Civil Aviation Regulations 1988 (Cth)
made under the
This compilation is in 2 volumes
Volume 2: Schedules and Endnotes
Each volume has its own contents
This is a compilation of the
The notes at the end of this compilation (the
The effect of uncommenced amendments is not shown in the text of the compiled law. Any uncommenced amendments affecting the law are accessible on the Register ( The details of amendments made up to, but not commenced at, the compilation date are underlined in the endnotes. For more information on any uncommenced amendments, see the Register for the compiled law.
If the operation of a provision or amendment of the compiled law is affected by an application, saving or transitional provision that is not included in this compilation, details are included in the endnotes.
For more information about any editorial changes made in this compilation, see the endnotes.
If the compiled law is modified by another law, the compiled law operates as modified but the modification does not amend the text of the law. Accordingly, this compilation does not show the text of the compiled law as modified. For more information on any modifications, see the Register for the compiled law.
If a provision of the compiled law has been repealed in accordance with a provision of the law, details are included in the endnotes.
Contents
These Regulations are the
Civil Aviation Regulations 1988 .
(1) In these Regulations, unless the contrary intention appears:
adopted in pursuance of the Convention means adopted by the International Civil Aviation Organization in pursuance of Article 37 of the Chicago Convention.
agricultural operations means the broadcasting of chemicals, seeds, fertilizers and other substances from aircraft for agricultural purposes, including purposes of pest and disease control.
aircraft component means:
(a) any part or equipment for an aircraft that, when fitted to, or provided in an aircraft may, if it is not sound or functioning correctly, affect the safety of the aircraft, its occupants or its cargo or cause the aircraft to become a danger to person or property; or
(b) flotation equipment, evacuation equipment, ration packs, portable breathing apparatus, fire‑fighting equipment, or any other equipment or apparatus, fitted to, or provided in, an aircraft for use in an emergency;
but does not include any part, equipment or apparatus for an aircraft in respect of which a direction is in force under subregulation (2).
aircraft log book means a log book kept for the purposes of subregulation 50A(1).
aircraft maintenance record means:
(a) an aircraft log book; or
(b) an approved alternative maintenance record.
aircraft material means a material (including a fluid) for use in the manufacture, maintenance, servicing or operation of an aircraft or of an aircraft component, but does not include an aircraft component.
aircraft welding authority means an authority granted under regulation 33D.
airworthiness authority means an authority under regulation 33B.
approved alternative maintenance record means a record kept for the purposes of subregulation 50B(3) or (4).
approved maintenance data , in relation to an aircraft, aircraft component or aircraft material, has the meaning given by regulation 2A.
approved system of certification of completion of maintenance means a system of certification of completion of maintenance for which an approval under regulation 42ZG is in force.
approved system of maintenance , for an Australian aircraft, means a system of maintenance for the aircraft that has been approved under regulation 42M, including any changes to the program that have been approved under regulation 42R.
CASA maintenance schedule means the schedule of maintenance set out in Schedule 5.
CASA system of certification of completion of maintenance means the system of certification of completion of maintenance set out in Schedule 6.
CASR means theCivil Aviation Safety Regulations 1998 .
centre of gravity , in relation to an aircraft at any time, means the centre of gravity of the aircraft at that time estimated in accordance with the method set out in a direction in force under regulation 235.
certificate of approval means a certificate of approval in force under regulation 30.
certificate of type approval means a certificate of type approval continued in force under regulation 313 or a type certificate issued under regulation 21.013A or 21.029 of CASR.
class A aircraft means an Australian aircraft, other than a balloon, that satisfies either or both of the following paragraphs:
(a) the aircraft is certificated as a transport category aircraft;
(b) the aircraft is being used, or is to be used, by the holder of an Australian air transport AOC which authorises the use of that aircraft in scheduled air transport operations.
Note: Subregulation 2(2C) sets out how an aircraft is certificated as a transport category aircraft.
class B aircraft means an Australian aircraft that is not a class A aircraft.
commercial operations means civil air operations other than private operations.
Commonwealth aircraft means an aircraft, other than a military aircraft, that is in the possession or under the control of the Commonwealth or an authority of the Commonwealth or is being used wholly or principally for a purpose of the Commonwealth.
daily inspection , in relation to an aircraft, means:
(a) if the aircraft is maintained in accordance with the CASA maintenance schedule—the inspection referred to in Part 1 of the schedule; and
(b) if the aircraft is not maintained in accordance with the CASA maintenance schedule—the inspection required to be carried out under:
(i) the manufacturer’s maintenance schedule; or
(ii) the aircraft’s approved system of maintenance;
before the start of flying operations on each day that the aircraft is to be flown.
dangerous lights means any lights which may endanger the safety of aircraft, whether by reason of glare, or by causing confusion with or preventing clear visual reception of aeronautical lights or signals.
dual flying means flying in an aircraft fitted with fully functioning dual controls for the purpose of receiving flying training from a person who is authorised by these Regulations to give the training.
Federal airport has the same meaning as in theFederal Airports Corporation Act 1986 .
flight control system , in relation to an aircraft, includes:
(a) the aircraft’s main control surfaces and associated operating mechanisms and control systems; and
(b) the aircraft’s lift and drag devices and associated operating mechanisms and control systems; and
(c) the aircraft’s trim and artificial feel systems and associated operating mechanisms and control systems; and
(d) the aircraft’s flight control lock system and associated operating mechanisms and control systems; and
(e) the aircraft’s yaw system and associated operating mechanisms and control systems; and
(f) if the aircraft is a rotorcraft—the aircraft’s pitch control systems; and
(g) if the aircraft is an airship—the aircraft’s ballonet system and associated operating mechanisms and control systems.
flight plan means specified information, provided to air traffic control, relative to the intended flight of an aircraft.
gross weight , in relation to an aircraft at any time, means the weight of the aircraft, together with the weight of all persons and goods (including fuel) on board the aircraft, at that time, estimated in accordance with the method set out in a direction in force under regulation 235.
I.F.R. is the symbol used to designate the Instrument Flight Rules prescribed in Part 12.
landing strip means a rectangular portion of the landing area, specially prepared for the take‑off and landing of aircraft in a particular direction.
maintenance controller means a person:
(a) appointed under regulation 42ZV; and
(b) whose appointment:
(i) is approved under regulation 42ZW; and
(ii) is not suspended or cancelled under regulation 42ZX.
maintenance control manual means a maintenance control manual mentioned in regulation 42ZY.
maintenance instruction means an instruction that is issued by:
(a) CASA or an authorised person in writing under regulation 38; or
(b) the manufacturer of an aircraft, aircraft component or aircraft material; or
(c) the designer of a modification or repair of an aircraft or aircraft component;
but does not include an instruction issued by a manufacturer or designer if it is clear from the terms of the instruction that the manufacturer or designer regards compliance with the instruction as optional.
maintenance release means a maintenance release in force under regulation 43.
maintenance schedule , in relation to a class B aircraft, means the maintenance schedule referred to in regulation 42A, 42B, 42C or 42CA that applies to the aircraft.
major damage , in relation to an aircraft, means damage of such a kind that it may affect the safety of the aircraft or cause the aircraft to become a danger to person or property.
manual welding means welding carried out and controlled completely by hand.
manufacturer’s maintenance schedule , in relation to an aircraft, means a schedule issued by the manufacturer of the aircraft that sets out what maintenance should be carried out on the aircraft and when it should be carried out.
moored , in relation to lighter‑than‑air aircraft, means the aircraft:
(a) is tethered; and
(b) is not occupied by any person.
operating crew means a crew member.
permissible unserviceability , for an aircraft, means:
(a) a defect in the aircraft approved by CASA as a permissible unserviceability under regulation 37; or
(b) a defect in the aircraft approved by CASA, an authorised person or an approved design organisation as a permissible unserviceability under regulation 21.007 of CASR.
servicing , in relation to an aircraft, means preparing the aircraft for flight, and includes providing the aircraft with fuel and other fluids that are necessary for its operation, but does not include any work that is maintenance.
synthetic flight trainer means a flight simulator, a flight training device, or a synthetic trainer.Note 1: For definitions of
flight simulator andflight training device , see the CASR Dictionary.Note 2: Standards for flight simulators and flight training devices are set out in the document called ‘Manual of Standards (MOS) – Part 60’ published by CASA.
Note 3: Standards for synthetic trainers are set out in the document called ‘FSD‑2 Operational Standards and Requirements – Approved Synthetic Trainers’ published by CASA.
synthetic trainer means a ground training device, other than a flight simulator or a flight training device, that simulates or represents flight conditions, aircraft characteristics and a cockpit environment.
the Convention means the Chicago Convention.
these Regulations includes CASR.
time‑lifed aircraft component means an aircraft component (including an engine or propeller) that:
(a) the manufacturer of the component; or
(b) if the component has been modified—the designer of the modification; or
(c) CASA;
has instructed must be retired or overhauled or removed from an aircraft within a particular period.
(2) CASA may direct that any part, equipment or apparatus for an aircraft shall, for the purposes of these Regulations, be deemed not to be an aircraft component.
(2A) A reference in these Regulations to maintenance on an aircraft includes a reference to maintenance on aircraft components and aircraft materials.
(2B) A reference in these Regulations to an aircraft component, or aircraft material, included in an aircraft includes a reference to an aircraft component or aircraft material that is usually included in the aircraft but that has been temporarily removed from the aircraft for any purpose (including for the purpose of having maintenance carried out).
(2C) For the purposes of these Regulations, an aircraft is certificated as a transport category aircraft if:
(a) there is a certificate of airworthiness in force in relation to the aircraft; and
(b) the certificate includes a statement to the effect that the certificate is issued in the transport category.
(2D) For the purposes of CAR, the categories of maintenance are as follows:
(a) maintenance on aircraft airframes;
(b) maintenance on aircraft engines;
(c) maintenance on aircraft radio systems;
(d) maintenance on aircraft electrical systems;
(e) maintenance on aircraft instruments.
(9) Any reference in these Regulations to the owner of an aircraft must, where under a contract of hire or charter agreement the control, maintenance and operation of the aircraft is vested in the hirer, be read as a reference to the hirer.
The arrangements, identified for the purposes of the definition of
ANZA mutual recognition agreements in section 3 of the Act, are:
(a) the arrangement set out in the document entitled ‘Arrangement between the Australian and New Zealand Governments on Mutual Recognition of Aviation‑Related Certification’, signed at Wellington on 13 February 2007; and
(b) the arrangement set out in the document entitled ‘Operational Arrangement between the Civil Aviation Safety Authority of Australia and the Civil Aviation Authority of New Zealand in relation to mutual recognition of Air Operator Certificates’, signed on 16 March 2007.
(1) Subject to subregulation (3), the approved maintenance data for an aircraft, aircraft component or aircraft material consists of the requirements, specifications and instructions that are:
(a) contained in the maintenance data set out in subregulation (2); and
(b) applicable to the maintenance of the aircraft, aircraft component or aircraft material, as the case requires.
(2) For the purposes of paragraph (1)(a), the maintenance data are:
(a) requirements in:
(i) regulations 42U, 42W, 42X, 42Y, 42Z and 42ZA or in instruments made under those regulations; and
(ii) directions (however described) made under an airworthiness directive or under regulation 25, 38 or 44;
being requirements that specify how maintenance on aircraft, aircraft components or aircraft materials is to be carried out; and
(b) specifications of how maintenance on an aircraft, aircraft component or aircraft material is to be carried out, in documents or designs approved under another provision of these Regulations; and
(c) instructions, issued by the manufacturers of aircraft, aircraft components or aircraft materials, that specify how maintenance on the aircraft, components or materials is to be carried out; and
(d) instructions, issued by the designers of modifications of aircraft or aircraft components, that specify how maintenance on the aircraft or components is to be carried out; and
(e) any other instructions, approved by CASA under subregulation (4) for the purposes of this paragraph, relating to how maintenance on aircraft, aircraft components or aircraft materials is to be carried out.
(3) CASA may, for the purpose of ensuring the safety of air navigation, declare in writing that an instruction mentioned in paragraph (2)(c) or (d) that CASA thinks is deficient is not included in the approved maintenance data for an aircraft, aircraft component or aircraft material.
(4) CASA may, for the purposes of paragraph (2)(e), approve instructions relating to how maintenance on aircraft, aircraft components or aircraft material is to be carried out.
(1) If:
(a) a provision of these Regulations refers to a prescribed act done by CASA or an authorised person; and
(b) there is no provision of the Act or these Regulations expressly authorising CASA or an authorised person to do the act;
the provision mentioned in paragraph (a) is taken to authorise CASA or an authorised person, as the case may be, to do the act.
(2) For the purposes of this regulation, CASA or an authorised person is taken to do a prescribed act if CASA or the authorised person issues, gives or grants a direction, instruction, notification, exemption, permission, approval or authority, or does any other act or thing.
(1) CASR is to be read with, and as if it formed part of, CAR.
(2) However, if there is any inconsistency between CAR and CASR, CASR prevails to the extent of the inconsistency.
(1) Subject to these Regulations, these Regulations apply to and in relation to:
(a) international air navigation within Australian territory;
(b) air navigation in relation to trade and commerce with other countries and among the States;
(c) air navigation within the Territories;
(d) air navigation to or from the Territories;
(e) air navigation in which a Commonwealth aircraft is engaged;
(f) air navigation in controlled air space that is of a kind not specified in paragraph (a), (b), (c), (d) or (e) but directly affects, or may endanger, the safety of persons or aircraft engaged in:
(i) air navigation of a kind specified in paragraph (a), (b), (d) or (e); or
(ii) air navigation in which a military aircraft is engaged; and
(g) all air navigation within Australian territory of a kind not specified in paragraph (a), (b), (c), (d) or (e).
(2) Except where otherwise prescribed, the provisions of these Regulations shall apply to and in relation to Australian aircraft engaged in air navigation outside Australian territory.
(3) When an Australian aircraft is flying over the high seas, the provisions of Annex 2 to the Convention shall apply to and in relation to that aircraft and that flight in substitution for the corresponding provisions of these Regulations relating to the flight and manoeuvre of aircraft.
(4) CASA shall notify in the AIP any differences between the provisions of these Regulations relating to the flight and manoeuvre of aircraft and the provisions of Annex 2 to the Convention.
(5) Subject to these Regulations, these Regulations do not apply to or in relation to state aircraft or to military aerodromes.
(6) Notwithstanding the provisions of subregulation (5), the provisions of these Regulations relating to flight and manoeuvre of aircraft and the licensing of personnel apply to and in relation to a flight by an Australian military aircraft where the aircraft is flown by a person other than a member of the Defence Force.
(1) CASA shall, subject to the directions of the Minister, be charged with the administration of these Regulations, and shall exercise and perform the powers and functions conferred on CASA by these Regulations.
(2) CASA shall maintain close liaison with the Department of Defence in matters of common interest.
(1) This regulation applies if CASA is empowered or required under these Regulations:
(a) to issue a direction, instruction or notification; or
(b) to give a permission, approval or authority.
(1A) CASA may, unless the contrary intention appears in the regulation conferring the power or function or imposing the obligation or duty, issue the direction, instruction or notification or give the permission, approval or authority in Civil Aviation Orders or otherwise in writing.
(2) Expressions used in Civil Aviation Orders shall, unless the contrary intention appears, have the same meanings as in these Regulations.
(3) If a direction, instruction or notification relating to a person is issued in Civil Aviation Orders, the direction, instruction or notification, as the case may be, is taken to have been served on the person on the date on which the making of the Order is registered on the Federal Register of Legislation.
(1) Where an aircraft possessing the nationality of a Contracting State is in Australian territory and is found to have suffered major damage or to have developed a major defect, CASA may direct that the aircraft shall not fly.
(2) Where CASA gives a direction under this regulation, CASA shall furnish to the appropriate authority of the Contracting State a notification of the action taken by CASA and a report of the damage or defect, as the case may be.
(3) CASA may, unless CASA considers that it would be detrimental to the safety of air navigation to do so, revoke a direction given under this regulation if the appropriate authority of the Contracting State notifies CASA that the appropriate authority:
(a) has revoked any suspension of the certificate of airworthiness of the aircraft to which the direction relates that the appropriate authority had imposed;
(b) considers that the damage or defect by reason of which the direction was given is not of such a nature as to prevent the aircraft from fulfilling the minimum requirements of safety adopted in pursuance of the Convention; or
(c) considers that, in the circumstances of the case, the aircraft to which the direction relates should be permitted to fly without passengers to a place at which the necessary repairs or modifications can be made.
(4) In revoking a direction under this regulation, CASA may give a further direction imposing such conditions on the operation of the aircraft as are notified to CASA by the appropriate authority referred to in subregulation (3).
(5) A direction given under this regulation does not have effect in relation to a person until it has been served:
(a) on the person; or
(b) if the direction cannot be served on the person—by affixing the direction to the aircraft to which it relates.
(6) A person must not fly an aircraft in contravention of a direction, or any condition imposed by a direction, given under this regulation.
Penalty: 50 penalty units.
(7) An offence against subregulation (6) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .
(1) In this Division:
aircraft welding examination means a welding examination:
(a) based on examination materials published by CASA in a document called ‘Aircraft Welding Examinations’ as in force from time to time; and
(b) conducted by CASA or an authorised person.
welding training means practical and theoretical training that:
(a) is based on Australian Standard AS 1796 as in force from time to time; and
(b) is conducted by an organisation that carries out training in welding.
(2) For the purposes of this Division, the types of manual welding are as follows:
(a) type 1—gas welding;
(b) type 2—braze welding;
(c) type 3—manual metal arc welding;
(d) type 4—gas tungsten arc welding;
(e) type 5—gas metal arc welding;
(f) type 6—plasma arc welding.
(3) For the purposes of this Division, the parent metal groups are as follows:
(a) group 1—aluminium alloys;
(b) group 2—magnesium alloys;
(c) group 3—carbon steel and low alloy steels;
(d) group 4—corrosion and heat resisting steels;
(e) group 5—nickel alloys;
(f) group 6—copper‑based alloys;
(g) group 7—titanium alloys.
(1) Subject to subregulation (1A), a person engaged, or intending to engage, in any stage of distribution or maintenance of aircraft, aircraft components or aircraft materials may apply to CASA for a certificate of approval in respect of those activities.
(1A) A person may make an application under subregulation (1) in relation to the maintenance of an aircraft or an aeronautical product only if Part 42 of CASR does not apply to the aircraft or aeronautical product.
(2) An application must be in writing and must:
(a) set out the following:
(i) a statement of the activities to be covered by the certificate, including any training or assessment in the maintenance of aircraft, aircraft components or aircraft materials that the applicant intends to conduct;
(ii) the address of the main place (if any) at which the applicant proposes to carry out those activities;
(iii) the number of appropriately qualified or experienced persons employed by the applicant who will be involved in carrying out those activities; and
(b) have with it evidence of:
(i) the relevant qualifications and experience of the applicant and the applicant’s employees; and
(ii) the facilities and equipment available to the applicant for the carrying out of the activities; and
(iii) the arrangements made to ensure the applicant has, and will continue to receive, information necessary for the carrying out of those activities; and
(iv) a system of quality control that satisfies the requirements of subregulation (2D); and
(c) if maintenance of class A aircraft is an activity to be covered by the certificate—have with it a copy of the procedures manual, in which the system of quality control procedures must be set out, that the applicant proposes to use if the certificate of approval is granted.
(2A) CASA must grant the applicant a certificate of approval covering the activities to which the application relates if CASA is satisfied that the applicant is able to carry out the activities in a satisfactory manner.
(2B) In deciding whether it is satisfied as mentioned in subregulation (2A), CASA must have regard to:
(a) the relevant qualifications and experience of the applicant and the applicant’s employees; and
(b) the facilities and equipment available to the applicant for the carrying out of those activities; and
(c) the arrangements made to ensure the applicant has, and will continue to receive, the information necessary for the carrying out of those activities; and
(d) the applicant’s system of quality control; and
(e) if the applicant is required by paragraph (2)(c) to have a procedures manual—the applicant’s procedures manual.
(2C) A certificate of approval is subject to:
(a) a condition that each activity the certificate covers must only be carried out at a place where the facilities and equipment necessary for the proper carrying out of the activity are available to the holder of the certificate;
(b) a condition that the activities the certificate covers must be carried out in accordance with a system of quality control that satisfies the requirements of subregulation (2D); and
(c) if the certificate covers some or all of the following activities:
(vii) the maintenance of aircraft;
(viii) the maintenance of aircraft components;
(ix) the maintenance of aircraft materials;
a condition that each of those activities that is covered by the certificate must be carried out under the control of a person appointed by the applicant to control the activities; and
(ca) if the certificate covers training or assessment in the maintenance of aircraft, aircraft components or aircraft materials—a condition that the holder of the certificate must comply with the requirements (if any) prescribed by legislative instrument issued by CASA under regulation 30AA that apply to the holder; and
(d) a condition that the holder of the certificate of approval must ensure that each person employed by, or working under an arrangement with, the holder receives adequate training in:
(i) the work performed by the person for the purposes of the activities covered by the certificate; and
(ii) the use of any equipment used in connection with that work.
(2D) A system of quality control must be in writing and must contain the following:
(a) the procedures to be followed in connection with the carrying out of the activities covered by the certificate that, in particular, includes procedures for:
(i) the control of the work carried out under the certificate; and
(ii) the maintenance, control and calibration of equipment; and
(iii) the control of stores;
(b) a statement:
(i) that sets out the places at which the activities covered by the certificate are, or will be, carried out and which activities are, or will be, carried out at each place; and
(ii) that identifies any mobile facilities available to the certificate of approval holder for the carrying out of the activities covered by the certificate and which activities are, or will be, carried out using each mobile facility;
(c) in relation to each activity covered by the certificate that is required, by paragraph (2C)(c), to be carried out under the control of a person—the name of the position occupied by the person who controls the carrying out of the activity;
(d) a description of the applicant’s organisational structure, the responsibilities of employees within the structure and the procedures to be followed by the employees in undertaking the activities covered by the certificate;
(e) a description of the resources for implementing quality management;
(f) a description of the audit system applying to the system of quality control;
(g) if the quality control system is set out in a procedures manual required under paragraph (2)(c)—a statement of the procedures to be followed in relation to the amendment of the procedures manual.
Note: Australian Standards AS3900 to AS3904 provide guidance for the content of a system of quality control.
(3) CASA may, for the purpose of ensuring the safety of air navigation, include in a certificate of approval granted under this regulation an endorsement that the certificate is granted subject to a condition set out in the endorsement, in a document issued with the certificate of approval or in a specified Part or Section of Civil Aviation Orders.
(3A) A person must not contravene a condition to which a certificate of approval is subject.
Penalty: 25 penalty units.
(3B) An offence against subregulation (3A) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .(3C) It is a defence to a prosecution under subregulation (3A) if the defendant had a reasonable excuse.
Note: A defendant bears an evidential burden in relation to the matter in subregulation (3C) (see subsection 13.3(3) of the
Criminal Code ).(4) An authorised person may, at any time, for the purpose of ascertaining whether the activities to which a certificate of approval relates are being carried on in a satisfactory manner:
(a) inspect any aircraft, aircraft component or aircraft material;
(b) inspect any process or systems carried on by, any records maintained by or any documents in the possession of, the holder of the certificate of approval in connection with the activities to which the certificate of approval relates;
(c) conduct any tests that the authorised person considers necessary; and
(d) require the holder of the certificate of approval to furnish to the authorised person such evidence as the authorised person requires:
(i) of the qualifications and competence of the holder or of the qualifications and competence of the employees of the holder; or
(ii) of the facilities at the disposal of the holder.
(4A) The holder of a certificate of approval must give to an authorised person the evidence required under paragraph (4)(d).
Penalty: 5 penalty units.
(4B) An offence against subregulation (4A) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .(5) An authorised person must produce his or her identity card for inspection while acting as an authorised person if asked to do so by:
(a) the holder of the certificate of approval; or
(b) a person:
(i) who has control over any subject matter or thing specified in subregulation (4); or
(ii) who apparently has control over any subject matter or thing specified in subregulation (4).
(6) Where an authorised person:
(a) is acting as an authorised person; and
(b) under subregulation (4), seeks to carry out an inspection, conduct a test or require evidence to be furnished or is carrying out an inspection, conducting a test or requiring evidence to be furnished; and
(c) fails to produce his or her identity card for inspection when asked to do so;
that person:
(d) is not authorised to carry out the inspection, conduct the test or require evidence to be furnished; and
(e) if that person is carrying out one of those activities, must cease that activity immediately.
For subsection 98(5A) of the Act, CASA may issue a legislative instrument prescribing requirements for the provision of training and assessment in the maintenance of aircraft, aircraft components or aircraft materials by holders of certificates of approval under regulation 30.
(1) The holder of a certificate of approval may, in writing, request CASA to approve a proposed change to any of the particulars specified in the certificate, including the activities covered by the certificate.
(2) The request must have with it a copy of the proposed change.
(3) CASA must approve the change if CASA is satisfied that, if the certificate of approval is changed in the manner proposed, the holder of the certificate will carry out the activities covered by the certificate in a satisfactory manner.
(4) In deciding whether it is satisfied as mentioned in subregulation (3), CASA must have regard to the matters referred to in subregulation 30(2B).
CASA may specify in a certificate of approval the period during which the certificate is to remain in force.
(1) CASA may, at any time, require the holder of an airworthiness authority or an aircraft welding authority to undergo an examination designed to test his or her competency as such a holder.
(2) An authorised person may, at any time, inspect an aircraft or aircraft component for the purpose of ascertaining the competence and diligence of the holder of an airworthiness authority or an aircraft welding authority.
(1) CASA may, in writing and in accordance with the Civil Aviation Orders, issue authorities of the following kinds:
(a) authorities to carry out maintenance on aircraft;
(d) authorities to conduct non‑destructive testing of aircraft and aircraft components;
(e) authorities to weigh aircraft and determine the centre of gravity of each aircraft for the purpose of determining requirements to control the centre of gravity during operation.
(2) An airworthiness authority may be issued subject to conditions specified in the airworthiness authority, in Civil Aviation Orders or in both.
(3) If an airworthiness authority is issued subject to a condition in Civil Aviation Orders CASA must, in writing, notify the holder of the authority of the relevant Part or section of the Civil Aviation Orders in which the condition is specified.
(4) A person must not contravene a condition to which an airworthiness authority is subject.
Penalty: 50 penalty units.
(5) An offence against subregulation (4) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .(6) It is a defence to a prosecution under subregulation (4) if the defendant had a reasonable excuse.
Note: A defendant bears an evidential burden in relation to the matter in subregulation (6) (see subsection 13.3(3) of the
Criminal Code ).
(1) A person may apply to CASA for an aircraft welding authority to carry out manual welding of a type, and on a parent metal group, mentioned in regulation 29A.
(2) An application must identify the type of manual welding and the parent metal group to which the application relates.
(1) CASA may grant an application for an aircraft welding authority if, and only if, satisfied that:
(a) the applicant:
(i) has passed the aircraft welding examinations that CASA considers necessary in the interests of the safety of air navigation; and
(ii) has successfully completed welding training in the type of manual welding on the parent metal group to which the application relates; or
(b) the applicant holds a current qualification, issued by the Defence Force or a recognised authority, authorising the applicant to carry out manual welding for aeronautical purposes.
(2) Subject to this regulation, if an application is made for more than 1 type of manual welding and parent metal group, CASA may grant the application in respect of some of the types of manual welding and parent metal groups and refuse it in respect of others.
(3) CASA must not grant an application if satisfied, on reasonable grounds, that the applicant has knowingly or recklessly made a statement that is false or misleading in a material particular in relation to the application.
(5) CASA must not grant an aircraft welding authority except under this regulation.
(6) If CASA grants an aircraft welding authority, it must:
(a) note the relevant type of manual welding and parent metal group on the authority; and
(b) specify in the authority a period not longer than 2 years for which the authority is to remain in force.
(7) In this regulation:
recognised authority means an authority declared to be a recognised authority under regulation 33E.
(1) For the purposes of regulation 33D, CASA may, in writing, declare an authority of a foreign country which issues qualifications for aeronautical purposes to be a recognised authority.
(2) A declaration must be published in the
Gazette within 21 days after it is made.
(1) Unless sooner suspended or cancelled, an aircraft welding authority remains in force:
(a) for the period specified in it; or
(b) if it has been renewed—until the end of the last period of renewal.
(2) If an aircraft welding authority is cancelled, its holder must return it to CASA within 7 days after the cancellation.
Penalty: 5 penalty units.
(3) An offence against subregulation (2) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .(4) It is a defence to a prosecution under subregulation (2) if the defendant returned the aircraft welding authority to CASA as soon as practicable.
Note: A defendant bears an evidential burden in relation to the matter in subregulation (4) (see subsection 13.3(3) of the
Criminal Code ).
(1) The holder of an aircraft welding authority may apply to CASA for renewal of the authority within 3 months before the authority stops being in force.
(2) An application must have with it the aircraft welding authority.
(3) CASA may renew an aircraft welding authority for a period not longer than 2 years if, and only if, satisfied that the applicant has passed the aircraft welding examinations that CASA considers necessary in the interests of the safety of air navigation.
(4) CASA must not grant an application for renewal if satisfied, on reasonable grounds, that the applicant has knowingly or recklessly made a false or misleading statement in relation to the application.
(6) CASA must not renew an aircraft welding authority except under this regulation.
(7) If CASA renews an aircraft welding authority:
(a) it must note on the authority the period of the renewal; and
(b) return the authority to the holder as soon as practicable after the renewal.
(8) If an application is not decided before the aircraft welding authority to which it relates would, but for this subregulation, stop being in force, the authority is taken to be in force until the day the application is decided.
(1) The holder of an aircraft welding authority may request CASA to approve a proposed change to any of the particulars set out in the authority.
(2) A request must:
(a) be in the approved form; and
(b) have with it the aircraft welding authority.
(3) Subject to subregulation (4), CASA may approve the change if satisfied that the change will not have an adverse effect on the safety of air navigation.
(4) If the change involves adding a type of manual welding or parent metal group, CASA may approve the change if, and only if, satisfied that the holder:
(a) has passed the aircraft welding examinations that CASA considers necessary in the interests of the safety of air navigation; and
(b) has successfully completed welding training in the type of manual welding on the parent metal group to which the request relates.
(5) CASA must not approve a request for a change if satisfied, on reasonable grounds, that the holder has knowingly or recklessly made a false or misleading statement in relation to the request.
(7) CASA must not approve a change except under this regulation.
(8) If CASA approves a change to an aircraft welding authority, it must note the change on the authority.
(9) CASA must return an aircraft welding authority to its holder as soon as practicable after a request to approve a change is decided.
(1) An aircraft welding authority is subject to any conditions that CASA considers necessary to impose in the interests of the safety of air navigation.
(2) A condition must be set out in the aircraft welding authority.
(3) The holder of an aircraft welding authority must not contravene a condition set out in the authority.
Penalty: 50 penalty units.
(4) An offence against subregulation (3) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .(5) It is a defence to a prosecution under subregulation (3) if the defendant had a reasonable excuse.
Note: A defendant bears an evidential burden in relation to the matter in subregulation (5) (see subsection 13.3(3) of the
Criminal Code ).
(1) CASA may, for the purposes of these Regulations, approve a defect in, an Australian aircraft, or any aircraft included in a class of aircraft, as a permissible unserviceability in relation to the aircraft or to Australian aircraft included in the class of aircraft, as the case may be.
(2) CASA may, for the purpose of ensuring the safety of air navigation, direct that the use of an Australian aircraft with a permissible unserviceability is subject to such conditions as are set out in the direction.
(2A) A person must comply with a condition set out in a direction.
Penalty: 50 penalty units.
(2B) An offence against subregulation (2A) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .(3) A direction given under subregulation (2) does not have effect in relation to a person until it has been served on the person.
(1) CASA may give directions relating to the maintenance of Australian aircraft for the purpose of ensuring the safety of air navigation.
(2) A direction is not binding on a person unless it has been served on the person.
(3) A person must not contravene a direction that is binding on the person.
Penalty: 50 penalty units.
(4) If a direction relating to an aircraft is binding on the holder of the certificate of registration for the aircraft, the holder must take reasonable steps to ensure the direction is brought to the attention of any person who is likely to fly, or issue a maintenance release for, the aircraft.
Penalty: 50 penalty units.
(5) An offence against subregulation (3) or (4) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .
(1) The holder of the certificate of registration for a class A aircraft must ensure that all maintenance required to be carried out on the aircraft (including any aircraft components from time to time included in or fitted to the aircraft) by the aircraft’s approved system of maintenance is carried out when required by that system.
Penalty: 50 penalty units.
(2) A person must not use a class A aircraft in an operation if there is not an approved system of maintenance for the aircraft that includes provision for the maintenance of all aircraft components from time to time included in, or fitted to, the aircraft.
Penalty: 50 penalty units.
Note: A system of maintenance is approved under regulation 42M.
(3) An offence against subregulation (1) or (2) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .
If the approved system of maintenance for a class A aircraft is:
(a) no longer appropriate; or
(b) defective;
within 7 days of becoming aware of the inappropriate aspect or the defect, the holder of the certificate of registration for the aircraft must make a request under regulation 42P for CASA or an authorised person to approve changes to the system to ensure that it is appropriate and not defective.
Penalty: 25 penalty units.
(1) The holder of the certificate of registration for a class B aircraft must ensure that all maintenance required to be carried out on the aircraft (including any aircraft components from time to time included in or fitted to the aircraft) by the aircraft’s maintenance schedule is carried out when required by that schedule.
Penalty: 50 penalty units.
(2) A person must not use a class B aircraft in an operation if there is not a maintenance schedule for the aircraft that includes provision for the maintenance of all aircraft components from time to time included in, or fitted to, the aircraft.
Penalty: 50 penalty units.
(3) An offence against subregulation (1) or (2) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .
If the maintenance schedule for a class B aircraft is defective or no longer appropriate, the holder of the certificate of registration for the aircraft, within 7 days after becoming aware of the defect, or that the schedule is inappropriate, must report the situation to CASA and take one of the following actions to ensure that the aircraft has a maintenance schedule that is appropriate and not defective:
(a) if the aircraft’s maintenance schedule is the manufacturer’s maintenance schedule:
(i) elect to use the CASA maintenance schedule as the aircraft’s maintenance schedule; or
(ii) under regulation 42J, request CASA or an authorised person to approve a system of maintenance for the aircraft;
(b) if the aircraft’s maintenance schedule is the CASA maintenance schedule:
(i) elect to use the manufacturer’s maintenance schedule as the maintenance schedule for the aircraft; or
(ii) under regulation 42J, request CASA or an authorised person to approve a system of maintenance for the aircraft;
(c) if the aircraft’s maintenance schedule is an approved system of maintenance:
(i) under regulation 42P, request CASA to approve a proposed change to the system; or
(ii) elect to use the manufacturer’s maintenance schedule as the maintenance schedule for the aircraft; or
(iii) elect to use the CASA maintenance schedule as the maintenance schedule for the aircraft.
Penalty: 25 penalty units.
(1) Subject to subregulations (2), (3), (4) and (5), if:
(a) the holder of the certificate of registration for a class B aircraft has elected to use a manufacturer’s maintenance schedule for the aircraft’s maintenance; and
(b) the election is in force; and
(c) use of the manufacturer’s maintenance schedule for the aircraft’s maintenance is not prohibited by a declaration under subregulation (6);
the aircraft’s maintenance schedule is the manufacturer’s maintenance schedule as in force from time to time.
(2) If CASA thinks that a manufacturer’s maintenance schedule should not, alone, be used as an aircraft’s maintenance schedule because the manufacturer’s maintenance schedule is deficient in a particular respect, the following provisions have effect:
(a) CASA may, for the purpose of remedying the deficiency, do either or both of the following:
(i) give directions under subregulation 38(1) to be complied with in relation to aircraft in addition to the requirements of the manufacturer’s maintenance schedule;
(ii) give directions under subregulation 38(1) requiring the holders of certificates of registration for aircraft to prepare documents to be complied with in relation to aircraft in addition to the requirements of the manufacturer’s maintenance schedule;
(b) if an election to use the manufacturer’s maintenance schedule as an aircraft’s maintenance schedule is in force:
(i) any directions under subparagraph (a)(i) in force in relation to the manufacturer’s maintenance schedule are to be taken to form part of the aircraft’s maintenance schedule and the election has effect accordingly; and
(ii) any documents prepared because of a direction under subparagraph (a)(ii) in force in relation to the manufacturer’s maintenance schedule are to be taken to form part of the aircraft’s maintenance schedule and the election has effect accordingly.
(3) If:
(a) a person has elected to use a manufacturer’s maintenance schedule for an aircraft’s maintenance; and
(b) either:
(i) the aircraft has been modified or repaired; or
(ii) an aircraft component included in, or fitted to, the aircraft has been modified or repaired;
all instructions for the continued airworthiness of the aircraft, or of the component, as the case requires, issued by the designer of the modification or repair are to be taken to form part of the manufacturer’s maintenance schedule and the election has effect accordingly.
(4) If a person has elected to use a manufacturer’s maintenance schedule for an aircraft’s maintenance, all instructions issued by the manufacturers of aircraft components permanently, or from time to time, included in, or fitted to, the aircraft, being instructions for the continued airworthiness of the components, are to be taken to form part of the manufacturer’s maintenance schedule and the election has effect accordingly.
(5) If:
(a) a person has elected to use a manufacturer’s maintenance schedule for an aircraft’s maintenance; and
(b) the manufacturer’s maintenance schedule does not include provisions equivalent to the sections of the CASA maintenance schedule that deal with the maintenance of electrical, instrument and radio systems;
those sections of the CASA maintenance schedule are to be taken to form part of the manufacturer’s maintenance schedule and the election has effect accordingly.
(6) CASA may, for the purpose of ensuring the safety of air navigation, declare in writing that a manufacturer’s maintenance schedule that CASA thinks is inadequate must not be used as an aircraft’s maintenance schedule.
(1) Subject to subregulation (2), if:
(a) the holder of the certificate of registration for a class B aircraft that is an aeroplane has elected to use the CASA maintenance schedule for the aircraft’s maintenance; and
(b) the election is in force;
the aircraft’s maintenance schedule is the CASA maintenance schedule.
(2) If:
(a) a person has elected to use the CASA maintenance schedule for an aircraft’s maintenance; and
(b) a turbine engine is included in the aircraft;
all instructions issued by the manufacturer of the engine for the continued airworthiness of the engine are to be taken to form part of the CASA maintenance schedule and the election has effect accordingly.
If:
(a) CASA or an authorised person has approved a system of maintenance for a class B aircraft under regulation 42M; and
(b) the approval is in force;
the aircraft’s maintenance schedule is the approved system of maintenance.
(1) The maintenance schedule for a class B aircraft certificated under subpart 21.B or 21.H of Part 21 of CASR in the primary, intermediate, restricted or limited category (except an aircraft mentioned in subparagraph 21.189(1)(a)(ii) of CASR) is the approved maintenance schedule developed in consultation with CASA during the certification process.
(2) The maintenance schedule for an aircraft mentioned in subparagraph 21.189(1)(a)(ii) of CASR is the approved maintenance schedule developed, in consultation with CASA or a limited category organisation, by the applicant for the special certificate of airworthiness for the aircraft under regulation 21.189 of CASR.
(3) For this regulation, an aircraft is certificated in a particular category if it was manufactured in accordance with a type certificate in the category, or if a certificate of airworthiness in the category is in force for the aircraft.
The holder of the certificate of registration for a class B aircraft that is an experimental aircraft must maintain the aircraft in accordance with any conditions to which the certificate is subject under regulation 21.195A of CASR.
If, apart from this regulation, there would be more than one maintenance schedule for an aircraft, the maintenance schedule for the aircraft is:
(a) if:
(i) CASA has approved a system of maintenance for the aircraft under regulation 42M; and
(ii) the system was submitted for approval because of a direction by CASA; and
(iii) the approval is still in force;
that approved system of maintenance; and
(b) in any other case—the maintenance schedule that the holder of the certificate of registration for the aircraft has most recently elected to use, or that CASA has most recently approved, as the case may be.
(1) An election made for the purposes of subregulation 42A(1) or 42B(1) must be made by completing the appropriate approved form and giving it to CASA.
(2) An election stops being in force if the person who made it revokes it by written notice given to CASA.
If there is a change of holder of the certificate of registration for a class B aircraft, an election under subregulation 42A(1) or 42B(1) that was in force immediately before the change has effect (including for the purposes of subregulation 42E(2)) after the change as if it had been made by the new holder.
(1) This regulation sets out the additional requirements to be complied with if any part of the flight control system of an Australian aircraft is assembled, adjusted, repaired, modified or replaced in the course of carrying out maintenance on the aircraft.
(2) Subject to subregulation (4), the system must:
(a) be inspected by the person who carried out the assembly, adjustment, repair, modification or replacement; and
(b) be independently inspected by another person who is an appropriate person within the meaning of subregulation (5).
(3) A person carrying out an inspection must:
(a) check that the assembly, adjustment, repair, modification or replacement was carried out in accordance with the aircraft’s approved maintenance data; and
(b) check that the system functions correctly.
(4) In spite of subregulation (2), if:
(a) optional dual controls were connected or disconnected without using tools; and
(b) no other part of the flight control system was assembled, adjusted, repaired, modified or replaced;
the system does not have to be independently inspected.
(5) For the purposes of this regulation, a person is an appropriate person if:
(a) the person holds an aircraft maintenance engineer licence or an airworthiness authority covering maintenance of a type that includes the inspection; or
(b) the person is the holder of a pilot licence that is valid for the aircraft; or
(c) the person is the holder of a flight engineer licence that is valid for the aircraft; or
(d) the person is authorised by CASA or an authorised person under subregulation (6) to carry out the inspection and the inspection is carried out in accordance with any conditions subject to which the authorisation was given; or
(e) in relation to an independent inspection performed overseas—the person is a person referred to in paragraph 42ZN(a).
(6) CASA or an authorised person may, in writing, authorise a person for the purposes of paragraph (5)(d).
(7) An authorisation is subject to any conditions that:
(a) CASA or the authorised person, as the case may be, considers are necessary in the interests of the safety of air navigation; and
(b) are included in the authorisation.
This Division has effect subject to Division 7 (‘Exemptions from, and variations of, requirements’).
(1) The holder of the certificate of registration for an Australian aircraft may, in writing, request CASA or an authorised person to approve a system of maintenance for the aircraft.
(2) The request must be accompanied by a copy of the system.
CASA may, under regulation 38, direct the holder of the certificate of registration for a class B aircraft:
(a) to develop a system of maintenance for the aircraft; and
(b) to submit the proposed system to CASA for approval.
A system of maintenance for an aircraft must include:
(a) a schedule that:
(i) sets out the regular maintenance inspections, tests and checks to be carried out on the aircraft; and
(ii) sets out when those maintenance inspections, tests and checks are to be carried out; and
(iii) nominates one of the maintenance inspections referred to in subparagraph (i) as the inspection to be carried out for the purposes of determining whether a maintenance release should be issued for the aircraft; and
(b) a schedule that sets out the inspection to be carried out on the aircraft if it has been struck by lightning and when that inspection is to be carried out; and
(c) a schedule that sets out the inspection to be carried out on the aircraft if abnormal flight or ground loads have been imposed on the aircraft; and
(d) a schedule that sets out the time‑lifed aircraft components included in the aircraft and when each of those components is to be retired, overhauled or removed; and
(e) a schedule that sets out the procedures to be followed in carrying out the inspections, tests and checks required by the system of maintenance; and
(f) if permissible unserviceabilities have been approved for the aircraft under subregulation 37(1) in the form of a minimum equipment list—that list; and
(g) a statement that sets out:
(i) the name of the holder of the certificate of registration for the aircraft; and
(ii) the type, model and registration mark of the aircraft.
(1) If:
(a) CASA or an authorised person receives a request for approval of a system of maintenance; and
(b) CASA or the authorised person is satisfied that:
(i) the system includes the matters set out in regulation 42L; and
(ii) the system adequately provides for the continued airworthiness of the aircraft;
CASA or the authorised person must approve the system.
(2) If, because of a direction of a kind referred to in regulation 42K, the holder of the certificate of registration for an aircraft submits a system of maintenance to CASA, the following provisions have effect:
(a) if CASA is satisfied that:
(i) the system includes the matters set out in regulation 42L; and
(ii) the system satisfies the requirements of the direction; and
(iii) the system adequately provides for the continued airworthiness of the aircraft;
CASA must approve the system;
(b) if CASA is not satisfied as mentioned in paragraph (a), CASA may:
(i) modify the system so that CASA is so satisfied and approve the modified system; or
(ii) refuse to approve the system.
(3) In deciding whether a system of maintenance adequately provides for the continued airworthiness of an aircraft, CASA or the authorised person must have regard to:
(a) if the system of maintenance relates to a class A aircraft—the manufacturer’s maintenance schedule and any inspection programs or documents issued by the manufacturer; and
(b) if the system of maintenance relates to a class B aircraft—the manufacturer’s maintenance schedule and the CASA maintenance schedule.
(4) CASA or the authorised person must, in writing, notify the holder of the certificate of registration for the aircraft concerned of CASA’s, or the authorised person’s, decision in relation to the system submitted.
(5) If CASA or the authorised person decides:
(a) not to approve the system of maintenance; or
(b) to modify the system of maintenance;
CASA or the authorised person must include in the notice required by subregulation (4) a statement of the reasons for that decision.
(1) If CASA or an authorised person approves a system of maintenance, the approval has effect from when notice of the approval is given to the holder of the certificate of registration for the aircraft concerned.
(2) An approval of a system of maintenance approved because of a request under regulation 42J stops being in force if:
(a) CASA revokes the approval by written notice given to the holder of the certificate of registration for the aircraft concerned; or
(b) the holder of the certificate of registration for the aircraft concerned gives CASA or an authorised person written notice that the holder no longer wants the approved system to apply to the aircraft.
(3) An approval of a system of maintenance submitted because of a direction of a kind referred to in regulation 42K stops being in force if CASA revokes the approval by written notice given to the holder of the certificate of registration for the aircraft concerned.
(4) CASA must not revoke an approval of a system of maintenance unless CASA thinks it is necessary to do so for the purpose of ensuring the safety of air navigation.
(1) The holder of the certificate of registration for an aircraft for which there is an approved system of maintenance may, in writing, request CASA or an authorised person to approve a proposed change to the system.
(2) The request must be accompanied by a copy of the proposed change.
CASA may, under regulation 38, direct the holder of the certificate of registration for an aircraft for which there is an approved system of maintenance:
(a) to make:
(i) a specified change to the system; or
(ii) a change to the system that will correct a specified deficiency in the system; and
(b) to submit the proposed change to CASA or an authorised person for approval.
(1) If:
(a) CASA or an authorised person receives a request for approval of a change to an approved system of maintenance; and
(b) CASA or the authorised person is satisfied that the system, as proposed to be changed, would:
(i) include the matters set out in regulation 42L; and
(ii) adequately provide for the continued airworthiness of the aircraft;
CASA or the authorised person must approve the change.
(2) If, because of a direction of a kind referred to in regulation 42Q, the holder of the certificate of registration for an aircraft submits a proposed change to an approved system of maintenance to CASA, the following provisions have effect:
(a) if CASA is satisfied:
(i) if the direction was for a specified change to be made—the change has been made; and
(ii) if the direction was for a change to correct a specified deficiency in the system—the deficiency would be corrected by the change; and
(iii) that the system, as proposed to be amended, would:
(A) include the matters set out in regulation 42L; and
(B) adequately provide for the continued airworthiness of the aircraft;
CASA must approve the change;
(b) if CASA is not satisfied as mentioned in paragraph (a), CASA may:
(i) modify the change so that CASA is so satisfied and approve the modified change; or
(ii) refuse to approve the change.
(3) In deciding whether a system of maintenance as proposed to be changed would adequately provide for the continued airworthiness of an aircraft, CASA or the authorised person must have regard to:
(a) if the system of maintenance relates to a class A aircraft—the manufacturer’s maintenance schedule and any inspection programs or documents issued by the manufacturer; and
(b) if the system of maintenance relates to a class B aircraft—the manufacturer’s maintenance schedule and the CASA maintenance schedule.
(4) CASA or the authorised person must, in writing, notify the holder of the certificate of registration for the aircraft concerned of CASA’s, or the authorised person’s, decision in relation to the change submitted.
(5) If CASA or the authorised person decides:
(a) not to approve the change; or
(b) to modify the change;
CASA or the authorised person must include in the notice required by subregulation (4) a statement of the reasons for that decision.
If CASA or an authorised person approves a change to an approved system of maintenance, the approval has effect from when notice of the approval is given to the holder of the certificate of registration for the aircraft concerned.
A purported change to an approved system of maintenance has no effect unless it has been approved under regulation 42R and that approval is in force.
(1) A person may modify or repair an Australian aircraft only if:
(a) the design of the modification or repair:
(i) has been approved under regulation 35, as in force before 27 June 2011; or
(ia) has been approved by a modification/repair design approval; or
(ib) has been approved by an approval mentioned in regulation 21.475 of CASR; or
(ic) is taken to have been approved under regulation 21.465 or 21.470 of CASR; or
(ii) has been specified by CASA in, or by means of, an airworthiness directive or a direction under regulation 44; or
(iii) is specified in the aircraft’s approved maintenance data; and
(b) the modification or repair is in accordance with that design.
Penalty: 50 penalty units.
(2) An offence against subregulation (1) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .
(1) A person carrying out maintenance on an Australian aircraft must ensure that the maintenance is carried out in accordance with the applicable provisions of the aircraft’s approved maintenance data.
Penalty: 50 penalty units.
Note: Regulation 2A sets out what is approved maintenance data for an aircraft.
(2) Subregulation (1) has effect subject to the requirements of Division 5 (‘Who may carry out maintenance’).
(3) An offence against subregulation (1) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .
(1) This regulation sets out requirements to be complied with in relation to the installation and use of aircraft components in carrying out maintenance on an Australian aircraft in Australian territory.
(2) Subject to subregulation (3), a person may replace an aircraft component in the aircraft with another aircraft component only if:
(a) the replacement component is serviceable; and
(b) the replacement component:
(i) is identical with the replaced component; or
(ii) has been approved under regulation 36, as in force before 27 June 2011, as a replacement for the replaced component; or
(iii) is approved for use as a replacement for the replaced component:
(A) by the manufacturer of the aircraft or the replaced component; or
(AA) in an Australian Parts Manufacturer Approval issued under regulation 21.303 of CASR; or
(B) in a Parts Manufacturers Approval issued by the Federal Aviation Administration of the United States of America; or
(BA) in a parts manufacturer approval issued by a national aviation authority to which subregulation (2A) applies; or
(C) by a modification/repair design approval; or
(D) by an approval mentioned in regulation 21.475 of CASR; or
(iv) is taken to have been approved for use as a replacement for the replaced component under regulation 21.465 or 21.470 of CASR; and
(c) if the replacement component has been removed or salvaged from another aircraft and has not had maintenance carried out on it—the replacement component is not damaged and complies with its manufacturer’s specifications.
Penalty: 50 penalty units.
(2A) For sub‑subparagraph (2)(b)(iii)(BA), this subregulation applies to the national aviation authority of a Contracting State if:
(a) Australia has an agreement (however described) with the Contracting State for the acceptance of parts manufacturer approvals; or
(b) CASA has an agreement (however described) with the national aviation authority for the acceptance of parts manufacturer approvals.
(3) A person may replace an aircraft component in the aircraft with another aircraft component that does not satisfy the requirements of paragraphs (2)(a) and (c) if inclusion of the replacement component in the aircraft amounts to a permissible unserviceability in the aircraft that is approved under regulation 37.
(4) Subject to regulations 42Y and 42Z, a person must not install an aircraft component in an aircraft if each of the following requirements is not satisfied:
(a) if the component, or a component that it incorporates, was manufactured in the course of carrying out maintenance—the completion of the maintenance was certified in accordance with regulation 42ZE or 42ZN;
(b) if the component, or another aircraft component that is incorporated in it, has had maintenance carried out on it—completion of the maintenance was certified in accordance with regulation 42ZE or 42ZN;
(c) if the component, or another aircraft component that is incorporated in it, has been modified or repaired—the modification or repair was carried out in accordance with a design that:
(i) was approved under regulation 35, as in force before 27 June 2011; or
(ia) was approved by a modification/repair design approval; or
(ib) was approved by an approval mentioned in regulation 21.475 of CASR; or
(ic) is taken to have been approved under regulation 21.465 or 21.470 of CASR; or
(ii) was specified by CASA in, or by means of, an airworthiness directive or a direction under regulation 44 or subregulation 21.176(2) of CASR; or
(iii) was specified in the component’s, or the incorporated component’s, approved maintenance data; or
(iv) if the modification or repair was carried out outside Australian territory—was approved or specified in a manner that is acceptable to CASA having regard to the safety of air navigation;
(d) if subregulation (5) applies to the component, and the component was supplied by another person—the supplier of the component supplied an authorised release certificate with it and for it;
(e) if the component includes a component to which subregulation (5) applies, and the included component was supplied by another person—the supplier of the included component supplied an authorised release certificate with it and for it.
Penalty: 50 penalty units.
Note:
Authorised release certificate means a certificate that complies with regulation 42WA—see the Dictionary.(5) This subregulation applies to:
(a) an aircraft component manufactured to approved data by a manufacturer that holds an approval from CASA or a national aviation authority to do so; or
(b) an aircraft component that has had maintenance carried out on it.
(6) An offence against subregulation (2) or (4) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .
(1) The requirements for an authorised release certificate for an aircraft component are the following:
(a) it has a unique identifying number;
(b) it is issued by, or with the authority or approval of:
(i) if maintenance has been carried out on the relevant component—the national aviation authority of the country in which the most recent maintenance was carried out; or
(ii) if no maintenance has been carried out on the component—the national aviation authority of the country in which it was manufactured;
(c) it specifies the national aviation authority that issued it or that authorised its issue;
(d) it contains at least the following information about the component (or, if it applies to 2 or more components, about each of them):
(i) the full name and business address of the supplier of the component;
(ii) enough information to identify the contract, work order or invoice related to the supply of the component;
(iii) the component’s name or description, and part number;
(iv) the types or models of aircraft, propeller or engine on which the component can be installed (if known to the body issuing the certificate);
(v) the serial number or batch number of the component;
(vi) the component’s status (that is, whether it is manufactured or newly overhauled, or has been inspected, modified or repaired, or is a prototype) and a statement of any limitations that apply to it;
(e) if the certificate applies to 2 or more components, it gives an identifying number for each;
(f) if the certificate applies to 2 or more components that have the same part number, it states how many of them the certificate applies to;
(g) it quotes or identifies the authorisation under which it is issued;
(h) the person who signed it is a proper person to do so, in accordance with subregulation (2), (3) or (4).
(2) A person is a proper person to sign an authorised release certificate for a component on which maintenance has been carried out in Australia if:
(a) he or she is permitted by regulation 42ZC to carry out the maintenance; and
(b) he or she is employed by, or is working under an arrangement with, the person who carried out the most recent such maintenance.
(3) A person is a proper person to sign an authorised release certificate for a component on which maintenance has been carried out in a country other than Australia if:
(a) he or she is permitted to carry out the maintenance by the national aviation authority of the country in which that maintenance was carried out; and
(b) he or she carried out the most recent such maintenance, or is employed by, or works under an arrangement with, the person who did so.
(4) A person is a proper person to sign an authorised release certificate for a component on which no maintenance has been carried out if he or she is the manufacturer of the component, or is employed by, or works under an arrangement with, its manufacturer.
Note: A document that complies with regulation 42WA is an authorised release certificate. Appendix 1 to Civil Aviation Order 100.16 gives a list of documents issued in foreign countries that, if completed correctly, will be authorised release certificates. Civil Aviation Advisory Publication 42W‑1 sets out documents necessary for the supply of components, parts and material. Also, Civil Aviation Advisory Publication 42W‑2 explains how to prepare a certificate. Both the Order and the Advisory Publications are available on CASA’s website.
(1) A person may use an aircraft material in an aircraft only if the person satisfies CASA or an authorised person that the material is suitable for use in the maintenance of the aircraft or the following requirements are satisfied:
(a) if:
(i) the material was supplied to the person by another person; and
(ii) the material is not a fuel or lubricant;
the material was supplied by the other person with a document that satisfies the requirements of subregulation (2);
(b) if the material has had maintenance carried out on it—completion of the maintenance was certified in accordance with regulation 42ZE or 42ZN.
Penalty: 50 penalty units.
(2) A document accompanying the supply of an aircraft material must:
(a) contain:
(i) a statement that identifies the material and that includes (if applicable) the specification of the material; and
(ii) if maintenance has been carried out on the material—details of the maintenance carried out and the data used in carrying out the maintenance; and
(b) have been issued by, or with the authority or approval of:
(i) if maintenance has been carried out on the material—the national aviation authority of the country in which the most recent maintenance was carried out; or
(ii) if no maintenance has been carried out on the material—the national aviation authority of the country in which the material was manufactured; and
(c) be signed by:
(i) if maintenance has been carried out on the material in Australia—a person who is permitted by regulation 42ZC to carry out the maintenance and who is employed by, or is working under an arrangement with, the person who carried out the most recent maintenance; or
(ii) if maintenance has been carried out on the material in a country other than Australia—a person who is permitted to carry out the maintenance by the national aviation authority of the country in which that maintenance was carried out and who is, is employed by, or is working under an arrangement with, the person who carried out the most recent maintenance; or
(iii) if no maintenance has been carried out on the material—a person who is, is employed by, or is working under an arrangement with, the person who manufactured the material; and
(d) set out the date on which the person signed the document.
(3) An offence against subregulation (1) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .
If a person satisfies CASA or an authorised person that there is a complete record of the airworthiness history of a time‑lifed aircraft component, the person may install the component in an aircraft even though the requirements of paragraphs 42W(4)(a) and (b) are not satisfied.
(1) This regulation applies to an aircraft:
(a) that has a flight manual; and
(b) that is not, in that manual, approved for use in IFR flight.
(2) Subject to subregulation (3), if:
(a) a removable item of radiocommunications equipment is installed in an aircraft; and
(b) that item is removed from the aircraft;
a person may re‑install that item, or install another item of the same type, in the aircraft even though the requirements of paragraphs 42W(4)(c) and (d) are not satisfied.
(3) If the person is not the holder of the certificate of registration for the aircraft, subregulation (2) does not apply unless the holder has approved the installation of the equipment.
(1) This regulation applies to the holder of the certificate of registration for, or the operator or pilot in command of, an Australian aircraft while the aircraft is outside Australian territory.
(2) A person to whom this regulation applies must not use, or permit the use of, an aircraft component, aircraft material or other thing in connection with the maintenance of the aircraft if:
(a) use of the component, material or thing would be an offence against these Regulations if the aircraft were in Australian territory; and
(b) CASA has not approved the use.
Penalty: 50 penalty units.
(3) An offence against subregulation (2) is an offence of strict liability.
Note: For
strict liability , see section 6.1 of theCriminal Code .
This Division has effect subject to Division 7 (‘Exemptions from, and variations of, requirements’).
(1) The holder of the certificate of registration for, the operator of, and the pilot in command of, an Australian aircraft must not authorise or permit any maintenance to be carried out on the aircraft in Australian territory by a person if the person is not permitted by this regulation to carry out the maintenance.
rep F2021L00200 | |
r 244.......................................... | am No 147, 1991; No 173, 1994; No 224, 1995; No 201, 2003 |
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r 245.......................................... | am No 147, 1991; No 173, 1994; No 224, 1995; No 201, 2003 |
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r 246.......................................... | am No 147, 1991; No 173, 1994; No 201, 2003 |
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r 247.......................................... | am No 147, 1991; No 173, 1994; No 201, 2003 |
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r 248.......................................... | am No 147, 1991; No 173, 1994; No 224, 1995; No 201, 2003; No 80, 2013 |
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r 248A....................................... | ad No 70, 2007 |
rep F2021L00200 | |
r 249.......................................... | am No 147, 1991; No 279, 1992; No 173, 1994; No 201, 2003; No 5, 2013; No 274, 2013 |
rep F2021L00200 | |
r 250.......................................... | am No 376, 1988; No 147, 1991; No 173, 1994; No 224, 1995; No 201, 2003 |
rep F2021L00200 | |
r 251.......................................... | am No 289, 1990; No 147, 1991; No 342, 1992; No 173, 1994; No 224, 1995; No 201, 2003 |
rep F2021L00200 | |
r 252.......................................... | am No 289, 1990; No 147, 1991; No 173, 1994; No 224, 1995; No 201, 2003 |
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r 252A....................................... | ad No 294, 1994 |
am No 147, 1995; No 224, 1995 | |
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am No 219, 1998; No 201, 2003; No 345, 2004; No 238, 2008 | |
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r 254.......................................... | am No 147, 1991; No 173, 1994; No 224, 1995; No 201, 2003 |
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r 255.......................................... | am No 342, 1992; No 173, 1994; No 224, 1995; No 201, 2003 |
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r 256.......................................... | am No 147, 1991; No 173, 1994; No 294, 2000; No 201, 2003 |
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r 256AA..................................... | ad No 174, 1992 |
am No 173, 1994; No 201, 2003 | |
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r 256A....................................... | ad No 331, 1990 |
am No 147, 1991; No 410, 1991; No 382, 1994; No 224, 1995; No 201, 2003 | |
rep F2021L00200 | |
r 257.......................................... | rs No 466, 1990 |
am No 173, 1994; No 224, 1995; No 201, 2003 | |
rep F2021L00200 | |
r 258.......................................... | am No 147, 1991; No 342, 1992; No 173, 1994; No 224, 1995; No 201, 2003 |
rep F2021L00200 | |
r 259.......................................... | am No 147, 1991; No 173, 1994; No 224, 1995; No 349, 2001 (as am by No 79, 2002); No 201, 2003; No 345, 2004 |
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r 260.......................................... | am No 147, 1991; No 287, 1991; No 410, 1991; No 173, 1994; No 224, 1995; No 349, 2001 (as am by No 79, 2002); No 201, 2003 |
rs No 201, 2003 | |
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r 261.......................................... | am No 147, 1991; No 173, 1994; No 224, 1995 |
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r 262.......................................... | am No 147, 1991; No 173, 1994; No 224, 1995; No 201, 2003 |
Division 5.................................. | ad No 219, 1998 |
rs No 213, 2012 | |
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am No 229, 1999; No 70, 2007 | |
rs No 213, 2012 | |
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am No 261, 2000; No 362, 2000; No 201, 2003; No 184, 2006 | |
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r 262AI...................................... | ad No 219, 1998 |
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rs No 213, 2012 | |
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r 262AJ...................................... | ad No 219, 1998 |
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rs No 213, 2012 | |
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r 262AJA................................... | ad No 213, 2012 |
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r 262AJB.................................... | ad No 213, 2012 |
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r 262AJC.................................... | ad No 213, 2012 |
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Division 6.................................. | ad No 235, 1998 |
r 262AK..................................... | ad No 235, 1998 |
am No 350, 2002 | |
rs No 321, 2005 | |
am F2016L01655 | |
r 262AL..................................... | ad No 235, 1998 |
am No 166, 1999; No 204, 2000; No 350, 2002; No 201, 2003; No 5, 2013 | |
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r 262AM.................................... | ad No 235, 1998 |
am No 166, 1999; No 204, 2000; No 227, 2000; No 350, 2002; No 201, 2003; No 5, 2013 | |
rep F2016L01655 | |
r 262AN..................................... | ad No 235, 1998 |
am No 350, 2002; No 201, 2003; No 80, 2013 | |
rs F2016L01655 | |
r 262AO..................................... | ad No 235, 1998 |
am No 204, 2000; No 350, 2002; No 201, 2003 | |
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r 262AP..................................... | ad No 235, 1998 |
am No 166, 1999; No 204, 2000; No 350, 2002; No 201, 2003; No 137, 2005; No 5, 2013 | |
rep F2021L00200 | |
r 262APA................................... | ad No 321, 2005 |
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r 262AQ..................................... | ad No 235, 1998 |
am No 201, 2003; No 328, 2010 | |
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r 262AR..................................... | ad No 235, 1998 |
am No 201, 2003; No 328, 2010 | |
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r 262AS..................................... | ad No 235, 1998 |
rs No 201, 2003 | |
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Part 15....................................... | ad No 410, 1991 |
rep No 365, 2003 | |
r 262A....................................... | ad No 410, 1991 |
rep No 365, 2003 | |
r 262B........................................ | ad No 410, 1991 |
am No 224, 1995 | |
rep No 365, 2003 | |
r 262C........................................ | ad No 410, 1991 |
rep No 365, 2003 | |
r 262D....................................... | ad No 410, 1991 |
rs No 95, 2003 | |
rep No 365, 2003 | |
r 262E........................................ | ad No 410, 1991 |
am No 224, 1995; No 95, 2003 | |
rep No 365, 2003 | |
r 262EA..................................... | ad No 93, 1994 |
am No 224, 1995 | |
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r 262EB..................................... | ad No 95, 2003 |
rep No 365, 2003 | |
r 262F........................................ | ad No 410, 1991 |
am No 224, 1995; No 95, 2003 | |
rep No 365, 2003 | |
r 262G....................................... | ad No 410, 1991 |
rep No 365, 2003 | |
r 262H....................................... | ad No 410, 1991 |
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r 262J......................................... | ad No 410, 1991 |
am No 224, 1995; No 95, 2003 | |
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r 262K....................................... | ad No 410, 1991 |
am No 95, 2003 | |
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r 262M....................................... | ad No 410, 1991 |
rep No 365, 2003 | |
r 262N....................................... | ad No 410, 1991 |
rep No 365, 2003 | |
r 262P........................................ | ad No 410, 1991 |
am No 93, 1994 | |
rep No 365, 2003 | |
r 262Q....................................... | ad No 410, 1991 |
rep No 365, 2003 | |
r 262R........................................ | ad No 410, 1991 |
rep No 365, 2003 | |
r 262S........................................ | ad No 410, 1991 |
rep No 365, 2003 | |
r 262T........................................ | ad No 410, 1991 |
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r 262TA..................................... | ad No 342, 1992 |
am No 173, 1994; No 224, 1995; No 201, 2003 | |
rep No 365, 2003 | |
r 262U....................................... | ad No 410, 1991 |
am No 224, 1995 | |
rep No 365, 2003 | |
r 262V....................................... | ad No 410, 1991 |
am No 224, 1995 | |
rep No 365, 2003 | |
Part 16 heading........................... | am No 93, 1994 |
rs No 328, 2010 | |
r 263.......................................... | am No 279, 1992; No 417, 1992; No 93, 1994; No 353, 1999; No 167, 2002; No 345, 2004; No 328, 2010; No 5, 2013; No 80, 2013; F2016L01655; F2018L01030; F2021L00200 |
r 264.......................................... | am No 174, 1992; No 279, 1992; No 417, 1992; No 224, 1995; No 345, 2004; No 328, 2010; No 77, 2011; No 80, 2013 |
rs No 5, 2013 | |
r 265.......................................... | am No 373, 1988; No 216, 1990; No 279, 1992; No 380, 1992; No 93, 1994; No 224, 1995; No 319, 2002; No 328, 2010; No 5, 2013 |
r 266.......................................... | am No 417, 1992; No 93, 1994; No 224, 1995; No 345, 2004 |
rep No 77, 2011 | |
r 267.......................................... | am No 93, 1994; No 224, 1995; No 328, 2010 |
r 268.......................................... | am No 215, 1990; No 93, 1994; No 224, 1995 |
rep Act No 105, 2003 | |
r 269.......................................... | am No 93, 1994; No 224, 1995; No 210, 1999; Act No 105, 2003; No 191, 2008; No 328, 2010; No 80, 2013 |
r 270.......................................... | am No 93, 1994; No 328, 2010 |
r 271.......................................... | rep No 215, 1990 |
r 272.......................................... | am No 93, 1994; No 224, 1995 |
rep No 236, 1998 | |
r 272A....................................... | ad No 310, 1990 |
rep No 287, 1991 | |
ad No 279, 1992 | |
am No 93, 1994; No 224, 1995; No 328, 2010; No 5, 2013; No 188, 2013 | |
Part XV...................................... | rep No 224, 1995 |
r 273.......................................... | am No 224, 1995 |
rep No 224, 1995 | |
r 274.......................................... | am No 224, 1995 |
rep No 224, 1995 | |
r 275.......................................... | am No 224, 1995 |
rep No 224, 1995 | |
r 276.......................................... | am No 224, 1995 |
rep No 224, 1995 | |
r 277.......................................... | am No 325, 1992 |
rep No 224, 1995 | |
r 278.......................................... | rep No 224, 1995 |
r 279.......................................... | am No 224, 1995 |
rep No 224, 1995 | |
r 280.......................................... | am No 342, 1992; No 173, 1994; No 224, 1995 |
rep No 224, 1995 | |
r 281.......................................... | am No 289, 1990; No 147, 1991; No 187, 1994 |
rep No 201, 2003 | |
r 282.......................................... | am No 147, 1991; No 93, 1994; No 173, 1994; No 201, 2003; No 80, 2013 |
r 283.......................................... | am No 147, 1991; No 279, 1992; No 173, 1994 |
rep No 201, 2003 | |
r 284.......................................... | am No 147, 1991; No 93, 1994; No 173, 1994 |
rep No 260, 1994 | |
r 285.......................................... | am No 147, 1991; No 173, 1994 |
rep Act No 137, 2000 | |
r 286.......................................... | am No 147, 1991; No 173, 1994; No 201, 2003 |
rep F2021L00200 | |
r 287.......................................... | am No 80, 2013 |
r 288.......................................... | am No 147, 1991; No 173, 1994; No 224, 1995; No 201, 2003; No 80, 2013 |
r 289.......................................... | am No 147, 1991; No 173, 1994; No 201, 2003; No 80, 2013 |
r 291.......................................... | am No 147, 1991; No 173, 1994; No 294, 2000 |
rs No 201, 2003 | |
r 292.......................................... | am No 147, 1991; No 173, 1994; No 224, 1995; No 294, 2000; No 201, 2003 |
r 293.......................................... | am No 224, 1995 |
r 294.......................................... | am No 147, 1991; No 417, 1992; No 173, 1994; No 224, 1995; No 201, 2003; No 345, 2004 |
r 295.......................................... | am No 147, 1991; No 174, 1992; No 173, 1994; No 224, 1995 |
rep No 349, 2001 | |
r 296.......................................... | am No 426, 1991; No 80, 2013 |
Division 3.................................. | ad No 157, 1991 |
r 296A....................................... | ad No 157, 1991 |
am No 221, 1993 | |
rs No 353, 1999 | |
am No 353, 1999; No 345, 2004 | |
r 296B........................................ | ad No 157, 1991 |
r 296C........................................ | ad No 157, 1991 |
am No 224, 1995; No 353, 1999; No 80, 2013 | |
r 296D....................................... | ad No 157, 1991 |
am No 174, 1992 | |
r 296E........................................ | ad No 157, 1991 |
am No 224, 1995; No 353, 1999 | |
r 296F........................................ | ad No 157, 1991 |
am No 353, 1999 | |
r 296G....................................... | ad No 157, 1991 |
am No 353, 1999 | |
r 296H....................................... | ad No 157, 1991 |
r 296I......................................... | ad No 157, 1991 |
am No 224, 1995; No 353, 1999 | |
r 296J......................................... | ad No 157, 1991 |
r 297.......................................... | am No 224, 1995; No 294, 2000; No 80, 2013; F2020L00913; F2021L00200 |
r 297A....................................... | ad No 410, 1991 |
am No 487, 1991; No 174, 1992; No 279, 1992; No 325, 1992; No 380, 1992; No 417, 1992; No 221, 1993; No 93, 1994; No 187, 1994; No 260, 1994; No 224, 1995; No 111, 1997; No 166, 1999; No 353, 1999; No 8, 2000; No 221, 2002; No 319, 2002; No 350, 2002; No 232, 2003; No 134, 2004; No 345, 2004; No 191, 2008; No 273, 2008; No 77, 2011; F2024L01299 | |
rs No 80, 2013 | |
am No 274, 2013; F2016L01655; F2021L00200 | |
r 298.......................................... | am No 224, 1995; No 345, 2004 |
rep No 77, 2011 | |
r 298A....................................... | ad No 260, 1994 |
am No 224, 1995; No 353, 1999; No 345, 2004; No 5, 2013; F2021L00200; F2024L01299 | |
r 298B........................................ | ad No 260, 1994 |
am No 224, 1995; No 201, 2003 | |
r 298C........................................ | ad No 260, 1994 |
am No 224, 1995; No 201, 2003 | |
r 298D....................................... | ad No 260, 1994 |
am No 224, 1995; F2024L01299 | |
r 298E........................................ | ad No 260, 1994 |
r 299.......................................... | am No 147, 1991; No 221, 1993; No 173, 1994; No 224, 1995; No 201, 2003 |
rep No 77, 2011 | |
ad No 5, 2013 | |
am F2021L00200; F2024L01299 | |
r 300.......................................... | rep No 215, 1990 |
r 301.......................................... | am No 147, 1991; No 173, 1994; No 224, 1995; No 201, 2003; No 80, 2013 |
r 302.......................................... | am No 147, 1991; No 279, 1992; No 173, 1994; No 201, 2003; No 5, 2013; No 80, 2013 |
r 303.......................................... | am No 279, 1992; No 224, 1995; No 5, 2013; No 80, 2013; F2021L00200 |
r 303A....................................... | ad No 187, 1994 |
am No 224, 1995; No 345, 2004 | |
rep No 77, 2011 | |
r 304.......................................... | am No 147, 1991; No 173, 1994; No 224, 1995; No 201, 2003 |
r 305.......................................... | am No 289, 1990; No 147, 1991; No 417, 1992; No 173, 1994; No 201, 2003; No 80, 2013; No 166, 2014 |
r 306.......................................... | am No 224, 1995; No 80, 2013 |
r 307.......................................... | am No 147, 1991; No 173, 1994; No 224, 1995 |
rep No 204, 2000 | |
r 308.......................................... | rs No 54, 1991 |
am No 342, 1992; No 173, 1994; No 224, 1995; No 349, 2001; No 201, 2003; No 345, 2004 | |
rep No 77, 2011 | |
r 309.......................................... | am No 80, 2013 |
rep F2021L00200 | |
r 309A....................................... | ad No 382, 1994 |
am No 201, 2003 | |
rep F2021L00200 | |
r 310.......................................... | am No 224, 1995; No 80, 2013 |
rep No 274, 2013 | |
r 310AA..................................... | ad No 368, 1993 |
am No 224, 1995 | |
rep No 224, 1995 | |
r 310A....................................... | ad No 268, 1993 |
am No 188, 1994; No 148, 1995; No 224, 1995 | |
rep No 345, 2004 | |
r 310B........................................ | ad No 268, 1993 |
am No 188, 1994; No 148, 1995; No 224, 1995; No 201, 2003 | |
rep No 345, 2004 | |
r 310C........................................ | ad No 188, 1994 |
am No 224, 1995 | |
rep No 345, 2004 | |
Part 20 heading........................... | rs No 328, 2010 |
Division 1 heading...................... | ad No 328, 2010 |
r 311.......................................... | am No 224, 1995 |
rs No 345, 2004 | |
rep F2021L00200 | |
r 312.......................................... | ad No 235, 1998 |
am No 345, 2004; No 80, 2013 | |
r 313.......................................... | ad No 235, 1998 |
am No 262, 1999; No 345, 2004 | |
r 314.......................................... | ad No 235, 1998 |
am No 262, 1999; No 345, 2004 | |
r 315.......................................... | ad No 235, 1998 |
am No 345, 2004 | |
r 316.......................................... | ad No 235, 1998 |
rep No 262, 1999 | |
r 317.......................................... | ad No 235, 1998 |
am No 262, 1999; No 345, 2004 | |
rep F2016L01448 | |
r 317A....................................... | ad No 166, 1999 |
am No 345, 2004 | |
rep No 76, 2011 | |
r 318.......................................... | ad No 235, 1998 |
am No 166, 1999; No 350, 2002; No 345, 2004 | |
r 319.......................................... | ad No 235, 1998 |
am No 345, 2004 | |
r 320.......................................... | ad No 235, 1998 |
am No 345, 2004 | |
r 321.......................................... | ad No 235, 1998 |
am No 345, 2004 | |
r 322.......................................... | ad No 167, 1999 |
am No 205, 2000; No 350, 2002; No 201, 2003; No 345, 2004 | |
rep No 188, 2013 | |
r 323.......................................... | ad No 167, 1999 |
rs No 345, 2004 | |
rep No 188, 2013 | |
r 323AA..................................... | ad No 243, 2005 |
rep F2021L00200 | |
r 323A....................................... | ad No 189, 2003 |
rs No 345, 2004 | |
rep F2021L00200 | |
r 324.......................................... | ad No 262, 1999 |
rs No 345, 2004 | |
am F2016L01655 | |
rep F2021L00200 | |
r 325.......................................... | ad No 353, 1999 |
rs No 345, 2004 | |
Division 2 heading...................... | rs No 275, 2013 |
Division 2.................................. | ad No 328, 2010 |
r 326.......................................... | ad No 328, 2010 |
rep No 275, 2013 | |
r 327.......................................... | ad No 328, 2010 |
rep No 275, 2013 | |
r 328.......................................... | ad No 328, 2010 |
rs No 275, 2013 | |
r 329.......................................... | ad No 328, 2010 |
rep No 275, 2013 | |
r 330.......................................... | ad No 328, 2010 |
am No 275, 2013 | |
r 331.......................................... | ad No 328, 2010 |
r 332.......................................... | ad No 328, 2010 |
am No 275, 2013 | |
rep F2021L00200 | |
Division 3 heading...................... | rs No 274, 2013 |
Division 3.................................. | ad No 5, 2013 |
r 333.......................................... | ad No 5, 2013 |
r 334.......................................... | ad No 5, 2013 |
r 335.......................................... | ad No 5, 2013 |
Division 4.................................. | ad No 275, 2013 |
r 336.......................................... | ad No 275, 2013 |
r 337.......................................... | ad No 275, 2013 |
r 338.......................................... | ad No 275, 2013 |
r 339.......................................... | ad No 275, 2013 |
r 340.......................................... | ad No 275, 2013 |
r 341.......................................... | ad No 275, 2013 |
r 342.......................................... | ad No 275, 2013 |
r 343.......................................... | ad No 275, 2013 |
Division 6.................................. | ad F2016L01655 |
rep 28 July 2017 (r 351(3)) | |
r 351.......................................... | ad F2016L01655 |
rep 28 July 2017 (r 351(3)) | |
Schedule.................................... | ad No 216, 1990 |
Schedule 1 (prev Schedule).......... | renum No 157, 1991 |
am No 287, 1991; No 279, 1992; No 382, 1994 | |
rep No 232, 2003 | |
Schedule 2.................................. | ad No 157, 1991 |
am No 410, 1991; No 279, 1992 | |
rs No 173, 1994 | |
rep No 353, 1999 | |
Schedule 3.................................. | ad No 382, 1991 |
rep No 319, 1993 | |
Schedule 4.................................. | ad No 410, 1991 |
am No 224, 1995; No 365, 2003 | |
rep No 365, 2003 | |
Schedule 5 heading...................... | rs No 345, 2004 |
Schedule 5.................................. | ad No 487, 1991 |
am No 174, 1992; No 245, 2015; F2021L00200; F2024L00297 | |
Schedule 6 heading...................... | rs No 345, 2004 |
Schedule 6.................................. | ad No 487, 1991 |
am No 174, 1992; No 93, 1994; No 224, 1995; No 328, 2010 | |
Schedule 7.................................. | ad No 487, 1991 |
am F2021L00200 | |
Schedule 8 heading...................... | rs No 174, 1992; No 382, 1994; No 246, 2015 |
Schedule 8.................................. | ad No 487, 1991 |
am No 174, 1992; No 246, 2015; F2021L00200 | |
Schedule 9.................................. | ad No 487, 1991 |
am No 80, 2013 | |
Schedule 10................................ | ad No 417, 1992 |
am No 224, 1995; No 294, 2000 | |
rep No 58, 2003 | |
Schedule 11................................ | ad No 417, 1992 |
am No 224, 1995 | |
rep No 58, 2003 |
The renumbering of provisions of the
Part I | Part 1 |
Part II | Part 2 |
Part III | Part 3 |
Division 1 | Division 1 |
Division 1A | Division 2 |
Division 1B | Division 3 |
Division 1C | Division 4 |
Division 1D | Division 5 |
Division 1E | Division 6 |
Division 2 | Division 7 |
Part IV | Part 4 |
Division 1 | Division 1 |
Division 3 | Division 2 |
Division 4 | Division 3 |
Division 5 | Division 4 |
Division 6 | Division 5 |
Part IVA | Part 4A |
Division 1 | Division 1 |
Division 2 | Division 2 |
Subdivision A | Subdivision 1 |
Subdivision B | Subdivision 2 |
Subdivision C | Subdivision 3 |
Division 3 | Division 3 |
Division 4 | Division 4 |
Division 5 | Division 5 |
Division 6 | Division 6 |
Subdivision A | Subdivision 1 |
Subdivision B | Subdivision 2 |
Subdivision C | Subdivision 3 |
Division 7 | Division 7 |
Division 8 | Division 8 |
Division 9 | Division 9 |
Division 10 | Division 10 |
Division 11 | Division 11 |
Part IVB | Part 4B |
Part 4C | Part 4C |
Part 5 | Part 5 |
Division 1 | Division 1 |
Division 2 | Division 2 |
Division 3 | Division 3 |
Division 4 | Division 4 |
Division 5 | Division 5 |
Division 6 | Division 6 |
Division 7 | Division 7 |
Division 8 | Division 8 |
Division 9 | Division 9 |
Division 10 | Division 10 |
Division 11 | Division 11 |
Division 12 | Division 12 |
Division 13 | Division 13 |
Division 14 | Division 14 |
Division 15 | Division 15 |
Division 16 | Division 16 |
Division 16A | Division 17 |
Division 17 | Division 18 |
Part 6 | Part 6 |
Part 7 | Part 7 |
Part VIII | Part 8 |
Part IXA | Part 9 |
Division 1 | Division 1 |
Division 2 | Division 2 |
Division 3 | Division 3 |
Division 4 | Division 4 |
Division 5 | Division 5 |
Division 6 | Division 6 |
Division 7 | Division 7 |
Division 8 | Division 8 |
Division 9 | Division 9 |
Part IXB | Part 10 |
Division 1 | Division 1 |
Division 2 | Division 2 |
Division 5 | Division 3 |
Part X | Part 11 |
Division 1 | Division 1 |
Division 2 | Division 2 |
Part XI | Part 12 |
Division 1 | Division 1 |
Division 2 | Division 2 |
Division 3 | Division 3 |
Division 4 | Division 4 |
Part XII | Part 13 |
Division 1 | Division 1 |
Division 2 | Division 2 |
Division 3 | Division 3 |
Division 4 | Division 4 |
Part XIII | Part 14 |
Division 1 | Division 1 |
Division 2 | Division 2 |
Division 3 | Division 3 |
Division 4 | Division 4 |
Division 5 | Division 5 |
Subdivision A | Subdivision 1 |
Subdivision B | Subdivision 2 |
Division 6 | Division 6 |
Part XIIIA | Part 15 |
Part XIV | Part 16 |
Part XVI | Part 17 |
Division 1 | Division 1 |
Division 2 | Division 2 |
Division 3 | Division 3 |
Part XVII | Part 18 |
Part XVIII | Part 19 |
Part XIX | Part 20 |
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