Key Benefits:
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(2) Any fraudulent or non-fraudulent entry in any record or report that is required to be kept, made, or used to show compliance with any resulting from the issuance or the exercise of the privileges of any. certificate or approval issued issued under this part;
(3) Any reproduction for the fraudulent purpose of any certificate or approval issued under this part;
(4) Any alteration of any certificate or approval issued under this part.
(b) The commission by any person of an act prohibited under paragraph (a) of this section is a basis for suspending or revoking any certificate or approval issued issued under this part and held by that person.
21.3 Reporting of failures, malfunctions, and defects.
(a) Except as provided in paragraph (d) of this section, the holder of a Type Certificate (including a Supplemental Type Certificate), a Parts Manufacturer Approval (PMA), or a TSO authorization, or the licensee of a Type Certificate shall report any failure, malfunction, or defect in any product, part, process, or article manufactured by it. that it determines that it has resulted in any of the occurrences listed in paragraph (c) of this section.
(b) The holder of a Type Certificate (including a Supplemental Type Certificate), a Parts Manufacturer Approval (PMA), or a TSO authorization, or the licensee of a Type of Certificate shall report any defect in any product, part, or article manufactured by it that has left its quality control system and that it determines could result in any of the occurrences listed in paragraph (c) of this section.
(c) The following occurrences must be reported as provided in paragraphs (a) and (b) of this section:
(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 components.
(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 or rotorcraft hub or blade structural failure.
(6) Flammable fluid leakage in areas where an ignition source became available.
(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, understrength, corrosion, etc.).
(9) Any abnormal vibration or buffeting caused by a structural or system malfunction, defect, or failure.
(10) An engine failure.
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(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 complete loss of more than one electrical power generating system or hydraulic power system during a given operation of the aircraft.
(13) A failure or malfunction of more than one attitude, airspeed, or altitude instrument during a given operation of the aircraft.
(d) The requirements of paragraph (a) of this section do not apply to-
(1) Failures, malfunctions, or defects that the holder of a Type Certificate (including a Supplemental Type Certificate), Parts Manufacturer Approval (PMA), or TSO authorization, or the licensee of a Type Certificate-
(i) Determines were caused by improper use. maintenance, or improper usage;
(ii) Knows were reported to the DGCA by another person under the renewable regulations; or
(iii) Has already reported under the requirements of the Reporting of Accidents and Overdue Aircraft.
(2) Failures, malfunctions, or defects in products, parts, or articles manufactured by a foreign Under Sec. 21.29 or Sec. 21.621, or exported to the Republic of Indonesia under Sec. 21.502.
(e) Each report required by this section-
(1) Shall be made to the DGCA within 24 hours after it has determined that the failure, malfunction, or defect required to be reported. However, a report that is due on a Sunday may be delivered on the following Monday and one that is due on a holiday may be delivered on the next workday;
(2) Shall be expected in a manner and form acceptable to the DGCA and by the most expeditious method available; and
(3) Shall include as much of the following information as is available and saved:
(i) Aircraft serial number.
(ii) When the failure, malfunction, or defect is associated with an article approved under a TSO authorization, the article serial number and model designation, as appropriate.
(iii) When the failure, malfunction, or defect is associated with an engine or propeller, the engine or propeller serial number, as appropriate.
(iv) Product model.
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(v) Identification of the part, component, or system involved. The identification must include the part number.
(vi) Nature of the failure, malfunction, or defect.
(f) Whenever the investigation of an accident or service difficulty report shows that an article manufactured under a TSO authorization is unsafe because of a manufacturing or design defect, the manufacturer shall, upon request of the DGCA, report to the DGCA 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 the DGCA.
21.4 ETOPS reporting requirements.
(a) Early ETOPS: reporting, tracking, and resolving problems. The holder of a type certificate for an airplane-engine combination approved using the Early ETOPS method specified in CASR part 25, Appendix K, must use a system for reporting, tracking, and resolving each problem resulting in one of the occurrences. The specified in paragraph (a) (6) of this section.
(1) The system must identify how the type certificate holder will promptly identify problems, report them to the DGCA, and propose a solution to the DGCA to resolve each problem. A proposed solution must be based on-
(i) A change in the airplane or engine type design;
(ii) A change in a manufacturing process;
(iii) A change in an operating or maintenance procedure; or
(iv) Any other solution Acceptable to the DGCA.
(2) For an airplane with more than two engines, the system must be in place for the first 250,000 world fleet engine-hours for the approved airplane-engine combination.
(3) For two-engine airplanes, the system must beson that allows the production of a product or article in accordance with its approved design and approved quality system, and can take the form of a production certificate, a PMA, or a TSO authorization;
(7) State of Design means the country or jurisdiction having regulatory authority over the organization responsible for the organization responsible for the design and continued airworthiness of a civil aeronautical product or article;
(8) State of Manufacture means the country or jurisdiction having regulatory authority over the organization responsible for the production and airworthiness of a civil aeronautical product or article.
21.2 Falsification of Application, reports, or records.
(a) No person shall make or cause to be made.
(1) Any fraudulent or false statement on any application for a certificate or approval under this part;
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(i) The world fleet 12-month rolling average IFSD rate is at or below the rate required by paragraph (b) (2) of this section; and
(ii) The DGCA determines that the rate is stable.
(4) For an airplane-engine combination that is a The Derivative of an airplane-engine combination previously approved for ETOPS, the system need only address those problems specified in the following table, provided the type certificate airworthiness provisions not complied with are compensated for by factors that provide an equivalent level of safety; and
(2) For an aircraft, that no feature or characteristic makes it unsafe for the category in which certification is requested.
21.23 [Reserved]
21.24 Issuance of type certificate: primary category aircraft.
(a) The body is entitled to a type certificate for an aircraft in the primary category if-
(1) The aircraft-
(i) Is unpowered; is an airplane powered by a single, naturally aspirat for example, for example, for example, for example, for example, owner or operator's product or operator's product; or
(6) Fabricated by an appropriately rated certificate holder with a quality system, and consumed in the repair or alteration of a product or article in accordance with CASR Part 43.
(b) Except as provided in paragraphs (a) (1) through (a) (2) of this section, a person who performs a replacement or modification article for sale may not represent that part as suitable for installation on a type-certificated product.
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SUBPART B TYPE CERTIFICATES
21.11 Applicability.
This subpart prescribes-
(a) Procedural requirements for the issue of type certificates for aircraft, aircraft engines, and propellers; and
(b) Rules governing the holders of those certificates.
21.13 Eligibility.
Any interested person as prescribes in Sub Part J Design Organization Approval (DOA) may apply for a type certificate.
21.15 Application for type certificate.
(a) An application for a type certificate is Made on a form and in a manner.
(b) An application for an aircraft type certificate must be accompanied by a three view drawing of that aircraft and available preliminary basic data.
(c) 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.
21.16 Special Conditions.
If the DGCA finds that the airworthiness regulations do not contain adequate or more appropriate safety standards for an aircraft, aircraft engine, or propeller because of a novel or unusual design feature of the aircraft, aircraft engine or propeller, he prescribes special conditions and amendments thereto for the product. The special conditions are issued in accordance with CASR Part 11 and contain such safety standards for the aircraft, aircraft engine or propeller as the DGCA finds necessary to establish a level of safety equivalent to that established in the Regulations.
21.17 Designation of Applicable Regulations.
(a) Except as provided in CASR Part 23 Sec. 23.2, CASR Part 25 Sec. 25.2, CASR Part 27 Sec. 27.2, CASR Part 29 Sec 29.2, Part 34, and Part 36, an Act for a type certificate must show that the aircraft, aircraft engine, or propeller concerned meets-
(1) The storage requirements of the airworthiness standard that are effective on the date of application for that certificate unless-
(i) Otherwise specified by the DGCA; or
(ii) Compliance with later effective amendments is elected or required under this section; and
(2) Any special conditions prescribed by the DGCA.
(b) For special classes of aircraft, including the engines and propellers installed thereon (e.g., gliders, airships, and other nonconventional aircraft), for which airworthiness standards have not been issued, the requirements of will. be the portions of those other airworthiness requirements contained in
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CASR PART 23, Part 25, Part 27, Part 29, Part 31, Part 31, and Part 33 found by the DGCA to be appropriate for the aircraft and corrected to a specific type design, or such airworthiness criteria as the DGCA may find provide an equivalent level of safety to those parts.
(c) An application for type certification of a transport category aircraft is effective for 5 years and an application for any other type certificate is effective for 3 years, unless an example shows at the time of application that his product requires a longer period of time for design, development, and testing, and the DGCA approves a longer period.
(d) In a case where a type certificate has not been issued, or it is clear that a type certificate will not be issued, within the time limit established under paragraph (c) of this section, the May-
(1) File a new application for a type certificate and comply with all the provisions of paragraph (a) of this section apply to an original application; or
(2) File for an extension of the original application and comply with the renewable airworthiness requirements that were effective on a date, to be selected by the note, not earlier than the date which precedes the date of issue of the type certificate by the time limit established under paragraph (c) of this section for the original application.
(e) If an individual has been able to comply with an amendment.) to the airworthiness standard that is effective after the filing of the application for a type certificate, he must also comply with any other amendment that the DGCA finds is directly related.
21.19 Changes requiring a new type certificate.
Any person who proposes to change a product must make a new application for a type certificate if the DGCA finds that the proposed change in design, configuration, power, power limitations (engines), speed limitations (engines), or weight is so extensive that a substantially complete investigation of compliance with the process Regulations are required.
21.20 Compliance with renewable requirements.
The law for a type certificate, including an amended or supplemental type certificate, must-
(a) Show compliance with all shares. * * * * * * * * * * * * * * * * * * * * * * * * * * * * *
(b) Provide a certifying statement that the event has complied with the requirements of the requirements.
21.21 Issue of Type Certificate: Normal, Utility, Acrobatic, Commuter, and Transport Category Aircraft; Special Classes of Aircraft; Aircraft Engines; Propellers.
An ordinary is entitled to a type certificate for an aircraft in the normal, utility, acrobatic, commuter, or transport category, special class of aircraft, or an aircraft engine or propeller, if-
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(a) [To be determined]
(b) The subject submits the type design, test reports, and computations necessary to show that the product to be certificated meets the air airworthiness, aircraft noise, fuel venting, and exhaust emission requirements and any special conditions prescribed by the DGCA, and the DGCA finds-
(1) Upon examination of the type design, and after completion all tests and inspections, that the type design and the product meet the air noise, fuel venting, and emissions requirements, and further finds that they meet the the airworthiness requirements or that anyation responsible for final assembly of the airplane.
21.8 Approval of articles.
If an article is required to be approved under the regulation of regulation, it is may be approved-
(a) Under a PMA;
(b) Under a TSO;
(c) In conjunction with type certification procedures for a product; or
(d) In any other manner approved by the DGCA.
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21.9 Replacement and modi ed engine witha 61-knot or less Vso stall speed as defined in CASR 23.49; or is a rotorcraft with a 6-pound per square foot main rotordisc loading limitation, under sea level standard day conditions;
(ii) Weighs not more than 2,700 pounds; or, for seaplanes, not more than 3,375 pounds;
(iii) Has a maximum seating capacity of not more than four persons, occurs later, and later make those instructions. available to any other person required by this pertinent CASRs to comply with any of the terms of these instructions. In addition, changes to the Instructions for Continued Airworthiness shall be made available to any person required by this pertinent CASRs to comply with any of those instructions.
(c) To designate commercial parts, the holder of a design approval, in a manner acceptable to the DGCA, must submit:
(1) A Commercial Parts List;
(2) Data for each part on the List showing that:
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(1) Compliance with the renewable requirements of the IBM CASR;
(2) Completion of necessary ground inspections and tests;
(3) That the aircraft conforms with the type design; and
(4) That the DGCA received a flight test report from the perp (signed, in the case of aircraft to be certificated under CASR Part 25, by the air pilot) containing the results of his tests.
(b) Upon showing compliance with paragraph (a) of this section, the necessary must make all flight tests that the DGCA finds necessary-
(1) To determine compliance with the renewable requirements of the IBM CASR; and
(2) For aircraft to be certificated under the replacement CASR, except gliders and except airplanes of 6,000 lbs. or less maximum certificated weight that are to be certificated under CASR Part 23 to determine whether there is reasonable assurance that the aircraft, its components, and its equipment are reliable and function properly.
(c) Each of the must, if practicable, make the tests prescribed in paragraph (b) (b) (2) of this section upon the aircraft that was used to show compliance with-
(1) Paragraph (b) (1) of this section; and
(2) For rotorcraft, the rotor drive endurance tests prescribed in CASR Part 27 Sec. 29.923 or CASR Part 29 Sec.
(d) Each of the must be shown for each Flight test that was made for the flight test crew for emergency egress and the use of parachutes.
(e) An important must be made flight tests under this section until he shows that corrective action has been taken, whenever-
(1) The official test pilot is unable or unwilling to make any of the required flight tests; or
(2) Items of noncompliance with requirements are found that may make additional test data meaningless or that would make further testing the download.
(f) The flight tests prescribed in paragraph (b) (2) of this section must include-
(1) 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
(2) For all other types Aircraft, at least 150 hours of operation.
21.37 Flight Test Pilot.
Each one for a normal, utility, acrobatic, commuter, or transport category aircraft type certificate must provide a person holding an appropriate pilot certificate to make the flight tests required by this part.
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21.39 Flight Test Instrument Calibration and Correction Report.
(a) Each is a normal for a normal, utility, acrobatic, commuter, or transport category aircraft type certificate must submit a report to the DGCA showing the computations and tests required in connection with the calibration of instruments used for test purposes and in the correction of test results to standard atmospheric conditions.
(b) Each additional must allow the DGCA to conduct any flight tests that he finds necessary to check the accuracy of the report behind paragraph (a) of this section.
21.41 Type certificate.
Each type certificate is considered to include the type design, the operating limitations, the certificate data sheet, the database regulations with which the DGCA records compliance, and any other conditions or limitations prescribed for the product.
21.43 Location of Manufacturing Facilities.
Except as provided in Sec. 21.29, the DGCA does not issue a type certificate if the manufacturing facilities for the product are located outside of the Republic of Indonesia, unless the DGCA finds that the location of the manufacturer's facilities places no undue burden on the DGCA in administering the airworthiness requirements.
21.45 Privileges.
The holder or licensee of a type certificate for a product may-
(a) In the case of aircraft, upon compliance with Secs. 21.173 through 21.189, obtain airworthiness certificates;
(b) In the case of aircraft engines or propellers, obtain approval for installation on certified aircraft;
(c) In the case of aircraft engines or propellers, or in the case of aircraft engines or propellers, case of any product, upon compliance with sub part G of this part, obtain a production certificate for the type certificated product;
(d) Obtain approval of replacement parts for that product.
21.47 Transferability.
A type certificate may be transferred to or made available to third persons by licensing agreements. Each grantor shall, within 30 days after the transfer of a certificate or execution or termination of a licensing agreement, notify in writing the DGCA. The notification must state the name and address of the transferee or licensee, date of the transaction, and in the case of a licensing agreement, the extent of authority granted the licensee.
21.49 Availability.
The holder of a type certificate shall make the certificate available for examination upon the request of the DGCA or Investigation Committee.
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21.50 Instructions for Continued Airworthiness and Manufacturer's Maintenance Manuals Having Airworthiness Limitations Sections.
(a) The holder of a type certificate for a rotorcraft for which a Rotorcraft Maintenance Manual containing an "Airworthiness Limitations" section has been issued under CASR Part 27 Sec. 27.1529 (a) (2) or CASR Part 29 Sec. 29.1529 (a) (2), and who obtains approval of changes to any replacement time, inspection interval, or related procedures in that section of the manual, shall make those changes available upon request to any operator of the same type of rotorcraft.
(b) The holder of a design approval, including either the type certificate or supplemental type certificate for an aircraft, aircraft engine, or propeller, shall furnish at least one set of complete Instructions for Continued Airworthiness, prepared in accordance with CASR Part 23 Sec. 23.1529, CASR Part 25 Sec. 25.1529, CASR Part 27 Sec. 27.1529, CASR Part 29 Sec. 29.1529, CASR Part 33 Sec. 33.4, or CASR Part 35 Sec. 35.4, or as Specified in the air airworthiness criteria for special classes of aircraft defined in Sec. 21.17 (b), U.s. (1), to the owner of each type of aircraft, aircraft engine, or propeller upon its delivery, or upon issuance of the first standard airworthiness certificate for the affected aircraft, whichever h paragraphs (b) (2) through (b) (4) of this section has been shown for that aircraft, aircraft engine, propeller, or part thereof; and
(2) (2) No change may be made to an aircraft, aircraft engine, propeller, or part between the time that compliance with paragraphs (b) (2) through (b) (4) of this section is shown ♪ For that aircraft, aircraft engine, propeller, or part ♪ ♪ and the time that it is presented to the ♪ DGCA for test.
(b) Each case must make all inspections and tests necessary to determine-
(1) Compliance with the renew er:always">
2015, No. 899 28
operating procedures, if his presence on the perform his duties and he has been authorized in writing by a responsible supervisor, listed in the Operations Manual as having that authority; and
(vi) A technical representative of the manufacturer of the aircraft or its components whose duties are directly related to the in-flight monitoring of aircraft equipment or operating procedures or operating procedures, if his presence on the flight deck is necessary to perform his duties, and he has been authorized in wriection; and
(ii) Operating in and out of airports where takeoffs or approaches over The populated areas are necessary. No person may operate that aircraft except in compliance with the approved procedures.
(7) Each person operating a provisionally certificated civil aircraft shall ensure that each flight crewmember is properly certificated and has adequate. knowledge of, and familiarity with, the aircraft and procedures to be used by that crewmember.
(8) Each person operating a provisionally certificated civil aircraft shall maintain it as required by renewable regulations and as may be specially created By the DGCA.
(9) Whenever the manufacturer, or the DGCA, determines that a change in design, construction, or operation is necessary to ensure safe operation, no person may operate a provisionally certificated civil aircraft until that change has been made And approved. Section 21.99 applies to operations under this section.
(10) Each person operating a provisionally certificated civil aircraft-
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(i) May carry in that aircraft only persons who have a proper interest in the operations allowed by this section or who are authorized to be authorized by both the manufacturer and the DGCA; and
(ii) Shall advise each person carried that the aircraft is provisionally certificated.
(11) The DGCA may prescribe additional limitations or procedures that the DGCA considers necessary, including limitations on the number of persons who may be carried in the aircraft.
(12) Flight test areas. No person may flight test an aircraft except over open water, or sparsely populated areas, having light air traffic.
21.83 Requirements for Issue and Amendment of Class II Provisional Type Certificates.
(a) An equal who Related types within the Republic of Indonesia is entitled to the issue or amendment of a Class II provisional type certificate if he shows compliance with this section and the DGCA finds that there is no feature, characteristic, or condition that would make the aircraft unsafe when operated in accordance with the limitations in paragraph (h) and (k) of this section, and Sec. 21.81 (h).
(b) An example who performs aircraft in a country which the Republic of Indonesia accepts of those aircraft for importation is entitled to the issue or amendment of a Class II provisional type certificate if the country in which the aircraft was manufactured certifies that the management has shown compliance with this section, that the aircraft meets the requirements of paragraph (f) of this section and that there is no feature, characteristic, or condition that would make the aircraft unsafe when operated in accordance with the limitations in paragraph (h) and (k) of this section, and Sec. 21.81 (h).
(c) The information must apply for a type certificate, in the transport category, for the aircraft.
(d) The information must hold a Republic of Indonesia type certificate for at least one other aircraft in the same transport category as the subject aircraft.
(e) The DGCA's official flight test program or the flight test program conducted by the authorities of the country in which the aircraft was manufactured, with respect to the issue of a type certificate for that aircraft, must be in progress.
(f) The heart or, in the case of a foreign manufactured aircraft, the country in which the aircraft was manufactured, must certify that-
(1) The aircraft has been designed and constructed in accordance with the airworthiness requirements for the issue of the type certificate applied for;
(2) The The aircraft has been operated safely under the appropriate operating limitations of the air airworthiness
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(g) The information must submit a report showing that the aircraft has been flown in all maneuvers necessary to show compliance with the flight requirements for the issue of the type certificate and to establish that the aircraft can be operated safely in accordance with the limitations of the air airworthiness.
(h) The heart must prepare a provisional aircraft flight manual containing all limitations required for the issue of the type certificate applied for, including limitations on weights, speeds, flight maneuvers, loading, and operation of controls and equipment unless, for each limitation not so established, appropriate operating capabilities are established for the aircraft.
(i) The data must establish an inspection and maintenance program for the continued Airworthiness of the aircraft.
(j) The heart must show that a prototype aircraft has been flown for at least 100 hours. In the case of an amendment to a provisional type certificate, the DGCA may reduce the number of required flight hours.
(k) Provisionally certificated air carrier airplane: Operating limitations. In addition to the limitations in Sec. 21.81 (h), the following limitations apply to the operation of provisionally certificated airplane by air carriers:
(1) In addition to crewmembers, each air carrier may carry on such an airplane only those persons who are listed in paragraph (k) (3) of this section or who are authorized to be authorized by both the air carrier and the DGCA.
(2) Each air carrier shall keep a log of each flight conducted under this section and shall keep accurate and complete records of each inspection made and all maintenance performed on the airplane. The air carrier shall make the log and records made under this section available to the manufacturer and the DGCA.
(3) Admission to flight deck. No person may admit any person to the flight deck unless there is a seat available for his use in the passenger compartment, except-
(i) A DGCA air carrier inspector or an authorized representative of the DGCA or Investigation Committee who is checking or observing flight operations;
(ii) An air traffic controller who is authorized by the DGCA to observe ATC procedures;
(iii) A certificated airman employed by the certificate holder whose duties require an airman certificate;
(iv) A certificated airman employed by another certificate holder whose duties with that carrier require an airman certificate and who is authorized by the certificate holder operating the aircraft to make specific trips over a route;
(v) An employee of the certificate holder operating the aircraft whose duty is directly related to the conduct or planning of flight operations or the inflight monitoring of aircraft equipment or
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(1) If the DGCA finds that design changes are necessary to correct the unsafe conditions of the product, and upon his request, submit appropriate design changes for approval; and
(2) Upon approval of the design changes, make available the descriptive data covering the changes to all operators of products previously certificated under the type certificate.
(b) In a case where there are no current unsafe conditions, but the DGCA or the holder of the type certificate finds through service experience that changes in type design will contribute to the safety of the product, the holder of the type certificate may submit appropriate design changes for approval. Upon approval of the changes, the manufacturer shall make information on the design changes available to all operators of the same type of product.
21.101Designation of Applicable Regulations.
(a) Except as provided in CASR Part 23 Sec. 23.2, CASR Part 25 Sec. 25.2, CASR Part 27 Sec. 27.2, CASR Part 29 Sec. 29.2, CASR Part 34, and CASR Part 36, an event for a change to a type certificate must comply with either-
(1) The regulations incorporated by reference in the type certificate; or
(2) The security regulations in effect on the date of the application, plus any other amendments the DGCA finds to be directly related.
(b) If the DGCA finds that a proposed change company of a new design or a substantially complete redesign of a component, equipment installation, or system installation, and that the regulations incorporated by reference in the type certificate for the product do not provide adequate standards with respect to the proposed change, the required must comply with-
(1) The renewable provisions of the airworthiness standard, in effect on the date of the application for the change, that the DGCA finds necessary to provide a level of safety equal to that established by the regulations incorporated by reference in the type certificate for the product; and
(2) Any special conditions, and amendments to those special conditions, prescribed by the DGCA to provide a level of safety equal to that established by the regulations incorporated by reference in the type certificate for the product.
(c) Unless otherwise required by Sec. 21.19 (a), an image for a change to a type certificate for a transport category airplane involving the replacement of reciprocating engines with the same number of turbopropeller powerplants must comply with the requirements of CASR Part 25 ase to the airplane as type certificated with reciprocating engines, and with the following:
(1) The certification performance requirements prescribed in Secs. 25.101 through 25,125 and 25,149, 25,1533, 25,1583, and 25,1587.
(2) The powerplant requirements CASR Part 25 turbocharged to turbo propeller engine powered airplanes.
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(3) The requirements of CASR Part 25 for the commission zation zation of cockpit controls and instruments, unless the DGCA finds that compliance with a particular detailed certificate would be impractical and would not contribute Materially materially to provide zation.
(4) Any other type of CASR Part 25 the air-powered to turbopropeller engine powered airplanes that the DGCA finds to be related to the changes in engines and that are necessary to ensure a level of safety equal to that of the airplane certificated with reciprocating engines. For each new limitation established with respect to weight, speed, or altitude that is significantly altered from those approved for the airplane with reciprocating engines, the information must show compliance with the requirements of CASR Part 25 add to the limitations being changed.
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SUBPART E SUPPLEMENTAL TYPE CERTIFICATES
21.111 Applicability.
This subpart prescribes procedural requirements for the issue of supplemental type certificates.
21.112 Eligibility.
Any interested person as prescribes in Sub Part J Design Organization Approval (DOA) may apply for a supplemental type certificate
21.113 MATERIAL EMENT of Supplemental Type Certificate.
(a) If a person holds the TC for a product and alters that product by introducing a major change in type design that does not require an application for a new TC under Section 21.19, that person must either apply to the DGCA for an STC or apply to amend the original type certificate under subpart D of this part.
(b) If a person does not hold the TC for a product and alters that product by introducing a major change in type design that does not require an application for a new TC under Section 21.19, that person must apply to the DGCA for an STC.
(c) The application for a suplemental type certificate is made on a form and in a manner prescribed by the DGCA.
21.115 Applicable Requirements.
(a) Each person for a supplemental type certificate must show that the altered product meets renewable airworthiness requirements as specified in paragraphs (a) and (b) of Sec. 21.101 and, in the case of an acoustical change described in Sec. 21.93 (b), show compliance with the renewable noise requirements of CASR Part 36 Secs. 36.7 and 36.9 and, in the case of an emissions change described in Sec. 21.93 (c), show compliance with the air fuel venting and exhaust emissions requirements of CASR Part 34.
(b) Each amount for a supplemental type certificate must meet Secs. 21.33 and 21.53 with respect to each change in the type design.
21.117 Issue of Supplemental Type Certificates.
(a) An insert is entitled to a supplemental type certificate if he meets the requirements of Secs. 21,113 and 21.115.
(b) A supplemental type certificate company of-
(1) The approval by the DGCA of a change in the type design of the product; and
(2) The type certificate previously issued issued for the product.
21.119 Privileges
The holder of a supplemental type certificate may-
(a) In the case of aircraft, obtain airworthiness certificates;
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(b) In the case of other products, obtain approval for installationges in a type design may be approved under a method acceptable to the DGCA before processing to the DGCA any substantiating or descriptive data.
21.97 Approval of Major Changes in Type Design.
(a) In the case of a major change in type design, the latter must-
(1) Provide substantiating data and necessary descriptive data for inclusion in the type design.
(2) Show that the change and areas affected by the change comply with the data requirements, and provide the DGCA the means by which such compliance has been shown; and
to supplier21.147 Amendment of the Production Certificates.
The holder of a production certificate must apply for an amendment to a production certificate in a form and manner prescribed by the DGCA. The Supporting for an amendment to a production certificate to add a type certificate or
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model, or both, must comply with the renewable requirements of Section 21.137, 21,138, and 21.150.
(1) Procedures to ensure that only products or articles are available. That means the design is installed on a type-certificated product. These procedures must provide for the identification, documentation, evaluation, segregation, and disposition of nonconforming products and articles. Only authorized individuals may make disposition determinations.
(2) Procedures to ensure that mathematical articles are rendered unusable.
(i) Corrective and Preventive Actions. Procedures for automated corrective and preventive actions to eliminate the causes of an actual or potential nonconformity to the approved design or noncompliance with the approved quality system.
(j) Handling and storage. Procedures to prevent damage and decay oration of each product and article during handling, storage, preservation, and packaging.
(k) Control of quality records. Procedures for identifying, storing, protecting, retaining, and retaining quality records. A production approval holder must retain these records for at least 5 years for the products and articles manufactured under the approval and at least 10 years for critical components identified under Section 45.15.
(b) Internal audits. Procedures for planning, conducting, and internal audits to ensure compliance with the approved quality system. The procedures must include reporting results of internal audits to the manager responsible for both corrective and preventive actions.
(m) In-service feedback. Procedures for receiving and processing feedback on in-service failures, malfunctions, and defects. These procedures must include a process for subjects the design approval holder to-
(1) Address any in-service problem involving design changes; and
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(2) Determine if any changes to the Instructions for Continued Airworthiness are necessary.
(n) Quality escapes. Procedures for analysis, analysis, and initiating appropriate corrective action for products or articles that have been released from the quality system and that do not conform to the database design data or quality system requirements.
21.138 Quality Manual.
Each controller for or holder a production certificate must provide a manual describing its quality system to the DGCA for approval. The manual must be in the Indonesian language and retrievable in a form acceptable to the DGCA.
21.139 Location of or Change to Manufacturing Facilities.
(a) An official may obtain a production certificate for manufacturing facilities located outside of the Republic of Indonesia if the DGCA finds no undue burden in administering the reserve regulation
(b) The production approval holder must obtain DGCA approval before making any changes to the location of any its manufacturing facilities.
(c) The production approval holder must immediately notify to DGCA, in writing, of any change to the manufacturing facilities that may affect the inspection, conformity or airworthiness of its product or article.
21.140 Inspections and Tests.
Each session for or holder of a production certificate shall allow the DGCA to inspect its quality system, facilities, technical data, and any Manufactured products or articles and witness any tests, including any inspections or test at supplier facility, necessary to determine compliance with the IBM Cloud Service.
21.141 Issuance.
The DGCA issues a production certificate after finding that the cules complies with the requirements of this subpart.
21.142 Production Limitation Record.
A production limitation record is issued as part of a production certificate. The record lists the type certificate of every product that the romantic is authorized to manufacture under the terms of the production certificate.
21.143 Duration.
A production certificate is effective until its death, suspended, revoked, or a termination date is otherwise established by the DGCA, or the location of the manufacturing facility is changed.
21.144 Transferability.
The holder of a production certificate may not transfer the production certificate.
21.145 Privileges.
(a) The holder of a production certificate may-
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(1) Obtain an aircraft airworthiness certificate without further showing, except that the DGCA may inspect the aircraft for conformity with the type design; or
(2) In the case of other products, obtain approval from the DGCA for installation on type-certificated aircraft.
(b) Provisions of the provisions of CASR Part 147 section 147.5, the holder of a production certificate for a primary category aircraft, or for a normal, utility, or acrobatic category aircraft of a type design that is eligible for a special airworthiness certificate in the primary category under section 21.184 (c), may-
(1) Conduct training for persons in the performance of a special inspection and preventive maintenance program approved as a part of the aircraft's type design under section 21.24 (b), provided a person holding a mechanic certificate with appropriate airframe and powerplant ratings issued under CASR part 65 gives the training; and
(2) Issue a certificate of competency to persons successfully created the approved training program, provided the certificate of the aircraft make and model to which the certificate applies.
21,146 Responsibility of Holder.
The holder of a production certificate shall-
(a) Amend the document required by section 21.135 as necessary to reflect changes in the organization and provide these amendments to the -DGCA.
(b) Maintain the quality system in compliance with the data and procedures approved for the production certificate;
(c) Mark the product or article for which a certificate or approval has been issued. Marking a must be in accordance with CASR part 45, including any critical parts;
(d) Identify any portion of the product or article (e.g., sub-assemblies, component parts, or replacement articles) that leave the manufacturer's facility as DGCA approved with the manufacturer's part number and name, trademark, symbol, or other DGCA approved manufacturer's identification;
(e) Have access to type design data necessary to determine conformity and airworthiness for each product and article produced under the production certificate;
(f) Retain its production certificate and make it available to the DGCA upon request; and
(g) Make available to the DGCA information regarding all delegation of authority product and article conforms to its approved design.
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(e) Inspecting and testing. Procedures for inspections and tests used to ensure that each product and article conforms to its approved design. These procedures must include the following, as well as the following:
(1) A flight test of each aircraft produced unless that aircraft will be exported as an unassembled aircraft.
(2) A functional test of in a good state of preservation and repair and is in a condition for safe operation.
(b) The DGCA prescribes limitations and conditions necessary for safe operation.
21,190 Issue of a special airworthiness certificate for a light-sport.
(a) Purpose. The DGCA issues a special airworthiness certificate in the light-sport category to operate a light-sport aircraft, other than a gyroplane.
(b) Eligibility. To be eligible for a special airworthiness certificate in the light-sport category:
(1) An airworthiness must provighting materials to which CASR Part 36 Sec. 36.1583 does not apply) that have not had any flight time before the renewable date specified in CASR Part 36, no standard airworthiness certificate is originally issued under this section unless the data shows that the type design complies with the air noise requirements of CASR Part 36 in addition to the air airworthiness requirements in this Section. For import
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airplanes, compliance with this paragraph is shown if the country in which the airplane was manufactured certifies, and the DGCA finds, that the renewable requirements of CASR Part 36 (or the air airplane noise) requirements of the country in which the airplane was manufactured and any other requirements the DGCA may prescribe to provide noise levels no greater than those provided by compliance with the renewable requirements of CASR Part 36) and paragraph (c) of this section are complied with.
(f) Passenger emergency exit requirements. Include all other provisions of this section, each issue for issuance of a standard airworthiness certificate for a transport category airplane manufactured after this Decree come into force, must show that the airplane meets the requirements of CASR Part 25 Sec. 25.807 (c) (7). For the purposes of this paragraph, the date of manufacture of an airplane is the date the inspection acceptance records reflect that the airplane is complete and meets the DGCA-approved type design data.
(g) Fuel venting and exhaust emission The requirements Include all other provisions of this section, and irrespective of the date of application, no airworthiness certificate is issued, on and after the dates specified in CASR Part 34 for the airplanes specified by the airplane specified in CASR Part 34 for the airplanes specified in CASR Part 34 for the airplanes with the security requirements.
(h) New aircraft manufactured under the provisions of Section 21.6 (b). An introduction for a standard airworthiness certificate for a new aircraft manufactured under the provisions of Section 21.6 (b) is entitled to a standard airworthiness certificate if-
(1) The exchange presents evidence to the DGCA that the aircraft conforms to a type design approved under a type certificate or supplemental type certificate and to air Airworthiness Directives;
(2) The aircraft has been inspected in accordance with the performance rules for a 100-hour list of sets forth in CASR 43 Section 43.15 and found airworthy by a person specified in paragraph (d) (2) of this section; and
(3) The DGCA finds after inspection, that the aircraft conforms to the type design, and is in condition for safe operation.
21.185 Issue of Airworthiness Certificates for Restricted Category Aircraft.
(a) Aircraft manufactured under a production certificate or type certificate. An issue for the original issue of a restricted category airworthiness certificate for an aircraft type certificated in the restricted category, that was not previously type certificated in any other category, must comply with the appropriate Provisions of Sec. 21.183.
(b) Other aircraft. An item for a restricted category airworthiness certificate for an aircraft type certificated in the restricted category, that was previously type certificated in another category, is entitled to an airworthiness certificate if the aircraft has been inspected by the DGCA and found by him
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to be in a good state of preservation and repair and in a condition for safe operation.
(c) Import aircraft. An issue for the original issue of a restricted category airworthiness certificate for an import aircraft type certificated in the restricted category only in accordance with Sec. 21.29 is entitled to an airworthiness certificate if the country in which the aircraft was manufactured certifies, and the DGCA finds, that the aircraft conforms to the type design and is in a condition for safe operation.
(d) Noise requirements. For propeller driven small airplanes (except airplanes designed for "agricultural aircraft operations,", or for dispensing firefighting materials) that have not had any flight time before the renewable date specified in, CASR Part 36 and notsed the other provisions of this section, no original restricted category airworthiness certificate is issued under this section unless the DGCA finds that the type design complies with the renewable noise requirements of CASR Part 36in addition to the The airworthiness requirements of this section. For importing airplanes, compliance with this paragraph is shown if the country in which the airplane was manufactured certifies, and the DGCA finds, that the renewable requirements of CASR Part 36 (or the air airplane noise requirements of the air) country in which the airplane was manufactured and any other requirements the DGCA may prescribe to provide noise levels no greater than those provided by compliance with the renewable requirements of CASR Part 36 and paragraph (c) of this section are complied with.
21,187 Issue of Multiple Airworthiness Certification.
(a) An For an airworthiness certificate in the restricted category, and in one or more other categories, is entitled to the certificate, if-
(1) He shows compliance with the requirements for each category, when the aircraft is in the configuration for that category; and
(2) He shows that the aircraft can be converted from one category to another by adding equipment by simple mechanical means.
(b) The operator of an aircraft certificated under this section shall have the aircraft inspected by the DGCA, or by a certificated mechanic with an appropriate airframe rating, to determine airworthiness each time the aircraft is converted from the restricted category to another category for the carriage of passengers for compensation or hire, unless the DGCA finds this unnecessary for safety in a particular case.
(c) The aircraft complies with the renewable requirements of CASR Part 34.
21,189 Issue of airworthiness certificate for limited category aircraft.
(a) An expression for an airworthiness certificate for an aircraft in the limited category is entitled to the certificate when-
(1) He shows that the aircraft has been previously issued a limited category type certificate and that the aircraft conforms to that type certificate; and
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(2) The DGCA finds, after inspection (including a flight check by the author), that the aircraft iscate:
(1) For transport category large airplanes and turbojet powered airplanes that have not had any flight time before the dates specified in CASR Part 36 Sec. 36.1 (d), no standard airworthiness certificate is originally issued under this section unless the DGCA finds that the type design complies with the noise requirements in CASR Part 36 Sec. 36.1 (d) in addition to the renewable airworthiness requirements in this section. For importing airplanes, compliance with this paragraph is shown if the country in which the airplane was manufactured certifies, esponding with the provisional type certificate.
(d) The information must submit a statement that the aircraft has been found by him to be in a safe operating condition under the limitations limitations.
(e) The aircraft must be flown at least five hours by the manufacturer.
(f) The aircraft must be supplied with a provisional aircraft flight manual containing the limitations established by Sec. 21.81 (h), 21.83 (h), and 21.83 (k).
21.225 Provisional Airworthiness Certificates Corresponding with Provisional Amendments to Type Cer aircraft has been flown for at least 50 hours, or for at least 5 hours if it is a type certificated aircraft which has been modified.
21.197 Special flight permits.
(a) A special flight permit may be issued for an aircraft that may not currently meet the airworthiness requirements but is capable of safe flight, for the following purposes:
(1) Flying the aircraft to a base where repairs, alterations, or maintenance are to be performed, or to a point of storage.
(2) Delivering or exporting the aircraft.
(3) Production flight testing testing new production aircraft.
(4) Evacuating aircraft from areas of Possible danger.
(5) Conducting customer demonstration flights in new production aircraft that have satisfactorily completed production flight tests.
(b) A special flight permit may also be issued to authorize the operation of an operation. 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.
(c) [To be determined]
21.199 Issue of special flight permits.
(a) An example for a special flight permit must submit a statement in a form and manner prescribed by the DGCA, indicating-
(1) The purpose of the flight.
(2) The proposed itinerary.
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(3) The crew required to operate the aircraft and its equipment, e.g., pilot, copilot, navigator, etc.
(4) The ways, if any, in which the aircraft does not comply with the air airworthiness requirements.
(5) Any restriction the information considers necessary for safe operation of the aircraft.
(6) Any other information considered necessary by the DGCA for the purpose of prescribing operating limitations.
(b) The DGCA may make, or require the role to make appropriate inspections or tests necessary for safety.
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SUBPART I PROVISIONAL AIRWORTHINESS CERTIFICATES
21.211 Applicability.
This subpart prescribes procedural requirements for the issue of provisional airworthiness certificates.
21.213 Eligibility.
(a) A manufacturer who is a Republic of Indonesia citizen may apply for a Class I or Class II provisional airworthiness certificate for aircraft manufactured by him within the Republic of Indonesia.
(b) Any holder of an air carrier operating certificate who is a Republic of Indonesia citizen may apply for a Class II provisional airworthiness certificate for transport category aircraft that meet either of the following:
(1) The aircraft has a current Class II provisional type certificate or an amendment thereto.
(2) The aircraft has a current provisional amendment to a type certificate that was corrected by a corresponding Class II provisional type certificate.
(c) An aircraft engine manufacturer who is a Republic of Indonesia citizen and who has altered a type certificated aircraft by installing different types certificated engines, manufactured by him within the Republic of Indonesia, may apply for a Class I provisional airworthiness certificate for that aircraft, if the basic aircraft, before alteration, was type certificated in the normal, utility, acrobatic, commuter, or transport category.
21.215 Application.
Application for provisional airworthiness certificates must be authorized to the DGCA. The application must be accompanied by the pertinent information specified in this subpart.
21.217 Duration.
unless it is the case of the word, super-ded, revoked, or otherwise terminated, provisional airworthiness certificates are on. effective for the duration of the corresponding provisional type certificate, amendment to a provisional type certificate, or provisional amendment to the type certificate.
21,219 Transferability.
Class I provisional airworthiness Certificates are not transferable. Class II provisional airworthiness certificates may be transferred to an air carrier eligible to apply for a certificate under Sec. 21.213 (b).
21.221 Class I Provisional Airworthiness Certificates.
(a) Except as provided in Sec. 21.225, an example is entitled to a Class I provisional airworthiness certificate for an aircraft for which a Class I provisional type certificate has been issued if-
(1) He meets the eligibility requirements of Sec. 21.213 and he complies with this section; and
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(2) The DGCA finds that there is no feature, characteristic or condition of the aircraft that would make the aircraft unsafe when operated in accordance with the limitations established in Sec. 21.81 (e) and 21.81 (h).
(b) The manufacturer must hold a provisional type certificate for the aircraft.
(c) The manufacturer must submit a statement that the aircraft conforms to the type design corresponding to the provisional type certificate and has been found by him to be in safe operating condition under all limitations limitations.
(d) The aircraft must be flown at least five hours by the manufacturer.
(e) The aircraft must be supplied with a provisional aircraft flight manual or other document and appropriate placards containing the limitations established by Secs. 21.81 (e) and 21.81 (h).
21.223 Class II Provisional Airworthiness Certificates.
(a) Except as provided in Sec. 21.225, an example is entitled to a Class II provisional airworthiness certificate for an aircraft for which a Class II provisional type certificate has been issued if-
(1) He meets the eligibility requirements of Sec. 21.213 and he complies with this section; and
(2) The DGCA finds that there is no feature, characteristic, or condition of the aircraft that would make the aircraft unsafe when operated in accordance with the limitations established in Sec. 21.81 (h), 21.83 (h), and 21.83 (k).
(b) The information must show that a Class II provisional type certificate for the aircraft has been issued to the manufacturer.
(c) The information must submit a statement by the manufacturer that the aircraft has been manufactured under a quality control system adequate to ensure that the aircraft conforms to the type design corrys">
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(b) A manufacturer of aircraft engines who has altered a type certificated aircraft by installing different engines, manufactured by him within the Republic of Indonesia, may apply for an experimental certificate for * That aircraft to be used for market surveys, sales demonstrations, or customer crew training, if the basic aircraft, before alteration, was type certificated in the normal, acrobatic, commuter, or transport category.
(c) A person who has altered the design of a type certificated aircraft may apply for an compliance with the renewable requirements of this Subpart; or
(2) The DGCA is prevented by the holder or any of its partners or companies to perform the following inspections in accordance with section 21.257; or
(3) There is evidence that the design assurance system cannot maintain control and supervision of the design of products or changes under the approval; or
(4) The certificate has been changed or revoked under the administrative administrative Established by the DGCA.
(b) Upon surrender or revocation, the certificate shalp-to-date description of the organization, and copies of amendments shall be supplied to the DGCA.
(d) The design organization shall furnish a statement of the qualifications and experience of the management staff and other persons responsible for making decisions affecting airworthiness and environmental protection in the organization.
(e) The design organization shall have a system for collecting, investigating and analyzing reports of and information related to failures, malfunctions, defects or other occurrences which cause or might cause adverse effects on the continuing airworthiness of the product, part or appliance covered by the type-certificate, restricted Type-certificate, supplemental type-certificate, TSO Authorization, major repair design approval or any other relevant approval deemed to have been issued under this Part. Information about this system shall be made available to all known operators of the product, part or appliance and, on request, to any person authorized under other downloaded Regulations.
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21.245 Approval requirements.
The design organization shall demonstrate, on the basis of the information rating in accordance with section 21.243 that, in addition to complying with section 21.239:
(a) Designate a DOA employee as the accountable manager whose responsibility is to ensure compliance.
(b) The staffs in all technical locations are of individual numbers and experience and have been given appropriate authority. to be able to discharge their allocated responsibilities and that these, together with the Accommodation, facilities and equipment are adequate to enable the staff to achieve the airworthiness, noise, fuel venting and exhaust emissions objectives for the product.
(c) There is a full and efficient coordination between the seers and the others. within its capacity in respect of airworthiness and environmental protection matters.
21.247 Changes in design assurance system.
After the issue of a design organization approval, each change to the design assurance system that is significant to the showing of compliance or to the airworthiness and environmental The protection of the product shall be approved by the DGCA. An application for approval shall be held in writing to the DGCA and the design organization shall demonstrate to the DGCA, on the basis of submission of proposed changes to the handbook, and before implementation of the change, that it will. continue to comply with this subpart after implementation.
21,249 Transferability.
Except as a result of a change in ownership, which is deemed significant for the purposes of section 21.247, a design organization approval is not Transferable.
21.251 Terms of approval.
The terms of approval shall identify the types of design work, the categories of products, parts and appliances for which the design organization holds a design organization approval, and the functions and duties that the organization is approved to perform in regard to the airworthiness and The characteristics of noise, fuel venting and exhaust emissions of products. For design and development of the Cloud Service, Client may not use the Cloud Service for any other use of the Cloud Service, including but not required to use the Cloud Service. Those terms shall be issued as part of a design organization approval.
21.253 Changes to the terms of approval.
Each change to the terms of approval shall be approved by the DGCA. An application for a change to the terms of approval shall be made in a form and manner established by the DGCA. The design organization shall comply with the renewable requirements of this Subpart.
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21.257 Inspections.
(a) The design organization shall make arrangements that allow the DGCA to make any inspections, including inspections of partners and companies, necessary to determine compliance and continued compliance with the renewable requirements of this Subpart.
(b) The design organization shall allow the DGCA to review any reports and make any inspection and perform or witness any flight and ground test necessary to check the validity of the compliance statements judged by the law under section 21.239 (b).
21.258 Findings.
(a) When objective evidence is found showing non-compliance of the holder of a design organization approval with the renewable requirements of this Part, the finding shall be classified as follows:
(1) A level one finding is any non-compliance with this Part which could lead to uncontrolled non-compliances with renewable requirements and which could affect the safety of the aircraft.
(2) A level two finding is any non-compliance with this Part which is not classified as level one.
(b) A level three finding is any item where it has been identified, by objective evidence, to contain potential problems that could lead to a non-compliance under paragraph (a) of this section.
(c) After receipt of notification of findings under the administrative administrative procedures established by the DGCA,
(1) In case of a level one finding, the holder of the design organization approval shall demonstrate corrective action to the satisfaction of the DGCA within a period of no more than 21 working days after written confirmation of the finding;
(2) In case of level two findings, the corrective action period granted by the DGCA shall be appropriate to the nature of the finding but in any case of their own shall not be more than six months. In certain circumstances and subject to the nature of the finding the DGCA may extend the six month period subject to a possible corrective action plan agreed by the DGCA.
(3) A level three finding shall not require immediate action by the holder of the design organization approval.
(d) In case of level one or level two findings, the design organization approval may be subject to a partial or full The suspension or revocation under the administrative administrative procedures established by the DGCA. The holder of the design organization approval shall provide confirmation of receipt of the notice of suspension or revocation of the design organization approval in a timely manner.
21.259 Duration and continued validity.
(a) A design organization approval shall be issued and valid for five years unless:
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(1) The design organization fails to demonstratesociated documentation to the DGCA.
(c) The design organization shall include the manner in which the design assurance system accounts for the acceptable tability of the parts or appliances designed or the tasks performed by partners or subcontractor according to methods which are the works subject of written procedures.
21.243 Data.
(a) The design organization shall furnish a manual to the DGCA describing, directly or by cross-reference, the organization, the relevant procedures and the products or changes to the products to be desi to an aircraft passes or has passed to a foreign purchaser-
(1) Request cancellation of the ROI registration and airworthiness certificates from the DGCA, giving the date of transfer of title, and the name and address of the foreign owner;
(2) Return the Registration and Airworthiness Certificates to the DGCA; and
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(3) Provide a statement to the DGCA certifying that the ROI Nationality and Identific.
Each holder of a PMA must-
(a) Amend the document required by sec. 21.305 as necessary to reflect changes in the organization and provide these amendments to the DGCA;
(b) Maintain the quality system in compliance with the data and procedures approved for the PMA;
(c) Ensure that each PMA article conforms to its approved design and is in a condition for safe operation;
(d) Mark the PMA article for which an approval has been issued. Marking must be in accordance with CASR part 45, including any critical parts;
(e) Identify any portion of the PMA article (e.g., sub-assemblies, component parts, or replacement articles) that leave the manufacturer's facility as DGCA approved. with the manufacturer's part number and name, trademark, symbol, or other DGCA approved manufacturer's identification;
(f) Have access to design data necessary to determine conformity and airworthiness for each article produced under the PMA;
(g) Retain each document granting PMA and make it available to the DGCA upon request; and
(h) Make available to the DGCA information regarding all delegation of authority to suppliers.
21.319 Design changes.
(a) Classification of design changes.
(1) A "minor change" to the design of an article produced under a PMA is one that has no longer capable effect on the approval basis.
(2) A "major change" to the design of an article produced under a PMA is any change that is not minor.
(b) Approval of design changes.
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(1) Minor changes to the basic design of a PMA may be approved using a method acceptable to the DGCA.
(2) The PMA holder must obtain obtain DGCA approval of any major change before including it in the design of an article produced under a PMA.
21.320 Changes in quality system.
After the issuance of a PMA-
(a) Each change to the quality system is subject to review by the DGCA; and
(b) The holder of the PMA must immediately notify the DGCA, in writing, of any change that may affect the inspection, conformity, or airworthiness of its article.
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SUBPART L EXPORT AIRWORTHINESS
21.321 Applicability.
This subpart prescribes-
(a) Procedural requirements for the issue of export airworthiness; and
(b) Rules governing the holders of those subjects.
21.325 Export Airworthiness Certificates.
(a) Export airworthiness approval for an aircraft is issued in the form of Export Certificates of Airworthiness. This certificate does not authorize the operation of aircraft.
(b) Export airworthiness approval an aircraft engine, propeller, or articles issued in the form prescribed by DGCA.
(c) Export airworthiness approval may be issued for a product or article located outside of the ROI, if DGCA finds no undue burden in administering the renewable regulations.
21.327 Application.
Any person may apply for export airworthiness approval. Each must apply in a form and manner of the prescribed form by the DGCA.
21.329 Issuance of Export Certificate of Airworthiness.
(a) A person may obtain from the DGCA an export certificate of airworthiness for an aircraft if-
(1) A new or used aircraft manufactured under subpart F or G of this part meets the airworthiness requirements under subpart H of this part H of this part for a-
(i) Standard airworthiness certificate; or
(ii) Special airworthiness certificate in the "primary" or "restricted" category; or
(2) A new or used aircraft not manufactured under subpart F or G of this part has a valid-
(i) Standard airworthiness certificate; or
(ii) Special airworthiness certificate in "primary" or "restricted" category
(b) An aircraft need not meet a specified specified in paragraph (a) of this section, as specified, if-
(1) The importing country or jurisdiction accepts, in a form and manner acceptable to the DGCA, a deviation from that ition; and
(2) The export certificate of airworthiness lists as an exception any difference between the aircraft to be exported and its type design.
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21.331 Issuance of export airworthiness for aircraft engines, propellers, and articles.
(a) A person may obtain from the DGCA an export airworthiness approval to export a new aircraft engine, propeller, or article that is manufactured under this part if it conforms to its approved design and is in a condition for safe operation.
(b) A new aircraft engine, propeller, or article need not meet a person of paragraph (a) of this section if-
(1) The importing country or jurisdiction accepts, in a form and manner acceptable to the DGCA, a deviation from that ition; and
(2) The export airworthiness approval lists as an exception any difference between the aircraft engine, propeller, or article to be exported and its approved design.
(c) A person may obtain from the DGCA an export airworthiness approval to export a used aircraft engine, propeller, or article if it conforms to its approved design and is in a condition for safe operation.
(d) A used aircraft engine or propeller need not meet a list of paragraph (c) of this section if-
(1) The importing country or jurisdiction accepts, in a form and manner acceptable to the DGCA, a deviation from that ition; and
(2) The export airworthiness approval lists as an exception any difference between the used aircraft engine or propeller to be exported and its approved design.
21,335 Responsibilities of Exporters.
Unless otherwise agreed to by the importing country or jurisdiction, each exporter must-
(a) Forward to the importing country or jurisdiction all documents specified by that country or jurisdiction;
(b) Preserve and package products and articles as necessary to protect them against corrosion and damage during transit or storage and state the duration of such preservation of such preservation andpackaging;
(c) Remove or cause to be removed any temporary installation incorporated on an aircraft for the purpose of export delivery and restore the aircraft to the approved configuration upon completion of the delivery flight;
(d) Secure all proper foreign entry clearances from all the countries or jurisdictions involved when conducting sales demonstrations or delivery flights; and
(e) When title otherwise authorized by the DGCA, the Holder or holder-
(1) May not present any article to the DGCA for an inspection or test unless compliance with Section 21.303 (b) (2) through (4) has been shown for that article; and
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(2) May not make any change to an article between the time that compliance with Section 21.303 (b) (2) through (4) is shown for that article and the time that the article is presented to ation mark have been removed from the aircraft in compliance with CASR 45.33.
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SUBPART M [To be determined]
SUBPART N ACCEPTANCE OF AIRCRAFT ENGINES, PROPELLERS, ARTICLES FOR IMPORTS
21,500 Acceptance of Aircraft Engines and Propellers.
An aircraft engine or propeller manufactured in a foreign country meets the requirements for acceptance under this subpart if-
(a) The holder or licensee of a ROI type certificate for that product furnishes with each such aircraft engine or propeller imported into Republic of Indonesia, an export airworthiness approval issued issued by the country of manufacturer of certifying that the individual aircraft engine or propeller-
(1) Conforms to its ROI type certificate and is in condition for safe operation; and
(2) Has been subjected by the manufacturer to a final operational check.
(b) That product is marked in accordance with CASR part 45.
21.502 Acceptance of Articles.
(a) An article manufactured in a foreign country which the Republic of Indonesia accepts of those materials, parts, or appliances for import, is considered to meet the requirements for acceptance in this CASR when the country of The individual article meets those requirements, unless the DGCA finds its requirements, unless the DGCA finds, based on the technical data. Consistent with the intent of this CASR.
(b) An importer for acceptance of an article must, upon request, submit to the DGCA any technical data respecting that article.
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SUBPART O TECHNICAL STANDARD ORDER AUTHORIZATIONS
21,601 Applicability and Definitions.
(a) This subpart prescribes-
(1) Procedural requirements for the issue of Technical Standard Order authorizations;
(2) Rules governing the holders of Technical Standard Order authorizations; and
(3) Procedural requirements for the issuance of a letter of Technical Standard Order design approval.
(b) For the purpose of this subpart-
(1) A Technical Standard Order (referred to in this subpart as "TSO") is issued by the DGCA and is a minimum performance standard for specified articles (for the purpose of this subpart, articles means materials, parts, processes, or appliances) used on civil aircraft.
(2) A TSO authorization is an DGCA design and production approval issued issued issued to the manufacturer of an article which has been found to meet a specific TSO.
(3) A letter of TSO design approval is a DGCA design approval for an article which has been found to meet a specific TSO in accordance with the procedures of Sec. 21.621.
(4) An article manufactured under an TSO authorization, a DGCA letter of acceptance as described in Sec. 21.613 (b), or an article manufactured under a letter of TSO design approval rating in Sec. 21.621 is an approved article for the purpose of meeting the regulations of this CASR that require the article to be approved; and
(5) An article manufacturer is the person who controls the design and quality of the article produced (or to be produced, in the case of an application), including the parts of them and any processes or services related to them that are procured from an outside source.
(c) The DGCA does not issue an TSO authorization if the manufacturing facilities for the product are located outside of the Republic of Indonesia, unless the DGCA finds that the location of the manufacturer's facilities places no undue burden on the DGCA in administering the regulations.
21.603 Application.
(a) An expression for a TSO authorization must apply in the form and manner prescribed by the DGCA. The information must include the following documents in the application:
(1) A statement of conformance certifying that the law has met the requirements of this subpart and that the article concerned meets the renewable TSO that is effective on the date of application for that article.
(2) One copy of the technical data required in the applicable TSO.
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(b) If the expected results are in accordance with Sec.21.619, the may set forth in its application the basic model number of the article and the part number of the components with open brackets after it to denote that suffix change letters or numbers (or else of them) will be added from time to time.
(c) If the application is deficient, the must, when requested by the DGCA, provide any additional additional information necessary to show compliance with this part. If the user fails to provide the additional information within 30 days after the DGCA's request, the DGCA denies the application and notifies the organization.
21,605 Organization.
Each person of a person of a TSO. Must provide the DGCA with a document describing how the organization's organization will ensure compliance with the provisions of this subpart. At a minimum, the document must describe assigned responsibilities and delegated authority, and the functional relationship of those responsible for quality to management and other organizational components.
21,607 Quality system.
Each forage for or holder of a TSO authorization must establish a quality system that meets the requirements of Sec. 21.137.
21.608 Quality manual.
Each law for or holder of a TSO authorization must provide a manual describing its quality system to the DGCA for approval. The manual must be in the Indonesian language and retrievable in a form acceptable to the DGCA.
21.609 Location of or change to manufacturing facilities.
(a) An official may obtain a TSO authorization for manufacturing facilities located outside of the ROI if the DGCA finds no undue burden in administering the renewable regulation.
(b) The TSO authorization holder must obtain DGCA approval before making any changes to the location of any of its manufacturing facilities.
(c) The TSO authorization holder must immediately notify the DGCA, in writing, of any change to the manufacturing facilities that may affect the inspection, conformity, or Airworthiness of its product or article.
21,610 Inspections and tests.
Each law for or holder of a TSO authorization must allow the DGCA to inspect its quality system, facilities, technical data, and any manufactured articles and witness any tests, including any inspections or tests at a supplier facility, necessary to determine compliance with this renewable CASR.
21.611 Issuance.
If the DGCA finds that the berates complies with the requirements of this renewable CASR, the DGCA issues a TSO authorization to the air (including all TSO deviations granted to the sound).
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21.613 Duration.
(a) A TSO's authorization or letter of TSO design approval is effective for two years until it is terminated, respectively, or otherwise terminated by the DGCA.
(b) If a TSO is revised or canceled, the holder of an affected DGCA letter of acceptance of a statement of conformance, TSO authorization, or letter of TSO design approval may continue to manufacture articles that meet the original TSO without A new acceptance, authorization, or approval but must comply with the CASR.
21.614 Transferability.
The holder of a TSO authorization or letter of TSO design approval may not transfer the TSO authorization or letter of TSO design approval.
21.616 Responsibility of holder.
Each holder of a TSO authorization must-
(a) Amend the document required by Sec 21.605 as necessary to reflect changes in the organization and provide these amendments to the DGCA
(b)} {\b}} {\b}} {\" \" (b)} {\" \" (b)} {\" \" (b)} { The Procedures approved for the TSO authorization;
(c) Ensure that each manufactured article conforms to its approved design, is in a condition for safe operation, and meets the renewable TSO;
(d) Mark the TSO article for which an approval has been issued. Marking must be in accordance with CASR part 45, including any critical parts;
(e) Identify any portion of the TSO article (e.g., sub-assemblies, component parts, or replacement articles) that leave the manufacturer's facility as DGCA approved. with the manufacturer's part number and name, trademark, symbol, or other DGCA approved manufacturer's identification;
(f) Have access to design data necessary to determine conformity and airworthiness for each article produced under the TSO It's The manufacturer must retain this data until it no longer comes into the article. At that time, copies of the data must be sent to the DGCA;
(g) Retain its TSO authorization and make it available to the DGCA upon request; and
(h) Make available to the DGCA information regarding all delegation of authority to suppliers
21.618 Approval for deviation.
(a) Each manufacturer who requests approval to deviate from any performance standard of a TSO must show that factors or design features providing an equivalent level level of safety compensate for the standards from which a deviation is requested.
(b) The manufacturer must send requests for approval to deviate, together with all pertinent data, to the appropriate aircraft certification office. If the article is manufactured under the authority of a foreign country or jurisdiction, the manufacturer must send requests for approval to deviate, together with all
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pertinent data, through the civil aviation authority of that country or jurisdiction to the DGCA.
21.619 Design changes.
(a) Minor changes by the manufacturer holding a TSO authorization. The manufacturer of an article under an authorization issued under this part may make minor design changes (any change other than a major change) without further approval by the DGCA. In this case, the changed article keeps the original model number (part numbers may be used to identify minor changes) and the manufacturer must forward to the appropriate aircraft certification office, any revised data that are necessary for compliance with Sec 21.603 (b).
(b) Major changes by the manufacturer holding a TSO authorization. Any design change by the manufacturer extensive enough to require a substantially complete investigation to determine compliance with a TSO is a major change. Before making a major change, the manufacturer must assign a new type or model designation to the article and apply for an authorization under Sec. 21.603.
(c) Changes by persons other than the manufacturer. No. Design change by any person (other than the manufacturer who provided the statement of conformance for the article) is eligible for approval under this part unless the person seeking the approval is a manufacturer and applies under Sec. 21.603 (a) for a separate TSO authorization. Persons other than a manufacturer may obtain approval for design changes under part 43 or under the air airworthiness regulations.
21.620 Changes in quality system.
After the issuance of a TSO authorization-
(a) Each change to the quality system is subject to review by the DGCA; and
(b) The holder of the TSO authorization must immediately notify the DGCA, in writing, of any change that may affect the inspection, conformity, or airworthiness of its article.
21.621 Issue of letters of TSO design approval: Import articles.
(a) The DGCA may issue a letter of TSO design approval for an article-
(1) Designed and manufactured in a foreign country to the export provisions of an agreement with ROI for the acceptance of these articles for import; and
(2) For importation into ROI if-
(i) The State of Design certifies that the article has been examined, tested, and found to meet the renewable TSO or the renewable performance standards of the State of Design and any other performance standards the DGCA may prescribe to provide a level of safety equivalent to that provided by the TSO; and
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(ii) The manufacturer has provided to the DGCA one copy of the technical data required in the renewable performance standard through its State of Design.
(b) The DGCA issues the letter of TSO design approval that lists any deviation granted under Sec.21.618.
MINISTER OF RELATIONS
REPUBLIC OF INDONESIA,
IGNASIUS JONAN
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