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									   Regulations Governing the Certification for Aviation Products,
                      Appliances and Parts

Promulgated on March 2, 2000.
Amendment to Articles 15 and 16, promulgated on September 19, 2000.
Amendment to Articles 1, 12 and Attachments, promulgated on December 23, 2005.
Amendment to Article 15, promulgated on August 28, 2007.
Amendment to all Articles promulgated on August 22, 2008.



                                        Chapter 1
                                         General

Article 1
      The Regulations are established pursuant to the provisions of Paragraph 3, Article 9
of the Civil Aviation Act.


Article 2
     In the Regulations herein, the definition of the terms referred hereinafter shall be:
      1) ―Appliance‖ means major components of aviation products and the failure of
          which will endanger the operation safety of the product.
      2) ―Part‖ means parts and components that are used on aviation products and
          appliances.
      3) ―Type Certificate (TC)‖ means a design approval issued when the applicant
          demonstrates that a product complies with the applicable regulations.
      4) ―Supplemental Type Certificate (STC)‖ means a design approval issued by the
         Civil Aeronautics Administration (CAA) approving a major design change for a
         type certificated aviation product when the applicant demonstrates that the
         design change complies with the applicable regulations.
      5) ―Type Validation Certificate (VTC)‖ means a design approval issued by the
         Civil Aeronautics Administration (CAA) approving an imported aviation product
         when the applicant demonstrates that the product complies with the applicable
         regulations.
      6) ―Production certificate‖ means an approval to manufacture duplicate products
         under a type certificate or a supplemental type certificate.
      7) ―Parts Manufacturer Approval (PMA)‖ means a combined design and production
         approval for modification and replacement parts for installation on type
         certificated products.


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8) ―Technical Standard Order (hereinafter referred to as TSO)‖ means the minimum
    performance standards that Civil Aeronautics Administration prescribes for TSO
    articles.
9) ―Technical Standard Order Article (Hereinafter referred to as TSO Article)‖
    means parts or components that are found to meet a specific TSO.
10) ―Technical Standard Order Authorization (TSOA)‖ means a combined design
    and production approval issued by the Civil Aeronautics Administration (CAA)
    for a TSO Article when the applicant demonstrates that the design change
    complies with the applicable regulations.
11) ―Production Approval Holder (PAH)‖ means a manufacurer who holds a
    production certificate, a parts manufacturer approval, or a technical standard
    order authorization.
12) ―Airworthiness Directive (AD)‖ means a notification issued by the CAA or other
    national civil aviation authorities to aircraft owners and operators of a known
    safety deficiency with a particular aviation product, equipment, component or
    parts and the necessary actions that they shall comply with. An AD is issued
    when an unsafe condition exists in a product, equipment, component or parts and
    the condition is likely to exist or develop in other products, equipment,
    components or parts of the same design.
13) ―Normal Category Aircraft‖ means an aircraft which satisfies the conditions
    below and is certified as a normal category aircraft by the CAA or by the civil
    aviation authority of the design state of the aircraft and intended for
    non-acrobatic operation:
   (a) airplane that has a seating configuration, excluding pilot seats, of nine or less
       and a maximum certificated takeoff weight of 5700 kg or less; or
   (b) helicopter that has a maximum certificated takeoff weight or maximum
       weight of 3180 kg or less.
14) ―Acrobatic Category Aircraft‖ means an airplane has a seating configuration,
    excluding pilot seats, of nine or less and a maximum certificated takeoff weight
    of 5700 kg or less and is certified as an acrobatic category airplane by the CAA
    or by the civil aviation authority of the design state of the aircraft.
15) ―Utility Category Aircraft‖ means an airplane has a seating configuration,
    excluding pilot seats, of nine or less and a maximum certificated takeoff weight
    of 5700 kg or less and is certified as a utility category airplane by the CAA or by
    the civil aviation authority of the design state of the aircraft.
16) ―Commuter Category Aircraft‖ means an airplane has a seating configuration,
    excluding pilot seats, of 19 or less and a maximum certificated takeoff weight of
    8640 kg or less and is certified as a commuter category airplane by the CAA or


                                      -2-
          by the civil aviation authority of the design state of the aircraft. The commuter
          category airplane is intended for non-acrobatic operation.
      17) ―Transport Category Aircraft‖ means an aircraft certified as a transport category
          aircraft by the CAA or by the civil aviation authority of the design state of the
          aircraft. The Transport Category Airplane is intended for non-acrobatic
          operation.


Article 3
     The holder of a Type Certificate (TC), a Supplemental Type Certificate (STC), a Parts
Manufacturer Approval (PMA), a Technical Standard Order Authorization (TSOA), or the
licensee of a Type Certificate shall report to the CAA any failure, malfunction or defect
during operation in any product, parts, or article, that has left its quality control system and
that it determines has resulted in any of the occurrences listed in this article. The initial
report shall be made in a prescribed form to the CAA within 24 hours after it has
determined that the malfunction, failure, or defect required to be reported has occurred.
       1) Fires caused by a system or equipment failure, malfunction, or defect;
       2) An engine exhaust system failure, malfunction, or defect which causes damage
           to the engine, adjacent aircraft structure, equipment, or component;
      3) The accumulation or circulation of toxic or noxious gases in the crew
         compartment or passenger cabin;
      4) A malfunction, failure, or defect of a propeller control system;
      5) A propeller of rotor craft hub or blade structural failure;
      6) Flammable fluid leakage in areas where an ignition source normally exists;
      7) A brake system failure caused by structural or material failure during operation;
      8) A significant aircraft primary structural defect or failure caused by any
         autogenous condition (fatigue, corrosion, under-strength, etc.);
      9) Any abnormal vibration or buffeting caused by a structural or system
          malfunction, defect, or failure;
      10) An engine failure;
      11) Any structural or flight control system malfunction, defect, or failure which
          causes an interference with normal control of the aircraft for which derogates the
          flying qualities;
      12) A malfunction or failure of more than one airspeed, attitude or altitude
          instrument during a given operation of the aircraft;
      13) A complete loss of more than one electrical power generating system or
          hydraulic power system during a given operation of the aircraft.
      Whenever the investigation of an accident or service difficulty report shows that an
article manufactured under the holder of a Type Certificate (TC), a Supplemental Type


                                              -3-
Certificate (STC), a Parts Manufacturer Approval (PMA), a Technical Standard Order
Authorization (TSOA), or the licensee of a Type Certificate shall report to the CAA the
results of its investigation and any action taken or proposed by the manufacturer to correct
that defect. If action is required to correct the defect in existing articles, the manufacturer
shall submit the data necessary for the issuance of an appropriate airworthiness directive to
CAA.


Article 4
     An applicant for Type Certificate (TC), Supplemental Type Certificate (STC),
Technical Standard Order Authorization (TSOA) governed by the applicable requirements
of the airworthiness standards, may petition the CAA (attachment 2) for a temporary or
permanent exemption from certain provisions of the airworthiness standards for technical
reasons.

Article 5
      For international cooperation on aviation product design, manufacture or assembly,
the certification shall be in accordance with the regulations herein unless an arrangement
between CAA and the foreign authority(ies) involved is otherwise established.


Article 6
     Appliances imported shall be certificated or validated in accordance with the
regulations herein unless an arrangement between CAA and the foreign authority(ies)
involved is otherwise established.


                                       Chapter 2
                                     Type Certificate
Article 7
      When applying for approval of a type design of any aircraft product, the applicant
should submit the application form (See attachment 3) to CAA for approval. An applicant
is entitled to a type certificate (See attachment 4) for an aircraft product if his/her
application is approved by CAA.
      An application for an aircraft type certificate must be accompanied by a three-view
drawing of that aircraft and available preliminary basic data. An application for an aircraft
engine type certificate must be accompanied by a description of the engine design features,
the engine operating characteristics, and the proposed engine operating limitations.


Article 8
     An applicant for a type certificate must show that the aircraft product concerned


                                             -4-
meets the applicable requirements that are effective on the date of application for that
certificate except the noise, fuel venting and exhaust emission requirements that have been
prescribed in other existing regulations.
       An application for type certification of transport category aircraft is effective for five
years, and an application for any other type certificate is effective for three years, unless an
applicant shows at the time of application that his/her product requires a longer period of
time for design, development, and testing, and the CAA approves a longer period.


Article 9
      Each person who proposes to change a type certified product must apply for a new
type certificate in accordance with Article 7, if CAA finds that the proposed change in
design, power, thrust, weight, engine rating limitation or speed limitation is so extensive
that a substantially complete investigation of compliance with the applicable regulations is
required.

Article 10
     Each applicant must allow CAA to make any inspection and, upon request by CAA,
make any inspection, flight and ground test necessary to determine compliance with the
applicable requirements. Each applicant must carry on all necessary inspections and tests
necessary to ensure that--
      1) The product concerned complies with the applicable airworthiness, aircraft noise,
          fuel venting, and exhaust emission requirements;
      2) Materials and products conform to the specifications in the type design;
      3) Parts of the products conform to the drawings in the type design; and
      4) The manufacturing processes, construction and assembly conform to those
          specified in the type design.
      Except as approved by CAA, the applicant should submit to CAA a statement,
certifying that the requirements stipulated in subparagraph (2)~(4) of the first paragraph of
this Article have been complied with, prior to his/her submission to CAA for inspection or
conduct any flight test or ground test requested by CAA,
      Except as approved by CAA, no change may be made to an aircraft product between
the time that compliance with subparagraph (2)~(4) of the first paragraph of this Article is
shown for that aircraft product and the time that it is presented to the CAA for test.
      The type design, as cited in the first paragraph of this Article, consists of
      1) The drawings and specifications, and a listing of those drawings and
         specifications, necessary to define the configuration and the design features of
         the product shown to comply with the requirements applicable to the product;
      2) Information on dimensions, materials, and processes necessary to define the


                                              -5-
         structural strength of the product;
      3) The Airworthiness Limitations section of the Instructions for Continued
         Airworthiness as required by applicable airworthiness standards;
      4) Any other data necessary to allow, by comparison, the determination of the
         airworthiness, noise characteristics, fuel venting, and exhaust emissions (where
         applicable) of later products of the same type.


Article 11
     When performing the flight tests as required in Article 10 of the regulations herein,
each applicant must abide by the requirement enclosed in Attachment 5.


Article 12
       Each applicant for a utility, acrobatic, commuter or transport category aircraft type
certificate must provide a person holding an appropriate pilot certificate who has
undertaken sufficient training to make the flight tests required by the regulations herein.


Article 13
     Each applicant for a utility, acrobatic, commuter, or transport category aircraft type
certificate must submit a report to CAA showing computations and tests that are required--
       1) In the connection with the calibration of instruments used for test purposes and;
       2) In the correction of test results to standard atmospheric conditions.
       CAA may require the applicant to conduct any flight test that it finds necessary to
check the accuracy of the report submitted under the first paragraph of this Article.


Article 14
     An applicant is entitled to a type certificate for an aircraft product, if CAA determines
that an application of type certificate submitted in accordance with Article 7 of the
regulations herein fulfills the followings:
      1) The applicant has submitted the type design, test reports, and computations
          necessary to show that the product to be certificated meets the applicable
          airworthiness, aircraft noise, fuel venting, and exhaust emission requirements
          and any other applicable airworthiness provisions;
      2) The type design complies with--
          a) The applicable airworthiness requirements and that any airworthiness
              provisions not complied with are compensated for by factors that has been
            approved by CAA to provide an equivalent level of safety and;
         b) Other applicable noise, fuel venting, and emissions requirements, if exist;
      3) No feature or characteristic makes it unsafe exists.


                                             -6-
Article 15
      For foreign aviation products that are certified by the cognizant Aviation Authorities
to be imported for civil aviation operation, the holder of the type certificate shall apply to
CAA for a type validation certificate (VTC, see Attachment 7) in accordance with type
validation procedure (See Attachment 6) unless an arrangement between CAA and the
foreign authority(ies) involved is otherwise established.


Article 16
     When petitioning for transfer of type certificate, the grantor shall provide CAA both
the original type certificate and the transferring agreement. A revised type certificate will
be issued to the grantee when the said petition is approved by CAA.


Article 17
     The holder of a type certificate for an aircraft may apply to CAA for—
      1) Production Certificate per Chapter 5 of the regulations herein;
      2) Airworthiness certificates per Chapter 6 of the regulations herein;
      3) Approval of replacement parts for that product.
     In the case of aircraft engines, or propellers, the holder of a type certificate may apply
to CAA for approval for installation on certificated aircraft.


Article 18
      The holder of a type certificate for an aircraft product shall, in a timely manner,
furnish the complete Instructions for Continued Airworthiness and its amendments, as
specified in the applicable airworthiness standards, to CAA and all owners of the aircraft
product involved.
      The holder of a type certificate for an aircraft shall establish the maintenance
program which includes a corrosion prevention program, to ensure the structural integrity
of that aircraft.


                                      Chapter 3
                              Changes to Type Certificates
Article 19
     Changes of type design are classified as follows:
      1) A "minor change" is one that has no appreciable effect on the weight, balance,
          structural strength, reliability, operational characteristics, noise, fuel venting, and
         emissions, or other characteristics affecting the airworthiness of the product.
      2) All other changes are "major changes".



                                              -7-
Article 20
       Minor changes in a type design can be undertaken only after the holder of the type
certificate has received CAA approval for minor design change. When such design change
has been completed, the holder of the type certificate should provide CAA with all the
related substantiating and technical data. In addition, the holder of type certificate shall
return the original type certificate to the CAA and apply for revising type certificate, if
deemed necessary.


Article 21
      In the case of a major change in type design, the applicant must submit substantiating
data and necessary descriptive data, along with a statement that the changed type design
complies with the requirement stipulated in Article 23 of the regulations herein. The
major change of type design can only be undertaken after CAA approval. In addition, the
holder of type certificate shall return the original type certificate to CAA and apply for
revising type certificate, if deemed necessary.


Article 22
     When the issuance of an Airworthiness Directive for a type certified aircraft product
is deemed necessary by CAA, the holder of the type certificate must submit appropriate
design changes to CAA for approval. When approved, the holder shall make information
on the design changes available to all operators of same type of product.
      When a design change to the type design of type certified aviation product is deemed
advantageous to enhance the flight safety of that product, as determined by CAA or by the
holder of the type certificate, the holder of the type certificate may submit appropriate
design changes to CAA for approval. Upon approval, the holder shall make information on
the design changes available to all operators of same type of product.


Article 23
      An applicant for changes to type design, operation limitations, Type Certificate Data
Sheets (TCDS) and restrictions relating to the type certified aircraft product, must show
that the changed product complies with the airworthiness requirements applicable to the
category of the product in effect on the date of the application for the change and/or any
other applicable noise, fuel venting and exhaust emission requirements.
      Except as provided in the first paragraph of this Article, if an applicant shows that the
amendment of a regulation and/or that a CAA previously granted equivalence of safety, as
in effect on the date of application of original type certificate, brings no significant impact
on flight safety, the previously defined requirement may be kept in effect, if approved by
CAA, for the changed product.


                                             -8-
                                    Chapter 4
                           Supplemental Type Certificates
Article 24
      Any person who alters a product by introducing a major change in type design, not
great enough to require a new application for a type certificate under Article 9 of the
regulations herein, shall apply to the CAA for a supplemental type certificate, except that
the holder of a type certificate for the product may apply for amendment of the original
type certificate in accordance with the requirement stipulated in Chapter 3 of the
regulations herein. The application must be made on the appropriate form, including all the
relevant design data. An applicant is entitled to a supplemental type certificate for an
aircraft product (See attachment 8) if his/her application is approved by CAA. The
requirements of Article 23 must be complied with.


Article 25
      When petitioning for the transfer of a supplemental type certificate, the grantor shall
provide CAA both the original supplemental type certificate and the transferring agreement.
A revised supplemental type certificate will be issued to the grantee when the said petition
is approved by CAA.


Article 26
       The holder of a supplemental type certificate for an aircraft may apply to CAA for—
        1) Production Certificate per Chapter 5 of the regulations herein;
        2) Airworthiness certificates per Chapter 6 of the regulations herein;
        3) Approval of replacement parts for that product.
       In the case of aircraft engines, or propellers, the holder of a supplemental type
certificate may apply to CAA for approval for installation on certified aircraft.


Article 27
      The holder of a supplemental type certificate shall, in a timely manner, furnish the
complete Instructions for Continued Airworthiness and its amendments, as specified in the
applicable airworthiness standards, to CAA and all owners of the aircraft product involved.
      The holder of a supplemental type certificate for an aircraft shall establish the
maintenance program which includes corrosion prevention, to ensure the structural
integrity of that aircraft.


                                      Chapter 5
                                 Production Certificate



                                            -9-
Article 28
      Any manufacturer may submit company and factory registration certificates to apply
 for a production certificate if he holds, for the product concerned a:
       1) Current type certificate;
       2) Right to the benefit of that type certificate under a licensing agreement; or
       3) Supplemental type certificate.


Article 29
     The applicant must show that he has established and can maintain a quality control
 system for any product, for which he requests a production certificate, so that each
 product will meet the design provisions of the pertinent type certificate.


Article 30
     Each applicant must submit attachment 9 applicable data to the CAA, for approval,
 data describing the inspection and test procedures necessary to ensure that each product
 produced conforms to the type design and is in a condition for safe operation.
     Each prime manufacturer shall make available to the CAA information regarding all
 delegation of authority to suppliers to make major inspections of parts or assemblies for
 which the prime manufacturer is responsible.


Article 31
      An applicant is entitled to a production certificate (Attachment 10), if the CAA finds,
 after examination of the supporting document, quality control data and after inspection of
 the organization and production facilities, that the applicant has established and
 maintained compliance with the requirements of Article 29 and Article 30 of this chapter,
 to ensure that each product produced meets the design requirements under the type
 certificate.
      A production certificate is not transferable.


Article 32
      After the issue of a production certificate, each change to the quality control system
 is subject to review by the CAA. The holder of production certificate shall immediately
 notify the CAA of any change that may affect the inspection, conformity, or airworthiness
 of the product. CAA may request any inspection and testing.


Article 33
     The holder of a production certificate desiring to amend it to add a type certificate or
 model, or both, must apply therefore in a form and manner prescribed by the CAA. The


                                             - 10 -
 applicant must comply with the applicable requirements of Article 29, Article 30 and
 Article 32 of this chapter.


Article 34
     Each holder of a production certificate shall allow the CAA to make any inspections
 and tests necessary to determine compliance with the applicable regulations.


Article 35
     The holder of a production certificate shall display it prominently in the main office
 of the factory in which the product concerned is manufactured.


Article 36
     The holder of a production certificate shall:
      1) Maintain the quality control system in conformity with the data and procedures
          approved for the production certificate;
      2) Determine that each product submitted for airworthiness certification or approval
          conforms to the type design and is in a condition for safe operation.


Article 37
      The holder of a production certificate after temporary registration may apply for an
 aircraft airworthiness certificate under chapter 6 requirement.
      In the case of an aircraft engine or propeller, apply an airworthiness approval tag for
 installation on certificated aircraft.


Article 38
     Each manufacturer of a product being manufactured under a type certificate shall
 submit a production inspection system, an approved flight test procedure, acceptable
 testing of engines and propellers and airworthiness approval procedures approved by
 CAA.




                                            - 11 -
                                        Chapter 6
                               Certificate of Airworthiness

Article 39
      Aircraft under the Republic of China's registration, the owner or operator must apply
for its airworthiness certification to the Civil Aeronautics Administration. The Certificate
of Airworthiness (attachment 11) or Special Airworthiness Certificate (attachment 12), as
appropriate, will be issued when the aircraft is found to meet the airworthiness standards.
      Airworthiness certificates are classified as normal, acrobatic, utility, commuter, and
transport category aircraft.
      Special airworthiness certificates are classified as special flight permits and
experimental certificates.

Article 40
      The Certificate of Airworthiness is valid for one year. In special circumstances, the
Civil Aeronautics Administration may issue a Certificate of Airworthiness valid for less
than a year.
       The validity period of a Special Airworthiness Certificate must be specified on the
certificate.
       The owner or operator shall not operate the aircraft beyond the limitations authorized
by airworthiness certificate.
       Upon the expiration of the aircraft's Certificate of Airworthiness, the operator shall
return the certificate to the Civil Aeronautics Administration within 20 days since its
expiration. The Civil Aeronautics Administration will publicly nullify the Certificate of
Airworthiness if the operator fails to return the Certificate of Airworthiness after the
expiration of the Certificate of Airworthiness.
      Special Certificate of Airworthiness should be returned to the Civil Aeronautics
Administration within 3 days since its expiration. The Civil Aeronautics Administration
will publicly nullify the Special Certificate of Airworthiness if the operator fails to return
the Certificate of Airworthiness after the expiration of the Special Certificate of
Airworthiness.


Article 41
     Aircraft's Certificate of Airworthiness must be displayed in the aircraft cabin or
cockpit at a readily visible spot.




                                            - 12 -
Article 42
       For the initial application of an aircraft's Certificate of Airworthiness, the owner or
operator must submit application documents 30 days before the intent of the aircraft's
operation to the Civil Aeronautics Administration.
       Initial application for Certificate of Airworthiness for aircraft imported from a foreign
country should have satisfactorily completed acceptance inspections and flight tests. The
application package should also include a copy of type validation certificate, export
certificate of airworthiness issued by the aviation authority of the state of manufacture or
the state of registry, noise certificate and other related documents required by the Special
Airworthiness Requirements. The Civil Aeronautics Administration may require additional
flight tests when deemed necessary.
      Application for renewal of the Certificate of Airworthiness should be submitted to the
CAA 30 days prior to the expiration date.

Article 43
      Imported cargo aircraft older than 14 years, in addition to meeting requirements
described in Article 42, must submit previous structural maintenance records, the structural
integrity program and the supplemental inspection program when applying for the issuance
of a Certificate of Airworthiness.
       The use of a cargo aircraft imported per the above paragraph shall not be changed
after the issuance of the Certificate of Airworthiness.


Article 44
      The aircraft's owner or the operator should continuously provide the Civil
Aeronautics Administration a current and complete set of all applicable manuals and
related documents.


Article 45
      Each applicant for an airworthiness certificate must show that his aircraft is identified
as prescribed in Article 71.


Article 46
      The applicants that meet the requirements of Attachment 13 may apply for a special
flight permit or an experimental certificate.
      For aircraft operated under a special airworthiness certificate, the owner or operator
should conduct the flight operation in accordance with the Civil Aeronautics
Administration approved flight area, nature of operation, valid period and other limitations.



                                             - 13 -
Article 47
     An applicant for a special flight permit must submit an application form and data
package to the Civil Aeronautics Administration, indicating:
      1) The purpose of the flight.
      2) The proposed itinerary.
      3) The crew required to operate the aircraft and its equipment.
      4) The ways, if any, in which the aircraft does not comply with the applicable
          airworthiness requirements.
      5) The operating limitations for safe operation and the substantiation of information
         necessary for the purpose of prescribing operating limitations.


Article 48
     An applicant for an experimental certificate must submit the following information to
the Civil Aeronautics Administration:
      1) The purpose for which the aircraft is to be used.
      2) Enough data (such as photographs) to identify the aircraft.
      3) Any pertinent information necessary to safeguard the general public.
      4) An execution plan which includes:
         (a) The purpose of the experiment;
         (b) The estimated time or number of flights required for the experiment;
         (c) The areas over which the experiment will be conducted; and
         (d) Three-view drawings or three-view dimensioned photographs of the aircraft.


                                  Chapter 7
            Approval of Materials, Parts, Processes, and Appliances

Article 49
     Whenever a material, part, process, or appliance is required to be approved under
 these regulations, unless it is designed、manufactured and marked according to the
 industry standards that is recognized by CAA, it may be approved:
      1) Under a Parts Manufacturer Approval under this subpart;
      2) Under a TSO Authorization issued under Chapter 8;
      3) In conjunction with type certification procedures for a product; or
      4) By an owner or operator for maintaining or altering his own product.




                                           - 14 -
Article 50
      An applicant shall apply to the CAA for a Parts Manufacturers Approval. An
 applicant is entitled to a PMA Certificate (see Attachment 14) if its product is properly
 certified by CAA .The applicant shall submit to CAA the following:
       1) The PMA application form (see Attachment 15);
       2) Drawings and specification necessary to show the configuration of the part;
       3) Information on dimensions, materials, and processes necessary to define the
           structural strength of the part; and
      4) Test reports and computations necessary to show that the design of the part meets
         the applicable airworthiness requirements, unless the applicant shows that the
         design of the part is identical to the design of a part that is covered under a type
         certificate. If the design of the part was obtained by a licensing agreement,
         evidence of the agreement must be furnished.

Article 51
      Each holder of a Parts Manufacturer Approval shall establish and maintain a
 fabrication inspection system (see Attachment 16) that ensures that each completed part
 conforms to its design data and is safe for installation on applicable type certificated
 products.
      The PMA applicant shall submit a statement certifying that he has established the
 fabrication inspection system as above required, and has presented the data to the CAA.


Article 52
     Each applicant for a Parts Manufacturer Approval must make all inspections and tests
 necessary to determine--
      1) Compliance with the applicable airworthiness requirements;
      2) That materials conform to the specifications in the design;
      3) That part conforms to the drawings in the design; and
      4) That the fabrication process, construction, and assembly conform to those
         specified in the design.
     Each applicant for a Parts Manufacturer Approval must make all inspections and tests
 necessary to determine--
     No part may be presented to the CAA for an inspection or test unless compliance
 with paragraphs (2) through (4) of this section has been shown for that part; and no
 change may be made to a part between the time that compliance with paragraphs (2)
 through (4) of this section is shown for that part and the time that the part is presented to
 the CAA for the inspection or test.


                                            - 15 -
Article 53
     A Parts Manufacturer Approval for a replacement or modification part is issued when:
 the CAA finds, upon examination of the design and after completing all tests and
 inspections, the design meets the applicable airworthiness requirements, and the applicant
 has established a fabrication inspection system as required at Article 51.
       A Parts Manufacturer Approval is not transferable.


Article 54
     PMA holders shall apply to CAA for ―Airworthiness Approval Tags‖ following the
 completion of procedures contained in attachment 17. The CAA will issue an
 Airworthiness Approval Tag when all procedures are satisfactorily completed on that
 PMA product.

Article 55
     The holder of a Parts Manufacturer Approval shall notify the CAA in writing within
 10 working days from the date the manufacturing facility at which the parts are
 manufactured is relocated or expanded to include additional facilities at other locations.


Article 56
      Each holder of a Parts Manufacturer Approval shall determine that each completed
 part conforms to the design data and is safe for installation on type certificated products.


Article 57
      No person may import appliances and parts for civil aviation use unless properly
 certificated. The holder of an appliance and part shall use the procedures in attachment 18
 for the validation of imported appliances and parts, unless otherwise prescribed in a treaty
 or an agreement.
      Airworthiness approval that were issued by the airworthiness authority of the
 exporting country shall be attached with the imported appliances and parts.


                                     Chapter 8
                      Technical Standard Order Authorizations
Article 58
     To produce aviation products, appliances and parts according to the airworthiness
 requirements of Technical Standard Order, the manufacturer shall submit an application
 for a Technical Standard Order Authorization (TSOA). An applicant is entitled to a TSOA
 Certificate (see Attachment 19) if its product is properly certified by CAA. The applicant


                                            - 16 -
 shall submit to CAA the following:
      1) The TSOA application form (see Attachment 20).
      2) A statement of conformance certifying that the applicant has met the
          requirements of this chapter and that the article concerned meets the applicable
          TSO that is effective on the date of application for that article. Each
          manufacturer who requests approval to deviate from any performance standard
          of a TSO shall submit to the CAA the application together with the request for
          approval to deviate, and show that the standards from which a deviation is
          requested are compensated for by factors or design features providing an
         equivalent level of safety.
      3) One copy of the technical data required in the applicable TSO.
      4) A description of its quality control system in the detail specified in Article 29 &
         30. In complying with this section, the applicant may refer to current quality
         control data filed with the CAA as part of a previous TSOA application.

Article 59
      After receiving the application and other documents required by Article 58 of this
 section to substantiate compliance with this part, and after a determination has been made
 of its ability to produce duplicate articles under this chapter, the CAA issues a TSO
 authorization (including all TSO deviations granted) to the applicant to identify the article
 with the applicable TSO marking.
      A Technical Standard Order Authorization is not transferable.


Article 60
     Each manufacturer of an article for which a TSOA has been issued shall-
      1) Manufacture the article in accordance with this chapter and the applicable TSO.
      2) Conduct all required tests, inspections and maintain a quality control system
         adequate to ensure that the article meets the requirements of paragraph 1 of this
         section and is in condition for safe operation.


Article 61
      TSOA holders shall apply to CAA for ―Airworthiness Approval Tags‖ for installation
 on the on applicable type certificated products, following the completion of procedures
 contained in attachment 17. The CAA will issue an Airworthiness Approval Tag when
 all procedures are satisfactorily completed on that TSO product.


Article 62
     The manufacturer of an article under a TSOA may make minor design changes (any


                                            - 17 -
 change other than a major change) without further approval by the CAA. In this case, the
 changed article keeps the original model number (part numbers may be used to identify
 minor changes) and the manufacturer shall forward to the CAA any revised data that are
 necessary for compliance with the requirement of this chapter.


Article 63
     Each manufacturer holding a TSOA shall, for each article manufactured under that
 authorization, keep the following records at its factory:
      1) A complete and current technical data file for each type or model article
          including design drawings and specifications;
      2) Complete and current inspection records showing that all inspections and tests
          required to ensure compliance with Article 60 paragraph (2) of this chapter have
          been properly completed and documented.
     The TSOA holder shall retain the records described in above paragraph until it no
 longer manufactures the article. When the article is no longer manufactured, copies of
 these records shall be sent to CAA.
     The manufacturer shall retain the records described in the above paragraph for a
 period of at least 2 years.


Article 64
     Each manufacturer holding a TSOA shall permanently and legibly mark his article
 with applicable TSO numbers. The CAA may withdraw the TSOA when the product
 marked as a TSO does not meet the performance standards of the applicable TSO.


Article 65
     No person may import a TSO article for civil aviation use unless properly certificated.
 The holder of the TSO article shall use the procedures in attachment 18 for the validation
 of imported TSO articles, unless otherwise prescribed in a treaty or an agreement.
      Airworthiness approval that were issued by the airworthiness authority of the
 exporting country shall be attached with the imported TSO articles.


                                   Chapter 9
                       Export Airworthiness Documentation

Article 66
      Export airworthiness approvals must be applied through the CAA and are categorized
 as follows:
      1) A Class I product is a complete aircraft, aircraft engine, or propeller, which has


                                           - 18 -
         been type certificated in accordance with the applicable regulations.
      2) A Class II product is a major component of a Class I product or any part,
         material, or appliance approved and manufactured under the (TSO) system.
      3) A Class III product is any part or component which is not a Class I or Class II
         product.


Article 67
     An aircraft owner or operator is entitled to apply for an export airworthiness approval
 when exporting aircraft or change aircraft registration to other country.
      An engine, propeller, class II product manufacturer or repair station is entitled to
 apply for an export airworthiness approval tag.
      A production approval holder is entitled to apply for an export airworthiness approval
 tag for Class III products.

Article 68
      An applicant is entitled to an export certificate of airworthiness when it meets the
 following requirements:
      1) Conform to the airworthiness requirement under Article 38.
      2) Conform to special requirement set by importing country.
      When exporting of an unassembled aircraft which has not been flight-tested or does
 not meet previous section’s requirements shall submit approved documents from the
 airworthiness authority of the importing country.
      When applying for an export certificate of airworthiness the applicant should return
 the aircraft's certificate of airworthiness to the Civil Aeronautics Administration.
      The valid period of an Export Certificate of Airworthiness is 90 days starting from
 the date of the issuance.


Article 69
      An applicant is entitled to an export airworthiness approval tag for engines,
 propellers or Class II products if that applicant conforms to the requirements of
 attachment 17.


Article 70
     An applicant is entitled to an export airworthiness approval tag for Class I, Class II
 and Class III products when:
      1) Providing documents and information to imported country airworthiness
         authorities containing the necessary information for safe operation the product.
      2) Exporting an unassembled aircraft which has not been flight-tested, provide


                                           - 19 -
         instructions for assembly and a flight test checklist to the country of
         airworthiness authority.
      3) When temporary installations are incorporated in an aircraft for the purpose of
         export delivery, the installation will be removed and the aircraft restored to the
         approved configuration upon completion of the delivery flight.


                                     Chapter 10
                               Supplementary Provisions

Article 71
     Aviation products, appliances and parts which are produced pursuant to these
 regulations must have identification plates and markings installed in accordance with
 Attachment 21.

Article 72
     Certificates issued pursuant to these regulations are valid until the expiration date
shown on the certificate.
     If a certificate issued pursuant to these regulations is lost, destroyed or damaged, the
holder shall reapply in writing for a certificate replacement or re-issuance.
     The holder of a Type Certificate or Type Validation Certificate requiring name change
must apply to the CAA for certificate replacement.


Article 73
      The applicant must show that the certificate issuance fee in the fee schedule has been
paid.
      The work expenses which are listed in the fee schedule shall be collected by the CAA
for a fund established for this specific purpose.


Article 74
     These regulations shall become effective on the date of promulgation.




                                             - 20 -
Attachment 1

                                              中華民國交通部民用航空局
                                       CIVIL AERONAUTICS ADMINISTRATION
                             MINISTRY OF TRANSPORTATION AND COMMUNICATIONS, R.O.C

             航空產品與其各項裝備及零組件使用中故障、失效或缺陷初步書面報告
                              Preliminary Report of Failures, Malfunctions, and Defects
  1.產品型號
    Product model
  2.航空器序號                               3.時間                                   4.地點
    Aircraft Serial Number                Date & Time                            Location



  5.技術標準件序號及型號代號
    Article Serial Number and Model Designation
    (When the failure, malfunction, or defect is associated with an article approved under a TSO authorization.)


  6.發動機或螺旋槳序號
    Engine or Propeller Serial Number
    (When the failure, malfunction, or defect is associated with an engine or propeller)


  7.零組件、組件或系統之名稱及件號
    Identification of the part, component, or system involved.
    (The Identification must include the part number.)


  8.故障、失效或缺陷之性質
    Nature of the failure, malfunction, or defect




  9.初步原因分析
    Preliminary Cause Analysis




  10.製造者代表簽章                                                 11.日期
     Signature of Manufacturer’s Representative                 Date




                                                    - 21 -
Attachment 2

                                            中華民國交通部民用航空局
                                     CIVIL AERONAUTICS ADMINISTRATION
                           MINISTRY OF TRANSPORTATION AND COMMUNICATIONS, R.O.C
                                      免予適用相關適航標準申請書
                         Application for Exemption from Parts of Airworthiness Standards
  1. 申請人名稱及地址
     Name and address of applicant


  2. 免予適用之適航標準及其具體條款
     Proposed requirements of airworthiness standards to be exempted




  3. 申請之原因
     Reason(s) for application




  4. 為確保具有等效安全所採取之措施及限制
     Provisions and limitations to ensure equivalent level of safety




  5. 免予適用之範圍,包括航空產品與其各項裝備及零組件、適用期限
      Scope of Exemption, including type and serial numbers of applicable aviation product, parts, and
 effective time




  6. 聲明 – 本人聲明以上陳述均屬事實
     I certify that the above statements are true.



  7. 申請人簽章                                                8.日期
     Signature of Applicant                                  Date




                                                 - 22 -
Attachment 3

                                                中華民國交通部民用航空局
                                         CIVIL AERONAUTICS ADMINISTRATION
                               MINISTRY OF TRANSPORTATION AND COMMUNICATIONS, R.O.C

                            型別檢定證、補充型別檢定證或製造許可證申請書
           APPLICATION FOR TYPE CERTIFICATE, PRODUCTION CERTIFICATE, OR SUPPLEMENTAL TYPE CERTIFICATE

  1.申請人名稱 Name of applicant                             6.申請類別 Application made for              7.檢定產品 Product Involved
                                                         □ 型別檢定證                                 □ 航空器        Aircraft
  2.地址 Address of applicant
                                                            (Type Certificate)                   □ 發動機        Engine
  3.電話 Tel                                               □ 補充型別檢定證                               □ 螺旋槳 Propeller
                                                            (Supplemental TypeCertificate)
  4.傳真 Fax                                               □ 製造許可證
                                                            (Production Certificate)
  5.電子郵件 E-mail

  8.型別檢定證 TYPE CERTIFICATE (填寫8a Complete item 8a below)
  a 產品型別名稱 Model designation(s)
  . (附上所申請之航空器、發動機、螺旋槳型別清單上產品之設計、材質、規範、構造及性能之技術資料/藍圖 All
     models listed are to be completely described in the required technical data, including drawings representing the design,
     material, specifications, construction, and performance of the aircraft, aircraft engine, propeller which is the subject of
     this application.)



  9.補充型別檢定證 SUPPLEMENTAL TYPE CERTIFICATE (填寫9a-d                                Complete items 9a-d below)
  a.修改之產品型別及製造廠 Make and model designation of product to be modified

  b.修改內容描述 Description of modification


  c.資料銷售或提供予他人                                           d.製造銷售零組件
    Will data be available for sale or release to other     Will parts be manufactured for sale?
    persons?
     □ 是Yes □ 否No                                           □ 是Yes         □否No
  10.製造許可證 PRODUCTION CERTIFICATE (填寫10a-c Complete items10a-c below)
  (與本申請書同時提交品質控制手冊或依要求因新增生產項目而修改之文件影本一份 Submit with this form, in manual
  form, one copy of quality control data or changes thereto covering new products, as required by applicable requirements.)
  a 工廠地址(若與上述地址不同)                                    b.申請 Application is for –                         製造許可證證號
  . Factory address (if different from above)         □ 首次申請 New production certificate                  P.C. No.
                                                      □ 新增製造許可項目(提供製造許可證證號)
                                                         Additions to production Certificate (Give
                                                         P.C. No.)
  c 申請人為型別檢定證或補充型別檢定證之持有人或其授權使用者                                                                        型別檢定證/補充型別
  . Applicant is holder of or a licensee under a Type Certificate or a Supplemental Type                檢定證證號
      Certificate                                                                                       T.C./S.T.C. No.
      (附上授權書並填寫證號) __________________________
      (Attach evidence of licensing agreement and give certificate number)
  11.保證 – 本人保證上述聲明屬實 I certify that the above statements are true.
  12.申請人簽章 Signature of certifying official                        13.日期 Date




                                                       - 23 -
Attachment 4

                               中華民國交通部民用航空局
                      CIVIL AERONAUTICS ADMINISTRATION
                      Ministry of Transportation and Communications
                                     Republic of China

                                          型別檢定證

                                      TYPE CERTIFICATE

                                 編號/No. CAA-TC-XXX

本型別檢定證係發給:
製造廠名稱:
產品型別/型號:

經本局對上述產品檢定後確認,其設計符合中華民國民用航空法之相關規定。該產
品型別設計、操作限制及適航要求詳列於型別檢定證數據規範表。


中華民國             年       月      日                    局      長:

This Type Certificate is issued to:
Name of Manufacturer:
Product Type/Model:


This certificate is to certify that the above aviation product has been found in
compliance with the Civil Aviation Act of the Republic of China. Details of type design,
operation limitations and associated airworthiness requirements are specified in the
type certificate data sheet.



Date of issue:     day of             ,              Director General:




                                            - 24 -
Attachment 5 Certification Flight Test

 (1) Upon showing compliance, the applicant must make all flight tests that the CAA
     finds necessary--
      (a) To determine compliance with the applicable requirements of this subchapter;
      and
      (b) For aircraft to be certificated under this rule, to determine whether there is
      reasonable assurance that the aircraft, its components, and its equipment are
      reliable and function properly.

 (2) Each applicant for an aircraft type certificate must make the tests listed in
      paragraph (1) of this section. Before making the tests the applicant must
      show—
       (a) Compliance with the applicable structural requirements of this subchapter;
       (b) Completion of necessary ground inspections and tests;
       (c) That the aircraft conforms with the type design; and
       (d) That the CAA received a flight test report from the applicant containing the
       results of his tests.

 (3) Each applicant must, if practicable, make the tests prescribed in paragraph
      (1)(b) of this section upon the aircraft that was used to show compliance with—
       (a) Paragraph (1) (a) of this section; and
       (b) For rotorcraft, the rotor drive endurance tests, as applicable.

 (4) Each applicant must show for each flight test (except in a glider or a manned
      free balloon) that adequate provision is made for the flight test crew for
      emergency egress and the use of parachutes.

 (5) Except in gliders and manned free balloons, an applicant must discontinue flight
      tests under this section until he shows that corrective action has been taken,
      whenever—
       (a) The applicant's test pilot is unable or unwilling to make any of the required
       flight tests; or
       (b) Items of noncompliance with requirements are found that may make additional
       test data meaningless or that would make further testing unduly hazardous.

 (6) The flight tests prescribed in paragraph (1)(b) of this section must include—
      (a) For aircraft incorporating turbine engines of a type not previously used in a type
      certificated aircraft, at least 300 hours of operation with a full complement of
      engines that conform to a type certificate; and
      (b) For all other aircraft, at least 150 hours of operation.




                                           - 25 -
Attachment 6 Procedure for Validating Imported Aircraft Products

 (1) Definition
      (a) Type Certificate Data Sheet (hereinafter referred to as TCDS): The supplemental
      document that accompanies with the TC that serves as one necessary essential part
      of TC. The TCDS specifies the principal design data and operation limitations of
      the authority certificated aviation product that were approved by certificated
      Authority.

      (b) Validation of Type Certificate (hereinafter referred to as VTC): The evaluation
      activity activities conducted by CAA for validating the design, manufacturing and
      performance of continuous maintenance support of the foreign certificated civil
      aviation products that prior to the importation into Taiwan.

      (c) Type Validation Certification Basis: The applicable airworthiness standards and
      environment requirements defined by CAA for type validation of civil aviation
      product. The special conditions and exemption items, if exist; also serve as part of
      certification.

 (2) Administrative procedure
      The VTC procedure is generally divided into following five stages: Pre-application
      Stage, Formal Application Stage, Document Compliance Stage, Certification Stage,
      Wrap-Up Stage.

      (a) Pre-application Stage:
         (i)    Assign the validation team numbers.
         (ii)   Notify the applicant the application is accepted being processed and
                inform him to submit the relevant certification documentation as required
                by CAA. In addition, inform the applicant of the validation process and
                negotiate with advise the applicant to settle down the validation schedule

       (b) Formal Application Stage
        (i)    Assist the applicant to get familiar with Taiwan’s validation system as
               well as the certification basis (including applicable airworthiness
               standards, environment requirements and the special requirements
               condition, if necessary) of the product under validation.
        (ii)   When necessary, conduct a preliminary evaluation, based on all
               information available, the certification capacity of both the applicant and
               the Exporting Authority.
        (iii)  As the document packages are received, check carry on the integrity and
               item for check completeness.

      (c) Document Compliance Stage
         (i)   Familiarization Meeting: The validation team members may invite
               applicant to visit CAA so as to convene a familiarization meeting. The
               functions of this meeting are to promote mutual understanding, and
               clarify technical issues arisen from the document review, and so as to
               expedite the pace of validation.

                                          - 26 -
       (ii)    Ensure if the provided documents are sufficient for document review.
       (iii)   Determine if the product under validation result of document review is
               acceptable and thereafter if an on-site evaluation is needed.

     (d) Certification Stage: Ensure that all the questions and technical issues arisen
     from document review all stages have been clarified.

     (e) Wrap-Up Stage: CAA will issue the VTC certificate for the validated product to
     the TC holder when it the result is deemed satisfactory or otherwise inform the
     applicant of the reason of rejection.

(3) A product under application can be waived from the above-mentioned procedure if it
     has been type certificated by FAA, JAA or EASA. However, the applicant still
     have to provide CAA copies of the effective TC, TCDS, special conditions,
     exemption items as well as the equivalent safety findings that were issued or agreed
     by the cognizant Authority. Additional documents may be requested by the CAA if
     deemed necessary before issuance of VTC certificate.




                                          - 27 -
Attachment 7

                              中華民國交通部民用航空局
                     CIVIL AERONAUTICS ADMINISTRATION
                     Ministry of Transportation and Communications
                                    Republic of China

                                        型別認可檢定證

                            TYPE VALIDATION CERTIFICATE

                                編號/No. CAA-VTC-XXX


本型別認可檢定證係發給:
製造廠名稱:
產品型別/型號:

經本局對上述產品審查後確認,其設計符合中華民國民用航空法之相關規定。本局
對於由________________ 發給之第________________號型別檢定證給予認可。


中華民國             年      月       日                    局      長:


This Type Validation Certificate is issued to:
Name of Manufacturer:
Product Type/Model:



This certificate is to certify that the above aviation product, as enclosed in the Type
Certificate No. ________________ issued by ________________, has been found in
compliance with the Civil Aviation Act of the Republic of China and is hereby validated.



Date of issue:     day of           ,                Director General:




                                            - 28 -
Attachment 8

                              中華民國交通部民用航空局
                     CIVIL AERONAUTICS ADMINISTRATION
                     Ministry of Transportation and Communications
                                    Republic of China

                                       補充型別檢定證

                        SUPPLEMENTAL TYPE CERTIFICATE

                               編號/No. CAA-STC-XXX

本補充型別檢定證係發給:
製造廠名稱:
產品型別/型號:

經本局對上述產品型別設計變更審查後確認,其設計變更符合中華民國民用航空法
之相關規定。



中華民國             年      月      日                    局      長:

This Supplemental Type Certificate is issued to:
Name of Manufacturer:
Product Type/Model:



This certificate is to certify that the above aviation product design change has been found
in compliance with the Civil Aviation Act of the Republic of China.




Date of issue:    day of           ,                Director General:




                                           - 29 -
Attachment 9

Each applicant must submit the following procedures to CAA for approval. Data
describing the inspection and test procedures necessary to ensure that each article produced
conforms to the type design and is in a condition for safe operation, including as
applicable-
  (1) A statement describing assigned responsibilities and delegated authority of the
      quality control organization, together with a chart indicating the functional
     relationship of the quality control organization to management and to other
     organizational components and indicating the chain of authority and responsibility
     within the quality control organization.
  (2) A description of inspection procedures for raw materials, purchased items, and parts
      and assemblies produced by manufacturers' suppliers including methods used to
      ensure acceptable quality of parts and assemblies that cannot be completely inspected
      for conformity and quality when delivered to the prime manufacturer's plant.
  (3) A description of the methods used for production inspection of individual parts and
      complete assemblies, including the identification of any special manufacturing
     processes involved, the means used to control the processes, the final test procedure
     for the complete product, and, in the case of aircraft, a copy of the manufacturer's
     production flight test produces and checkoff list.
  (4) An outline of the materials review system, including the establishment of material
      review board and the procedure for recording review board decisions and disposing
      of rejected parts.
  (5) An outline of a system for informing company inspectors of current changes in
      engineering drawings, specifications, and quality control procedures.
  (6) A list or chart showing the location and type of inspection stations.




                                             - 30 -
Attachment 10

                                             A

                              中華民國交通部民用航空局
                     CIVIL AERONAUTICS ADMINISTRATION
                     Ministry of Transportation and Communications
                                    Republic of China

                                        製造許可證

                             PRODUCTION CERTIFICATE

                                 編號/No. CAA-PC-XXX


本製造許可證係發給:
製造廠名稱:
產品型別/型號:



經本局審查確認,上述製造商之佐證資料、組織架構及製造設施符合中華民國民用
航空法之相關規定,本證所附製造許可項目單(No. )所列產品之製造,符合型
別檢定之資料,准予製造。

中華民國             年      月       日                    局      長:

This Production Certificate is issued to:
Name of Manufacturer:
Product Type/Model:


This certificate is to certify that the supporting data, organization and facilities of above
manufacturer have been found in compliance with the Civil Aviation Act of the Republic
of China. The products are manufactured in conformity with authenticated data,
including drawings, for which Type Certificates specified in the pertinent and currently
effective Production Limitation Record No.                 were issued.



Date of issue:     day of           ,                Director General:




                                            - 31 -
Attachment 10

                                           B

                             中華民國交通部民用航空局

                     CIVIL AERONAUTICS ADMINISTRATION
                     Ministry of Transportation and Communications
                                    Republic of China

                                      製造許可項目表

                        PRODUCTION LIMITATION RECORD

                               編號/No. CAA-PLR-XXX



本製造許可項目表為製造許可證 No.                                     之附件,准許此製造許可證之持
有人得製造下列航空產品。


中華民國             年      月     日                    局      長:


This Production Limitation Record serves as part of Production Certificate
No.                   .
The holder of the said Production Certificate is permitted to produce the following civil
aviation products.




Date of issue:    day of          ,                Director General:




        型別檢定證                 型號                       核准製造日期
     Type Certificate       Model            Date of Production Authorized




                                          - 32 -
Attachment 11

                                                                                                        編號
                                                                                                        Number
                         中華民國交通部民用航空局民用航空器適航證書
                                                    REPUBLIC OF CHINA

         CIVIL AERONAUTICS ADMINISTRATION, MINISTRY OF TRANSPORTATION AND COMMUNICATIONS

                                         CERTIFICATE OF AIRWORTHINESS
    國籍及登記標誌                               航空器之製造廠名稱及型別                                              航空器序號
    Nationality and Registration Marks    Manufacturer and Manufacturers’ Designation of Aircraft   Aircraft Serial Number



    類別                                                              用途
    Categories                                                      Use




    上開航空器依據民國三十三年議定之國際民用航空公約及中華民國民用航空法之規定發給本適航證書。

    該航空器在前述規定及相關之運用限制下維護及使用即屬適航。

    This Certificate of Airworthiness is issued Pursuant to the Convention on International Civil Aviation(1944), and the

    Civil Aviation Act and and related regulations of the Republic of China. The aircraft is considered to be airworthy when

    maintained and operated in accordance with the pertinent regulations and approved operating limitations.


    發 證 日 期 Date of Issue                                           局長 Director General

    本證有效期至 Valid Until                                        止

*附記事項如本證背面 SEE REVERSE SIDE FOR REMARKS




                                                           - 33 -
Attachment 12
                                                                                                            編號
                                                                                                            NO.
                        中華民國交通部民用航空局民用航空器特種適航證書
                                                  REPUBLIC OF CHINA

        CIVIL AERONAUTICS ADMINISTRATION, MINISTRY OF TRANSPORTATION AND COMMUNICATIONS

                                        SPECIAL AIRWORTHINESS CERTIFICATE
   國籍及登記標誌                                   航空器之製造廠名稱及型別                                         航空器序號
   Nationality and Registration Marks        Manufacturer and Manufacturers’ Designation of       Aircraft Serial Number
                                             Aircraft



   類別                                        飛航地區及目的 Operation Area and Purpose
   Categories




                   姓名
   使用人             Name
   Operator        地址
                   Address


   附註:          (1)民航局派                                    隨機查核。

   Remark         CAA ASI                                              is assigned for inspecting the aircraft.
                (2)詴飛人員依航空器特種適航證申請書名冊為準。

                 The flight crew must be listed on the application form.
                (3)於                      核准特種適航作業限制,為本證書之一部分。

                 Operating Limitions Dated                                  are part of this Certificate.


   發證日期 Date of Issue                                             局長 Director General

   有效期至 Valid Until                                    止




                                                        - 34 -
Attachment 13 Special flight permits

 (1) A special flight permit may be issued for an aircraft for the following purposes:
      (a) Flying the aircraft to a base where repairs, alterations, or maintenance are to be
      performed, or to a point of storage.
      (b) Delivering or exporting the aircraft.
      (c) Production flight testing new production aircraft.
      (d) Evacuating aircraft from areas of impending danger.
      (e) Conducting customer demonstration flights in new production aircraft that have
      satisfactorily completed production flight tests.
      (f)To authorize the operation of an aircraft at a weight in excess of its maximum
      certificated takeoff weight for flight beyond the normal range over water, or over
      land areas where adequate landing facilities or appropriate fuel is not available. The
      excess weight that may be authorized under this paragraph is limited to the
      additional fuel, fuel-carrying facilities, and navigation equipment necessary for the
      flight.

 (2) Experimental certificates are issued for the following purposes:
      (a) Research and development. Testing new aircraft design concepts, new aircraft
      equipment, new aircraft installations, new aircraft operating techniques, or new
      uses for aircraft.
      (b) Showing compliance with regulations. Conducting flight tests and other
      operations to show compliance with the airworthiness regulations including flights
      to show compliance for issuance of type and supplemental type certificates, flights
      to substantiate major design changes, and flights to show compliance with the
      function and reliability requirements of the regulations.
      (c) Crew training. Training of the applicant's flight crews.
      (d) Exhibition. Exhibiting the aircraft's flight capabilities, performance, or unusual
      characteristics at air shows, motion picture, television, and similar productions, and
      the maintenance of exhibition flight proficiency, including (for persons exhibiting
      aircraft) flying to and from such air shows and productions.
      (e) Air racing. Participating in air races, including (for such participants) practicing
      for such air races and flying to and from racing events.
      (f) Market surveys. Use of aircraft for purposes of conducting market surveys, sales
      demonstrations, and customer crew training.

 (3) The manufacture of aircraft, the manufacture of aircraft Engines and the person who
      has altered the design of a type certificated aircraft may apply for an experimental
      certificate, if
       (a) He has established an inspection and maintenance program for the continued
       airworthiness of the aircraft; and
       (b) He shows that the aircraft has been flown for at least 50 hours, or for at least 5
       hours if it is a type certificated aircraft that has been modified.




                                            - 35 -
Attachment 14


                         中華民國交通部民用航空局
                  CIVIL AERONAUTICS ADMINISTRATION
           MINISTRY OF TRANSPORTATION AND COMMUNICATIONS
                          REPUBLIC OF CHINA

                               零組件製造者核准書
                        PARTS MANUFACTURER APPROVAL

                               編號/No. CAA-PMA-XXX



經本局審查確認
公司名稱:
地  址:
符合中華民國民用航空法之設計及製造檢定要求,得製造下列之零組件:
    - XXXX
據此授予零組件製造者核准書。


中華民國             年     月       日                   局      長:

This is to certify that the Civil Aeronautics Administration, Republic of China, has found
that
Name of Company:
Address of Company:
meets the Civil Aviation Act requirements that applicable to the following listed parts:
          - XXXX
A Parts Manufacturer Approval is hereby granted for production of the parts as
prescribed.



Date of issue:    day of           ,               Director General:




                                          - 36 -
Attachment 15

                                               中華民國交通部民用航空局
                                        CIVIL AERONAUTICS ADMINISTRATION
                              MINISTRY OF TRANSPORTATION AND COMMUNICATIONS, R.O.C

                                        零組件製造者核准書申請書
                                 APPLICATION FOR PARTS MANUFACTURER APPROVAL


  1.申請人名稱 Name of applicant                              6.申請項目:Application Made for
                                                            新申請 New Application
  2.地址 Address of applicant                                 重大修改 Major Change
                                                            增加新零件 Add New Part
  3.電話 Tel
                                                            增加新適用機型 Add New Model Eligibility
                                                            工廠擴充或地點變更 Expansion or Change Location
  4.傳真 Fax
                                                            公司名稱變更 Change Company Name
                                                            公司組織變更 Change Organization
  5.電子郵件E-mail


  7.申請之零組件名稱
    Part Name

  8.申請之零組件編號
    Applicant’s Par Number

  9.適用之航空產品型號
    Model Eligibility

  10.擬改裝或更換之原零組件編號
     PAH’s Part Number

  11.原零組件藍圖編號及其版別(如適用)
    PAH’s Drawing Number and Revision (If
    Applicable)

  12.取得設計驗證之方法
    Method of Design Approval

  13.本申請書填具之內容正確無誤。I hereby certify that the contents of this application are correct.



  14.申請人簽章 Signature of certifying official              15.日期 Date




                                                - 37 -
Attachment 16


The requirements of fabrication inspection system for Article 51:

(1) Incoming materials used in the finished part must be as specified in the design data.

(2) Incoming materials must be properly identified if their physical and chemical properties
cannot otherwise be readily and accurately determined.

(3) Materials subject to damage and deterioration must be suitably stored and adequately
protected.

(4) Processes affecting the quality and safety of the finished product must be accomplished
in accordance with acceptable specifications.

(5) Parts in process must be inspected for conformity with the design data at points in
production where accurate determination can be made. Statistical quality control
procedures may be employed where it is shown that a satisfactory level of quality will be
maintained for the particular part involved.

(6) Current design drawings must be readily available to manufacturing and inspection
personnel, and used when necessary.

(7) Major changes to the basic design must be adequately controlled and approved before
being incorporated in the finished part.

(8) Rejected materials and components must be segregated and identified in such a manner
as to preclude their use in the finished part.

(9) Inspection records must be maintained, identified with the completed part, where
practicable, and retained in the manufacturer's file for a period of at least 2 years after the
part has been completed.




                                              - 38 -
Attachment 17 Airworthiness Approval Procedure

(1)Application
   (a)The applicant and application items for airworthiness approval including :
      (i)The holder of Production Certificate for aircraft engines, propellers that apply for
         the airworthiness approval of its products.
      (ii)The holder of PMA and TSOA intended to supply its products to be
         installed in the type certified aircraft shall apply for the airworthiness
         approval of its products.

   (b)The manufacturer or repair station for aircraft engines, propellers, the
     manufacturer for Category II products and the PAH for Category III products
     can apply the for the export airworthiness approval of its products.

   (c)The applicant applies for the domestic and export airworthiness approval shall
     complete the application form thoroughly (see attached form )and submit the
     statement document to show that the product conform to the approved design data
     and is in a condition for safe operation .

   (d)If the application package is not correct or complete. The CAA will notify the
     applicant to submit the supplemental data.

(2)Airworthiness Inspection
The inspector will visit the PAH’s facility (and the suppliers, if necessary) to perform the
airworthiness inspection. The inspection will consist of the following to ensure the
product is:
    (a)In conformity to the approved the design data,
    (b)In a condition for safe operation,
    (c)In compliance with the marking requirements of the ―Regulations Governing the
     Certification for Aviations Products, Appliances and Parts‖ and
   (d)For the export approval, in compliance with requirements (if any) of the importing
     country.

(3)Approval
   (a)After the review, the CAA will issue the Airworthiness Approval Tag for the
     domestic airworthiness approval or export approval.
   (b)The holder of Airworthiness Approval Tag for the domestic airworthiness approval
     or export approval will submit the original Airworthiness Approval Tag and the
     products to the buyer. The holder will keep the copy of the singed Airworthiness
     Approval Tag for at lest two years.

(4)Domestic Airworthiness Approval and Export Approval of the

                                             - 39 -
Newly-Overhauled or Used Product
  (a)An export approval for a newly overhauled or used product may not be issued unless
    the country of import has provided a written confirmation indicating that it will
    accept the product. The applicant also has to fulfill the requirement of paragraph(c).
   (b)If the applicant applies for the export airworthiness approval of the used product, a
     written statement from the importing country's CAA, submitted by the applicant, is
     required to acknowledge the status of the products being exported and that such an
     export approval is acceptable.
   (c)The applicant must show that the products conform to the approved design data.




                                           - 40 -
                                                             適航掛籤申請書
                                                 Application Form for Airworthiness Approval Tag

                                                 第一部分:供申請人申請掛籤時使用
                                                   Part I: Application for the following approval:
 □ 適航掛籤 Airworthiness Approval                              □ 出口用適航掛籤 Export Airworthiness Approval
1.申請人名稱 Name of Applicant                                     2.申請人地址 Address of Applicant

3.買受人 Purchaser                                                4.進口國 Country of Destination
                                                               (申請出口用適航掛籤時填寫 for export approval only)
5.本產品/零組件適用於下列型號之產品上:
   Product(s)/part(s) is (are) eligible for installation on the following make and model of product:


6.本產品係:         □ 新製造 New                 □ 新翻修 Newly Overhauled
7.產品內容 The product(s) is (are) described:
  □ 如發貨單或出貨資料 On the attached invoice or packing sheet, by name, part number and quantity
  □ 產品名稱/件號/數量如下 Below by name, part number, and quantity:
  產品型號或名稱                           件號             序號或批號                                                                 數量
     Model or Name                         Part No.                     Serial No. or Batch No.                         Quantity


8.是否符合適用之進口國特殊要求 (申請出口用適航掛籤時填寫, for export approval only)
   Have applicable special requirements of the importing country been complied with?
   □ 是 YES
   □ 否 NO (勾選此項者,應於備註欄詳註原因 Explain in item 11 "Remarks")
9.是否符合適用之適航法規要求
   Have applicable airworthiness requirements been complied with?
   □ 是 YES
  □ 否 NO (勾選此項者,應於備註欄詳註原因 Explain in item 11 "Remarks")
10.說明使產品免受侵蝕或損壞之保存及包裝方法 (列出規範或方法名稱)
    Preservation and packaging methods used to protect parts against corrosion and damage (List Spec. or Title)

上述方法之有效期間 Effective duration of above methods:

11.備註 Remarks


12.出口者聲明:本申請表及有關附件所填各項均屬實。除第 11 項備註欄所列原因外,本產品為適航並符合
   經核准之設計資料,且可安全使用。
   EXPORTER’S CERTIFICATION – I certify that the foregoing statements are true and that the parts described herein are airworthy, conform
   to CAA approved design data, and are in condition for safe operation except as may be noted in items 11 "Remarks".
13.申請人簽名 Signature                      14.職稱 Title                                          15.申請日期 Date

                                                         第二部分:供民航局使用
                                                Part II: APPROVAL (FOR CAA USE ONLY)
16.針對申請之產品共發給 □適航掛籤 □出口用適航掛籤                                                                      份。
     Quantity of approval tags, CAA Form 21-01, issued for the product(s)/part(s) described in this form.
17.除第 11 項備註欄所列原因外,本申請表所列之產品為適航,並符合適當之要求。
   It is considered that the product(s)/part(s) described in this form is (are) airworthy and conform(s) to pertinent requirements except as noted
   in item 11 "Remarks".
18.簽名 Signature                             19.證號 Authorization No.                                20.核准日期 Date




                                                                 - 41 -
Attachment 18 Appliance Design Validation Procedure


(1) Appliance imported to use on the type certificated product, the appliances manufacturer
    shall submit the following document, together with an Application Letter, to the CAA
    for the application of the design validation unless that appliance already validated by
    CAA together under product type validation:

  (a) Certification Plan: To prescribe the certification overview and list all the applicable
      airworthiness requirements and industrial standards, including the ―Compliance
       Checklist‖ to elaborate the means of compliance.

  (b) The Certificate/Approval issued by the Civil Aviation Authority of the exporting
      country to demonstrate the eligible design and production approval.

  (c) The test reports or analyses to demonstrate the compliance with the applicable
      requirements and standards.

  (d) Instructions for Continued Airworthiness: Components Maintenance Manual (CMM)
      and Illustrated Parts Catalog (IPC) etc.

  (e) The relevant approval document showing the validity of the installation of the
      concerning appliances; and other document deemed necessary.

  (f) Statement of Conformance: A statement to certify that all the applicable
      requirements have been complied with and signed by the authorized personnel.

(2) Manufacturer submitted document shall comply CAA requirement. Manufacturer shall
    submit supporting document for reviewing when notify by CAA.

(3) An manufacturer is entitled to a Appliance Design Validation Letter, if the CAA finds,
   after examination of the submitted document compliance with the CAA requirements.




                                            - 42 -
Attachment 19


                          中華民國交通部民用航空局
                  CIVIL AERONAUTICS ADMINISTRATION
                 Ministry of Transportation and Communications
                                Republic of China

                                 技術標準件核准書

            TECHNICAL STANDARD ORDER AUTHOR IZATION

                            編 號 /No. CAA- TSOA -XXXX

經本局審查確認
公司名稱:
地  址:

符合頒布之技術標準規定之設計及製造檢定要求,得製造下列技術標準件:
   -XXXX
據此授予技術標準件核准書。

註記:

中華民國             年     月       日                   局      長:

This is to certify that the Civil Aeronautics Administration, Republic of China, has found
that the
Name of Company:
Address of Company:
meets the Civil Aviation Act requirements applicable to the following listed TSO items:
        -XXXX
A Technical Standard Order Authorization is hereby granted for production of the TSO
items as prescribed.


Remark:


Date of issue:     day of          ,               Director General:




                                          - 43 -
Attachment 20

                                              中華民國交通部民用航空局
                                        CIVIL AERONAUTICS ADMINISTRATION
                              MINISTRY OF TRANSPORTATION AND COMMUNICATIONS, R.O.C

                                         技術標準件核准書申請書
                         APPLICATION FOR TECHNICAL STANDARD ORDER AUTHORIZATION

  1.申請人名稱 Name of applicant                              6.申請項目:Application Made for

                                                            新申請 New Application

  2.地址 Address of applicant                                 重大修改 Major Change

                                                            工廠擴充或地點變更 Expansion or Change Location

  3.電話 Tel                                                  公司名稱變更 Change Company Name

                                                            公司組織變更 Change Organization

  4.傳真 Fax



  5.電子郵件 E-mail



  7.申請之技術標準件名稱
    TSO Appliance

  8.申請適用之《技術標準
    規定》編號及名稱
    TSO Number

  9.本申請書填具之內容正確無誤 I hereby certify that the contents of this application are correct.



  10.申請人簽章 Signature of certifying official              11.日期 Date




                                                - 44 -
Attachment 21 Identification plate and marking requirements


(1) Any product being manufactured in accordance with these regulations must be
  identified by means of a fireproof plate and marking, that will not likely be defaced, and
  contain legible identification information, including the approved type certificate number,
  builder's serial number, and manufacturing date, and shall comply with the following
  requirements-

   (a) For aircraft, the identification plate must be secured adjacent to main (or aft)
       entrance door, or at a prominent location on the fuselage surface near the tail
       surfaces.
   (b) For aircraft engine, the identification plate must be affixed to the engine at an
       accessible location in such a manner that it will not likely be defaced or lost during
       normal service.
   (c) For propeller, the marking shall be placed on a non-critical surface of blades and
       hubs.

(2) For critical part installed on the aircraft, for which the replacement time and inspection
   interval are specified, the part number and serial number must be marked on the part.

(3) The parts manufactured according to a Parts Manufacturer Approval as prescribed in
    the Chapter 7 of this procedure shall permanently and legibly marked with the
    following information-

   (a) The CAA-PMA marking;
   (b) The name and address of the manufacturer;
   (c) The name, type, part number and series number of the parts;
   (d) Date of manufacturing, the type and model of the aviation product to be installed
       on.
(4) For the parts that is not able to be marked with above information, due to the size of the
  parts or otherwise, may be marked on an affixed tag on its package.

(5) The TSO Article manufactured according to the Chapter 8 of this procedure shall
  permanently and legibly mark each article to which this section applies with the
  following information-

   (a) The name and address of the manufacturer;
   (b) The name, type, part number, or model designation of the article;
   (c) The serial number and the date of manufacture of the article;


                                             - 45 -
(d) The CAA approved TSOA marking and the applicable TSO number.




                                   - 46 -
Table. Fees for certification of Aviation Products, Appliances and parts

Descriptions to Items for certification of Aviation Products, Appliances and parts
    (1) Foreign applicants who apply for issuance of a certificate in ROC by the
        Regulations herein shall pay certificate issuance fee listed in fee schedule 1 and
        certification application fee listed in Fee schedule 2. If CAA deems it necessary to
        assign inspectors to foreign country to conduct on-site evaluation during
        certification, foreign applicants shall pay additional inspection manpower fee
        listed in Fee schedule 2 and work expense in accordance with Fee schedule 3.


     (2) Native applicants
        (a) Apply for issuance of a certificate in ROC by the Regulations herein shall pay
        certificate issuance fee listed in Fee schedule 1.
        (b) Apply for sending a CAA inspector(s) to issue a certificate in a foreign country
        shall pay additional work expense in accordance with Fee schedule 3.



Fee schedule 1. Certificate issuance fees
                                                                               Certificate
                                 Certificate
                                                                              Issuance Fee
     Type Certificate                                                          NT$ 6,000
     Validation of Type Certificate                                             NT$ 4,000
     Type certificate amendment                                                 NT$ 2,000
     Supplemental Type Certificate                                              NT$ 2,000
     Production Certificate                                                     NT$ 6,000
     Parts Manufacturer Approval                                                NT$ 2,000
     Technical Standard Order Authorization                                     NT$ 3,000
     Certificate of Airworthiness (For aircraft with maximum takeoff
                                                                                NT$ 6,000
     weight exceeds 5,700 Kilograms)
     Certificate of Airworthiness (For aircraft with maximum takeoff
                                                                                NT$ 3,000
     weight equal or less than 5,700 Kilograms)

Fee schedule 2. Certification application and Inspection manpower fees
                  Item                            Fee                  Remark
                                                                  The foreign applicant must pay
                                                                  the certification application fee
     Certification application fee                                when he applies for the
                                               USD $1,500         validation of type certificate for
     for Aviation Products
                                                                  the imported aircraft, engine,
                                                                  and propeller.
                                                                  The foreign applicant must pay
     Certification application fee                                the certification application fee
     for parts, components, or TSO             USD $150           when he applies for the
     articles                                                     validation for the imported
                                                                  parts, components, or TSO

                                            - 47 -
                                                                    articles.
                                                                    This fee shall be collected
                                                                    based on the number of
      Inspection manpower fee              USD $245 per day         inspectors and total days
                                                                    traveling abroad for the
                                                                    certification functions.


Fee schedule 3. Work Expense


This work expense shall be collected based on number of man-days involved in the
certification work and the total days required for that trip. It is determined according to the
following formula:


Work Expense=【Basic work expense(A)+Daily work expense(B)×Total days for the
trip】×Total number of inspectors assigned for the certification work.

             Working Area               Basic work expense(A)        Daily work expense(B)
      Northern Asia Area                      USD $600                     USD $316
      Mid-Asia Area                          USD $1,777                    USD $289
      Southern Asia Area                      USD $700                     USD $199
      Europe, Australia Area                 USD $1,833                    USD $167
      Northern America Area                  USD $1,300                    USD $218
      Southern America Area                  USD $2,700                    USD $238

       Remarks: If the amount of the basic work expense (A) is not enough to cover the
       expense for the inspector to carry out the on-site certification due to transportation
       cost, the work expense will be charged according to the actual cost generated from
       conducting the on-site certification.




                                             - 48 -

								
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