GreatNorthCollective/greatnorth-canada-federal-laws-text huggingface dataset:
Canadian Aviation Regulations — 571.10
571.10 (1) No person shall sign a maintenance release required pursuant to section 605.85 or permit anyone whom the person supervises to sign a maintenance release, unless the standards of airworthiness applicable to the maintenance performed and stated in Standard 571 — Maintenance have been complied with and the maintenance release meets the applicable requirements specified in section 571.10 of the Airworthiness Manual . (2) Except as provided in subsection (4), a maintenance release shall include the following, or a similarly worded, statement: “The described maintenance has been performed in accordance with the applicable airworthiness requirements.” (3) No maintenance release is required in respect of any task designated as elementary work in the Aircraft Equipment and Maintenance Standards that is performed by (a) in the case of a glider, a balloon or an unpressurized small aircraft that is powered by a piston engine and not operated pursuant to Part IV or VII, the pilot of the aircraft; (b) in the case of an aircraft operated under Part IV or VII, a person who has been trained and authorized in accordance with the flight training unit’s or the air operator’s maintenance control manual (MCM), approved under Subpart 6 of Part IV or of Part VII, respectively; or (c) in the case of an aircraft operated pursuant to Subpart 4 of Part VI, a person who has been trained in accordance with those sections of a private operator’s operations manual that contain details of the operator’s maintenance control system. (4) Where a person signs a maintenance release in respect of maintenance performed on an aircraft, the satisfactory completion of which cannot be verified by inspection or testing of the aircraft on the ground, the maintenance release shall be made conditional on the satisfactory completion of a test flight carried out pursuant to subsections 605.85(2) and (3), by the inclusion of the phrase “subject to satisfactory test flight”. (5) No person shall sign a maintenance release in respect of specialized maintenance unless the requirements of section 571.04 have been met. SOR/2000-404, s. 8; SOR/2003-154, s. 6(F) SOR/2019-122, s. 21
Canadian Aviation Regulations — Canadian Aviation Regulations
“The described maintenance has been performed in accordance with the applicable airworthiness requirements.”
Canadian Aviation Regulations — 571.11
the holder of an AME licence specifying a rating appropriate to the aeronautical product being maintained may sign a maintenance release if the person holds a restricted certification authority issued in accordance with subsection (8), in respect of a particular case specified on the restricted certification authority. (8) The Minister shall issue a restricted certification authority and specify therein its validity period and the scope of the work that may be performed, if (a) an application is made in accordance with section 571.11 of the Airworthiness Manual ; (b) the applicant demonstrates to the Minister that there is no holder of an AME licence specifying a rating appropriate to the aeronautical product being maintained available within a geographical area accessible within one hour by surface transportation; (c) the person to whom the restricted certification authority is to be issued has received the training and has the knowledge equivalent to that of a holder of an AME licence specifying a rating appropriate to the aeronautical product being maintained; and (d) the level of aviation safety is not affected by the issuance of the restricted certification authority. SOR/2000-404, s. 9; SOR/2002-112, s.11 SOR/2019-122, s. 3
Canadian Aviation Regulations — 571.12
571.12 A person who performs a major repair or major modification on an aeronautical product or installs on an aircraft a part that has undergone a major repair or major modification shall report the action to the Minister in accordance with the procedures specified in section 571.12 of the Airworthiness Manual .
Canadian Aviation Regulations — 571.13
571.13 (1) Subject to sections 571.07 to 571.09, no person shall install a part on an aeronautical product unless the part is (a) inspected and its accompanying documentation verified in accordance with a procedure that ensures that the part conforms to its type design, as is indicated by the maintenance release; and (b) installed in accordance with the requirements of section 571.13 of the Airworthiness Manual . (2) If a part is obtained from an aeronautical product that was damaged or permanently withdrawn from service, the part shall not be installed unless it (a) can be traced to the manufacturer certificate holder; and (b) is inspected in conformity with the instructions for continued airworthiness or, if the part has been repaired or modified, it can be ascertained that the work was performed in accordance with approved data within the meaning of section 571.06 of the Airworthiness Manual . SOR/2002-112, s. 12
Canadian Aviation Regulations — Canadian Aviation Regulations
The following tasks constitute the specialized maintenance referred to in section 571.04 of these Regulations.
Canadian Aviation Regulations — (1)
(1) The modification, repair or replacement by riveting, bonding or laminating, or the making of any of the following airframe parts is structural specialized maintenance: (a) a box beam; (b) a wing stringer or chord member; (c) a spar; (d) a spar flange; (e) a member of a truss-type beam; (f) the web of a beam; (g) a keel or chine member of a flying boat hull or a float; (h) a corrugated sheet compression member in a wing or tail surface; (i) a wing main rib; (j) a wing or tail surface brace strut; (k) an engine mount; (l) a fuselage longeron or frame; (m) a member of a side truss, horizontal truss or bulkhead; (n) a seat support brace or bracket, excluding the replacement of seat rails; (o) a seat rail replacement for transport category aircraft; (p) a landing gear strut or brace strut; (q) an axle; (r) a wheel; and (s) a ski or ski pedestal, excluding the replacement of a low-friction coating.
Canadian Aviation Regulations — (g)
(g) a keel or chine member of a flying boat hull or a float;
Canadian Aviation Regulations — (h)
(h) a corrugated sheet compression member in a wing or tail surface;
Canadian Aviation Regulations — (m)
(m) a member of a side truss, horizontal truss or bulkhead;
Canadian Aviation Regulations — (n)
(n) a seat support brace or bracket, excluding the replacement of seat rails;
Canadian Aviation Regulations — (o)
(o) a seat rail replacement for transport category aircraft;
Canadian Aviation Regulations — (p)
(p) a landing gear strut or brace strut;
Canadian Aviation Regulations — (s)
(s) a ski or ski pedestal, excluding the replacement of a low-friction coating.
Canadian Aviation Regulations — (2)
(2) The modification or repair of any of the following parts of an airframe is structural specialized maintenance: (a) aircraft skin, or the skin of an aircraft float, if the work requires the use of a support, jig or fixture; (b) aircraft skin that is subject to pressurization loads, if the damage to the skin measures more than 15 cm (6 inches) in any direction; (c) a load-bearing part of a control system, including a control column, pedal, shaft, quadrant, bellcrank, torque tube, control horn and forged or cast bracket, but excluding (i) the swaging of a repair splice or cable fitting, and (ii) the replacement of a push-pull tube end fitting that is attached by riveting; and (d) any other structure that a manufacturer has identified as a primary structure in its maintenance manual, structural repair manual or any instructions for continuing airworthiness.
Canadian Aviation Regulations — (a)
(a) aircraft skin, or the skin of an aircraft float, if the work requires the use of a support, jig or fixture;
Canadian Aviation Regulations — (b)
(b) aircraft skin that is subject to pressurization loads, if the damage to the skin measures more than 15 cm (6 inches) in any direction;
Canadian Aviation Regulations — (c)
(c) a load-bearing part of a control system, including a control column, pedal, shaft, quadrant, bellcrank, torque tube, control horn and forged or cast bracket, but excluding (i) the swaging of a repair splice or cable fitting, and (ii) the replacement of a push-pull tube end fitting that is attached by riveting; and
Canadian Aviation Regulations — (i)
(i) the swaging of a repair splice or cable fitting, and
Canadian Aviation Regulations — (ii)
(ii) the replacement of a push-pull tube end fitting that is attached by riveting; and
Canadian Aviation Regulations — (d)
(d) any other structure that a manufacturer has identified as a primary structure in its maintenance manual, structural repair manual or any instructions for continuing airworthiness.
Canadian Aviation Regulations — 2
2 Any of the following types of tasks is engine specialized maintenance: (a) the reassembly of a multi-part engine crankshaft or a crankshaft equipped with a dynamic counterweight system; (b) the reassembly of the crankcase of a reciprocating engine that is equipped with an integral supercharger or a propeller reduction gear; (c) the overhaul of a reciprocating engine that is equipped with an integral or turbo supercharger; and (d) the overhaul of a turbine engine or turbine engine module.
Canadian Aviation Regulations — (a)
(a) the reassembly of a multi-part engine crankshaft or a crankshaft equipped with a dynamic counterweight system;
Canadian Aviation Regulations — (b)
(b) the reassembly of the crankcase of a reciprocating engine that is equipped with an integral supercharger or a propeller reduction gear;
Canadian Aviation Regulations — (c)
(c) the overhaul of a reciprocating engine that is equipped with an integral or turbo supercharger; and
Canadian Aviation Regulations — (d)
(d) the overhaul of a turbine engine or turbine engine module.
Canadian Aviation Regulations — 3
3 Any of the following types of propeller repair, if the work is beyond the limits recommended in the manufacturer’s maintenance manual or service instructions for service in the field is propeller specialized maintenance: (a) the re-contouring, twisting, shortening or straightening of a propeller blade or the blending of damage thereto; (b) the repair or machining of a propeller hub, excluding the removal of surface corrosion or application of a protective coating; (c) the reinstallation of a metal leading edge sheath or tip of a wooden blade; (d) the replacement of the outer protective coating on a wooden blade, excluding the restoration of varnish; (e) the repair of an elongated propeller attachment or propeller blade attachment bolt hole; (f) the inlaying of a repair patch on a wooden blade; (g) the repair of a composite blade; and (h) an overhaul or repair involving the reassembly of a controllable-pitch propeller, excluding the reassembly of a propeller that has been disassembled for shipping purposes, or the replacement of seals.
Canadian Aviation Regulations — (a)
(a) the re-contouring, twisting, shortening or straightening of a propeller blade or the blending of damage thereto;
Canadian Aviation Regulations — (b)
(b) the repair or machining of a propeller hub, excluding the removal of surface corrosion or application of a protective coating;
Canadian Aviation Regulations — (c)
(c) the reinstallation of a metal leading edge sheath or tip of a wooden blade;
Canadian Aviation Regulations — (d)
(d) the replacement of the outer protective coating on a wooden blade, excluding the restoration of varnish;
Canadian Aviation Regulations — (e)
(e) the repair of an elongated propeller attachment or propeller blade attachment bolt hole;
Canadian Aviation Regulations — (f)
(f) the inlaying of a repair patch on a wooden blade;
Canadian Aviation Regulations — (g)
(g) the repair of a composite blade; and
Canadian Aviation Regulations — (h)
(h) an overhaul or repair involving the reassembly of a controllable-pitch propeller, excluding the reassembly of a propeller that has been disassembled for shipping purposes, or the replacement of seals.
Canadian Aviation Regulations — (1)
(1) The repair of avionics components and systems is avionics specialized maintenance, except for: (a) repairs of wiring and connectors; (b) replacement of connectors and electrical components with identical or equivalent items; (c) replacement of antennas with identical or equivalent items; (d) replacement of integral fuses and lighting components when the line replaceable unit (LRU) is designed for flight-line replacement of these components; (e) replacement of an avionics LRU provided that any testing required can be done using standard test equipment, built-in test equipment (BITE) or equipment specified in the aircraft manufacturer’s instructions for continuing airworthiness; (f) on-site maintenance of passenger entertainment systems performed in accordance with the applicable instructions in the maintenance manual of the aircraft or systems manufacturer or the manufacturer’s instructions for continuing airworthiness; and (g) routine maintenance that is described in the aircraft manufacturer’s maintenance manual or instructions for continuing airworthiness or performed in accordance with currently recognized industry practices for service in the field.
Canadian Aviation Regulations — (b)
(b) replacement of connectors and electrical components with identical or equivalent items;
Canadian Aviation Regulations — (c)
(c) replacement of antennas with identical or equivalent items;
Canadian Aviation Regulations — (d)
(d) replacement of integral fuses and lighting components when the line replaceable unit (LRU) is designed for flight-line replacement of these components;
Canadian Aviation Regulations — (e)
(e) replacement of an avionics LRU provided that any testing required can be done using standard test equipment, built-in test equipment (BITE) or equipment specified in the aircraft manufacturer’s instructions for continuing airworthiness;
Canadian Aviation Regulations — (f)
(f) on-site maintenance of passenger entertainment systems performed in accordance with the applicable instructions in the maintenance manual of the aircraft or systems manufacturer or the manufacturer’s instructions for continuing airworthiness; and
Canadian Aviation Regulations — (g)
(g) routine maintenance that is described in the aircraft manufacturer’s maintenance manual or instructions for continuing airworthiness or performed in accordance with currently recognized industry practices for service in the field.
Canadian Aviation Regulations — (2)
(2) Any avionics system installation or modification is avionics specialized maintenance except for: (a) installation of ELT systems conforming to the CAN-TSO as set out in section 551.104 of Chapter 551 — Aircraft Equipment and Installation of the Airworthiness Manual , if the ELT systems are not interfaced with any other systems; (b) installation of single VHF communication or single integrated navigation/communication systems that are not interfaced with any other system, other than an intercom system; (c) installation of VFR long-range navigation systems which are not interfaced with any other systems; (d) modifications to existing avionics installations, where no additional test requirements are imposed on the affected system other than those which would be required following routine maintenance of that system; (e) installation of instruments which are not interfaced with any other systems; and (f) replacement of an avionics LRU where equivalency is maintained, and where no additional test requirements are imposed on the affected system other than those which would be required following routine maintenance of that system.
Canadian Aviation Regulations — (a)
(a) installation of ELT systems conforming to the CAN-TSO as set out in section 551.104 of Chapter 551 — Aircraft Equipment and Installation of the Airworthiness Manual , if the ELT systems are not interfaced with any other systems;
Canadian Aviation Regulations — (b)
(b) installation of single VHF communication or single integrated navigation/communication systems that are not interfaced with any other system, other than an intercom system;
Canadian Aviation Regulations — (c)
(c) installation of VFR long-range navigation systems which are not interfaced with any other systems;
Canadian Aviation Regulations — (d)
(d) modifications to existing avionics installations, where no additional test requirements are imposed on the affected system other than those which would be required following routine maintenance of that system;
Canadian Aviation Regulations — (e)
(e) installation of instruments which are not interfaced with any other systems; and
Canadian Aviation Regulations — (f)
(f) replacement of an avionics LRU where equivalency is maintained, and where no additional test requirements are imposed on the affected system other than those which would be required following routine maintenance of that system.
Canadian Aviation Regulations — 5
5 Maintenance of instruments, other than display devices whose operation is integrated with an appliance to which another category of specialized maintenance applies, if the work is beyond the limits recommended in the manufacturer’s maintenance manual or service instructions for service in the field, is instrument specialized maintenance.
Canadian Aviation Regulations — 6
6 Any of the following types of maintenance of an appliance or component, where the work is beyond the limits recommended in the manufacturer’s maintenance manual or service instructions for service in the field, is component specialized maintenance: (a) the reassembling of valves that are activated electrically or through the use of controlled fluid pressure; (b) the calibrating or flow checking of any fuel metering or air metering component, other than a float-type carburettor; (c) the overhaul of any pressure-type fuel, oil, pneumatic or hydraulic pump; (d) a repair involving the disassembly of speed-regulating devices, including an engine or propeller governor or a constant-speed drive; (e) the overhaul of a rotor head, transmission or any mechanism used to transmit power to the rotors of a tilt-wing aircraft or helicopter; (f) the repair of a helicopter rotor blade; (g) the rewinding of the field coil or armature of an electrical accessory; (h) the overhaul of an aircraft magneto; and (i) the patch repair of a bladder-type fuel tank.
Canadian Aviation Regulations — (a)
(a) the reassembling of valves that are activated electrically or through the use of controlled fluid pressure;
Canadian Aviation Regulations — (b)
(b) the calibrating or flow checking of any fuel metering or air metering component, other than a float-type carburettor;
Canadian Aviation Regulations — (c)
(c) the overhaul of any pressure-type fuel, oil, pneumatic or hydraulic pump;
Canadian Aviation Regulations — (d)
(d) a repair involving the disassembly of speed-regulating devices, including an engine or propeller governor or a constant-speed drive;
Canadian Aviation Regulations — (e)
(e) the overhaul of a rotor head, transmission or any mechanism used to transmit power to the rotors of a tilt-wing aircraft or helicopter;
Canadian Aviation Regulations — (f)
(f) the repair of a helicopter rotor blade;
Canadian Aviation Regulations — (g)
(g) the rewinding of the field coil or armature of an electrical accessory;
Canadian Aviation Regulations — (h)
(h) the overhaul of an aircraft magneto; and
Canadian Aviation Regulations — (i)
(i) the patch repair of a bladder-type fuel tank.
Canadian Aviation Regulations — 7
7 The welding of the following parts is welding specialized maintenance: (a) any part of the primary structure, including a wheel, an axle and a passenger restraint or cargo restraint system; (b) any part of an aircraft system, including a fuel tank, an oil tank and a pneumatic or hydraulic container; and (c) any structural or dynamic engine part.
Canadian Aviation Regulations — (a)
(a) any part of the primary structure, including a wheel, an axle and a passenger restraint or cargo restraint system;
Canadian Aviation Regulations — (b)
(b) any part of an aircraft system, including a fuel tank, an oil tank and a pneumatic or hydraulic container; and
Canadian Aviation Regulations — (c)
(c) any structural or dynamic engine part.
Canadian Aviation Regulations — 8
8 Any required inspection of an aeronautical product that uses liquid penetrant, magnetic particle, radiographic, ultrasonic or eddy current methods, unless the inspection is performed under Appendix K to Standard 571 — Maintenance , is Non-Destructive Testing (NDT) Specialized Maintenance.
Canadian Aviation Regulations — 573.01
573.01 (1) An applicant for an approved maintenance organization (AMO) certificate or for an amendment of an AMO certificate that is in effect shall make an application in the form and manner specified in Standard 573 — Approved Maintenance Organizations . (2) An applicant referred to in subsection (1) shall submit to the Minister with the application a copy of its maintenance policy manual (MPM) required pursuant to subsection 573.10(1). SOR/2005-173, s. 28
Canadian Aviation Regulations — 573.02
573.02 (1) The Minister shall issue to a maintenance organization that demonstrates that it meets the requirements of this Subpart an approved maintenance organization (AMO) certificate authorizing the maintenance of specified aeronautical products or the provision of specified maintenance services. (2) The AMO certificate shall specify, in accordance with the criteria specified in section 573.02 of Standard 573 — Approved Maintenance Organizations , any category in which ratings have been issued and shall list the aeronautical products that the AMO is authorized to maintain or the maintenance services that the AMO is authorized to perform. (3) The scope of the work that may be performed under each rating specified on the AMO certificate is determined by limitations that are set out in the certificate. (4) Unless an expiry date is specified in an AMO certificate issued pursuant to subsection (1), the certificate remains in effect until it is surrendered, suspended or cancelled. SOR/2005-173, s. 15