8/7/87 AC 21-2F Appendix 2 II. If an aircraft of the same model previously has been exported to, and certificated in the Philippines, the following documents or materials shall be furnished by the exporter:
a. Sale documents.
b. Current weight and balance report.
c. Export Certificate of Airworthiness.
d. Flight Test Report.
e. Detailed listing of all AD and method and date of each compliance.
f. Any other documentation when specifically asked for.
III. Export - Flyaway Aircraft (new or used)
a. An aircraft which is being exported to the Philippines shall display the Philippine nationality and registration marks and shall carry on the delivery flight:
I. Philippine Registration Certificate.
2. Philippine Certificate of Airworthiness (provisional)
3. Export Certificate of Airworthiness
4. Philippine Ferry Permits
5. 5. Such other documents as may be essential to the safe operation of the aircraft.
IV. It shall be the responsibility of the Philippine purchaser to ensure that the identification markings are properly displayed upon the aircraft prior to departure from the exporter's base and to ensure that the necessary documents are carried on board the aircraft at the time of delivery.
Mailing Address:
Director of Air Transporation Aviation Safety Manila International Airport Pasay City, PHILIPPINES 117
Appendix 2
REPUBLIC OF PORTUGAL - SPECIAL REQUIREMENTS (Revised March 1987)
GENERAL Aircraft or any other Class I product, to be eligible for registration and airworthiness certification by the Government of the Republic of Portugal, must be eligible for certification in the United States, and should be covered by Export Certificates of Airworthiness - FAA Form 8130.4 - in accordance with Part 21 of the United States Federal Aviation Regulations and should comply with the applicable special requirements contained in paragraphs 3., 4., and 5.
NOTE: Aircraft and other Class I products eligible for certification in the U.S. "Restricted," "Limited," or "Experimental" classification, may be exported to the Republic of Portugal only if a prior and specific approval of the Director, Directorate-General of Civil Aviation, is obtained.
Class II and Class III products, to be eligible for approval and installation of certified civil aircraft of Portuguese registry, should be exported in accordance with the applicable provisions of Part 21 of the United States Federal Aviation Regulations. An Airworthiness Approval Tag - FAA Form 8130-3 - is acceptable.
3. The Manufacturer of Supplier must hold or obtain one or more of the following documents, unless otherwise approved by the Republic of Portugal, Directorate- General of Civil Aviation:
(a) A current valid Federal Aviation Administration, Production Certificate (FAA-PC) for the product involved, as outlined in FAR Part 21, Subpart G;
(b) An FAA Approved Production Inspection System (FAA-APIS) letter, as provided in FAR 21, Subpart F;
(C) An FAA replacement and modification Parts Manufacturer Approval (FAA-PMA) letter issued by the FAA as per FAR 21, Subpart K. In this case, parts, containers and invoices, will bear evidence of the manufacturer's name, address, the part number, registered trademark, when described in the FAA approval letter, and the symbol FAA-PMA;
(d) Technical Standard Order (TSO) letter of acknowledgement or authorization issued by the FAA as per FAR Part 21, Subpart 0.
Reconditioned, used or surplus parts must be accompanied by a certificate signed by an appropriately rated FAA certified repair station holding a currently valid certificate, as provided under Part 145 of the United States Federal Aviation Regulations.
(a) The return to service maintenance records required by FAR Part 43 shall accompany the parts;
8/7/87 AC 21-2F Appendix 2
(b) The provisions of this paragraph 4. 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.).
In all instances, suppliers must certify on the face of their invoice, that the product involved was manufactured under one or more of the preceding procedures: 1.e., FAA PC No._ _; FAA-APIS letter dated _; FAA-PMA letter dated ; TSO NO._ _; MIL. Spec.. ; other Government or Industry Specifications
AIRCRAFT OF FIRST OR SAME MODEL in addition to the oregoing, applicable parts of the following requirements prescribed by the Republic of Portugal, Directorate-General of Civil Aviation will be complied with when exporting aircraft:
(a) If the aircraft is the first of a model exported to Portugal, the following material shall be furnished with the new aircraft:
(1) A copy of the type flight test report. Flight characteristics of the aircraft shall be described in this report in a manner convenient for calculating che perrormance of the aircraft over a reasonable range of weights, altitudes and atmospneric conditions. Performance figures contained in, or furnished with the type flight test report, must be corrected to standard atmospheric conditions and a statement to this effect shall be made a part of the report. Established operational limitations, speeds and approved loads shall be indicated;
(2) A copy of the manufacturer's production flight test report applying to the aircraft being operated, including a copy of the flight check-off form utilized when testing the aircraft;
(3) A type record of stress analysis summary showing, for all members of the primary structure, their design loads, dimensions, materials, strength, and margins of safety, or a copy of the static strength test reports when type approval was granted on the basis of such tests. If the aircraft has been approved for ditching in its country of origin, appropriate substantial data shall be submitted;
(4) A statement by an authorized representative of the manufacturer to the effect that all pertinent information, modification service bulletins and revisions and up-dates to such bulletins, will be automatically distributed to the Directorate-General of Civil Aviation of the Republic of Portugal;
(5) Two copies of each of the approved flight manual and weight and balance report applicable to the particular aircraft, including aircraft not exceeding 6,000 lbs. M.T.O.W.;
Appendix 2
(6) One copy of each of the operating manual maintenance and service manual overhaul, wiring diagrams and repair manuals, applying to the aircraft, aircraft engines(s), propeller(s) and major auxiliary equipment installed on the aircraft;
(7) One copy of spare parts relating to the aircraft, aircraft engine(s), propeller(s) and major auxiliary equipment installed;
(8) One copy of maintenance planning data relating to the aircraft;
(9) A list of the necessary special tools and equipment (including a tolerance chart) essential to the inspection and servicing of the aircraft, engine(s), propeller(s) and associated equipment. This should include inspection timetables and appropriate charts and instructions relating to the installed systems;
(10) One copy of information or instructions essential to the assembly and rigging of the aircraft;
(11) A list of communication and navigation equipment installed, by make and model, and operating instructions;
(12) One copy of the current official aircraft, engine and propeller specifications and special conditions and/or exemptions included in the certification basis;
(13) One copy of minimum equipment list (MEL) for aircraft type certificated in Transport category;
(14) One copy of the record of all "mandatory" modifications accomplished prior to exporting, as well as "non-mandatory;"
(15) Certified aircraft, engine(s) and propeller(s) logbook or other equivalent historical records showing total operating time and time since overhaul;
(16) A written undertaking shall be furnished by the manufacturers of the aircraft, its engine(s) and propeller(s) to supply as appropriate all amendments and reissues for the data specified in paragraphs (a) (5) through (a)(10);
(17) Any other information or documentation when specifically asked for.
(b) If an aircraft of the same model has previously been exported to and certified in Portugal, the following documents or material shall be furnished with the new aircraft:
(1) One copy of approved flight manual and weight and balance report applicable to the particular aircraft, including aircraft not exceeding 6,000 lbs. M.T.O.W.;
Appendix 2
(2) Certified aircraft, engine(s) and propeller(s) logbooks or other equivalent historical records, showing total operating time and time since overhaul;
(3) Record of all modifications accomplished prior to exporting, "mandatory" as well as "non-mandatory;"
(4) A list of communications and navigation equipment installed by make and model, and operating instructions;
(5) Any other information or documentation when specifically asked for.
(c) If the aircraft is certificated in the restricted category, the following material shall be furnished with aircraft in addition to above 6(a):
(1) A statement by the Federal Aviation Administration, describing the manner in which the aircraft has been modified from the "standard category" configuration to make it suitable for "special purpose" operation;
(2) A statement indicating part of the Federal Aviation Regulations, the Special technical requirements:
7. Noise Limits:
An aircraft will be eligible for a Certificate of Airworthiness only If it complies with the noise standards of ICAO Annex 16, Volume I, First Edition (1981), chapters 2, 3, 5 or 6, as applicable. The following material shall be furnished with the aircraft, in addition to referred in paragraph 6:
(a) Certified maximum noise levels and their 90 percent confidence limits in accordance with the applicable chapters and appendix of the ICAO Annex 16, Volume I, First Edition (1981);
(b) Description of noise measuring and analyzing procedures including correction methods which should include the following items:
(1) A measured and corrected sound pressure levels presented in one-third octave band levels obtained with equipment conforming to the standards described in applicable chapters of the ICAO Annex 16, First Edition.
(2) The type of equipment used for measurement and analysis of all acoustic aeroplane performance and meteorological data.
Appendix 2
(3) The following atmospheric environmental data, measured immediately before, after, or during each test at the observation points prescribed in applicable chapters and appendices of the ICAO Annex 16, First Edition.
(i) Air temperature and relative humidity.
(11) Maximum, minimum and average wind velocities.
(ii1) Atmospheric pressure.
interfere with sound recordings. (4) Comments on local topography, ground cover, and events that might
(5) The following aeroplane information:
(1) Type, model and serial number (if any) of aeroplane and engines.
(11) Gross dimensions of aeroplane and location of engines.
(111) Aeroplane gross weight for each test run.
(tv) Aeroplane configuration such as flap and landing gear positions.
(v) Airspeed in knots.
(vi) Engine performance in terms of net thrust, engine pressure ratios jet exhaust temperatures and fan or compressor shaft rotational speeds as determined from aeroplane instruments and manufacturer's data.
(vi1) Aeroplane height above ground determined by a method independent of cockpit instrumentation such as radar tracking, theodolite triangulation, or photographic scaling techniques approved by the certification authorities.
(6) Aeroplane speed and position and engine performance parameters recorded at an approved sampling rate sufficient to correct to the noise certification reference conditions and synchronized with the noise measurement.
(7) Lateral position relative to the extended center line of the runway, configuration, and gross weight.
(8) Description of such noise measuring and analyzing procedures including correction methods that differ from or are not specified in the ICAO Annex 16, First Edition (1981), if any.
(9) Description and analysis of the sources of possible errors which may exist in the final values of EPNL.
(c) Statement of any additional modification incorporated for the purpose of compliance with the applicable noise certification standards.
Appendix 2
8. Radio Equipment Radio equipment must be FAA approved and comply with TSO/FAA TC specifications. When a radio equipment model is exported to Portugal for the first time, one copy of the following material will be furnished:
- The manufacturer's statement of conformance submitted to FAA.
- The letter of acceptance issued by FAA.
- The technical manuals and bulletins (service bulletins, etc).
Special technical requirements regarding the radio equipment are:
- VHF radio-communication equipment must be compatible for use with 25 kHz spacing between channels;
- VHF radio-navigation equipment must be compatible for use with 50 kHz spacing between VOR and LOC channels and 150 kHz between associated glide slope channels.
- Communication and navigation antennas are to be distinct.
- VOR/LOC and glide slope antennas are to be distinct.
9. Flight Instruments Airspeed indicators must show airspeed in knots only.
Altimeters must be of the sensitive type, showing altitude in feet, with adjustable setting in millibar scale.
10. Flight Data Recorder and Cockpit Voice Recorder Turbine powered transport category airplanes of a maximum weight of over 5,700 kg must be equipped with an approved flight data recorder. When the maximum weight is over 27,000 kg, an approved cockpit voice recorder is also required. The technical manuals and the last calibration charts pertinent to the installed recorders will be furnished.
11. Changes to Type Certification Each change of a product must be FAA approved and related material must be furnished for its inclusion in the type design. Changes in this context are:
(a) "Major changes" according to FAR 21.93(a); and
(b) Changes covered by a supplemental type certificate in accordance with FAR Part 21, Subpart E.
Appendix 2
EXPORT - FLYAWAY AIRCRAFT
12. An aircraft being exported to Portugal via flyaway, without U.S. nationality and registration marks, should display Portuguese nationality and registration marks and should carry the following documents on the delivery flight:
(a) Portuguese Certificate of Registration;
(b) Portuguese Certificate of Airworthiness;
(c) U.S. Certificate of Afrworthiness for Export - FAA Form 8130-4;
(d) FAA Approved Flight Manual;
(e) Portuguese Radio License or a letter of authority to cover the use of radio, valid for the delivery flight, for the radio equipment installed on the aircraft;
(f) Such other documents as may be essential for the safe operation of the aircraft.
NOTES: 1) - (a) and (b) may be replaced by a Special Permit for a delivery flight. The Government of Portugal, the Directorate-General of Civil iation, requests to be advised by cable of the issuance of a Certificate of lirworthiness for Export in respect to any aircraft which is to De exported to Portugal via flyaway.
2) - It will be the responsibility of the Portuguese purchaser to ensure that the identification marks are properly displayed upon the aircraft prior to the departure from the exporter's base and to ensure that the necessary flight documents are installed and carried in the aircraft during the delivery flight.
NOTES
13. The address of the Directorate-General of Civil Aviation of Portugal is as follows:
PORTUGUESE GOVERNMENT
DIRECCAO-GERAL DA AVIACAO CIVIL
DIRECCAO DO MATERIAL AERONAUTICO Rua B - Edificio 6 - Aeroporto 1700 - LISBOA (Portugal) CABLE ADDRESS: AEROCIVIL LISBOA TELEX: 12120 AERCIV P PHONES: 88 81 51 - 88 81 52 - 88 81 53 - 89 66 71
14. The manufacturer or exporter will be advised by purchaser on the basis of information furnished to the purchase by the Directorate-General of Civil Aviation of Portugal when an aircraft is the first of a type or model to be imported into Portugal.
Appendix 2
KINGDOM OF SAUDI ARABIA - SPECIAL REQUIREMENTS (Revised - August 30, 1983)
1. GENERAL Aircraft and other Class I, Il and Ill products to be eligible for export to the Kingdom of Saudi Arabia, in addition to the requirements prescribed in Part 21 of the U.S. FARs, must be eligible for airworthiness certification in the "standard" classification and comply with the applicable special requirements.
NOTE: Aircraft eligible for certification in the United States, 'restricted, " "limited," or "experimental" classification, may be exported to the Kingdom of Saudi Arabia only if a prior and specific approval of the Director General of Civil Aviation is obtained.
b. In all instances, manufacturers or suppliers must certify on the face of their invoice that the product involved was manufactured under one or more of the preceding procedures: 1.e., FAA PC No.; FAA - APIS letter dated: FAA - PMA letter dated; TSO No.; MIL. Spec.; other government or industry specifications.
2. AIRCRAFT OF FIRST OR SAME MODEL d • In addition to the foregoing the following requirements prescribed by the Kingdom of Saudi Arabia will be complied with when exporting aircraft:
(1) If the aircraft is the first of a model exported to the Kingdom of Saudi Arabia, the following material shall be furnished to the DGCA, including revision service.
(a) Approved Flight Manual.
(b) Production Flight Test Report.
(c) Weight and Balance Report.
(d) Aircraft Operating Manual.
(e) Aircraft, Powerplant, Propeller and APU;
1 Maintenance Manual 2 Overhaul Manual 3 Structural Repair Manual 4 Tool and Equipment Manual
(f) Alert and/or Highly Recommended Service Bulletins.
Appendix 2
(g) Maintenance/Inspection Program Planning Document/Data.
(h) Detailed listing of all Airworthiness Directives, method and date of compliance, if applicable.
(2) If an aircraft of the same model previously has been exported to, and certificated in the Kingdom of Saudi Arabia, the following documents or material shall be furnished by the exporter.
(a) Current Weight and Balance Report
(b) Flight Test Report
(c) Detailed listing of all Airworthiness Directives and method and date of each compliance
(d) Any other information or documentation when specifically asked tor
3. EXPORT - FLYAWAY AIRCRAFT
a. An aircraft which is being exported to the Kinydom of Saudi Arabia via flyaway should display Saudi Arabian nationality and registration marks and should carry the following documents on the delivery flight:
(1) Saudi Arabian Certificate of Registration;
(2) Saudi Arabian Certificate of Airworthiness or Delivery Flight Authorization'u.S. Certificate of Airworthiness for Export; (5) Suproved Flocaus Such other documents as may be essential to the safe operation of the aircraft.
b. The Saudi Arabian Director General of Civil Aviation requests to be advised by telegram of the issuance of a Certificate of Airworthiness for Export in respect of any aircraft which is to be exported to the Kingdom of Saudi Arabia via flyaway.
NOTE: It will be the responsibility of the Saudi Arabian purchaser to ensure that the identification markings are properly displayed upon the aircraft prior to departure from the exporter's base and to ensure that the necessary flight documents are installed and carried in the aircraft during the delivery flight.
Mailing Address:
Presidency of Civil Aviation Director of Flight Standards Department P.0. Box 887 Jeddah, Saudi Arabia Cable Address:
PCA - FSD 403235 SJ 126
Appendix 2
REPUBLIC OF SINGAPORE - SPECIAL REQUIREMENTS (Revised November 3, 1978)
1. The following identifies those special administrative requirements which must be satisfied at the time of export (in addition to any additional validation Requirements) for a particular product to be eligible for a Singapore registration certification and/or airworthiness validation:
a. New Aircraft.
* (1) Statement of Build Standard. This statement to include the aircraft specification and a list of Service Bulletins incorporated in production.
(2) Statement of Modification status (above 2730 kg). This must include:
(1) Customer options incorporated;
(11) Equipment incorporated;
(iii) Service Bulletin including Alert Service Bulletin compliance.
(3) FAA Export Certificate of Airworthiness.
NOTE: It will be necessary for this to be supplied in advance of the aircraft delivery date, so that the Singapore Certificate of Validation may be issued and accompany the aircraft during training flying and delivery flight.
(4) Airworthiness Directives. A declaration of compliance with all Airworthiness Directives issued by the FAA must be provided. Where optional means of compliance are offered, the means chosen shall be stated.
* (5) Type Certificate Technical Data Sheets or Specifications. FAA Aircraft, Engine and Propeller Data Sheets including any supplemental type specifications.
(6) Equipment List.
* (7) Wiring Diayram.
(8) Weight schedule and weighing report.
Appendix 2 * (9) Electrical load analyses.
* (10) MRB program, where applicable.
(11) Time/Life limitations.
(12) Copy of Production Flight Test Report related to the specific aircraft.
(13) Record of Compass System and Magnetic compass swings.
(14) Detailed list of radio equipment constituting the radio station.
(15) Statement of compliance with mandatory equipment and radio apparatus as specified in the schedules of the Singapore Air Navigation Order.
(16) MANUALS: Number Required * (1) Flight Manual 1 (+1 for each aircraft) * (ii) Aircraft Maintenance and Overhaul * (iii) Operations 1 * (iv) Engine Maintenance and Overhaul 1 * (v) Maintenance Planning Guide * (vi) Structural Repair 1 * (vif) Parts Catalog 1 * (viii) Weight and Balance Loading Procedures * (ix) Standard Practices 1 * (x) Propeller Maintenance and Overhaul 1 * (xi) Structurally Significant Items 1 * (x11) Complete set of Service Bulletins (Aircraft) 1 128