies only 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 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.
3a. Export from New Zealand to the U.S. 18 limited to:
(1) Fixed-wing aircraft constructed 1n New Zealand not exceeding a maximum weight of 12,500 1bs.
(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.
3b. 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.
(6) Components for use on civil aircraft.