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3.2—the maintenance has been co-ordinated;
(c) certifications that are required to be made by paragraph 2.1 or 3.7 have been
made.
Civil Aviation Regulations 1988 Scheds — 29
Amended CAR – 2nd Ed Legal Services Group
August 2003 Civil Aviation Safety Authority
SCHEDULE 7 Paragraph 42ZC (4) (b)
MAINTENANCE THAT MUST NOT BE CARRIED OUT
ON A CLASS B AIRCRAFT BY A PERSON
REFERRED TO IN PARAGRAPH 42ZC (4) (b)
Part 1—General
1.1 The inspection of an aircraft for the purpose of the issue of a maintenance release.
1.2 Maintenance involving disturbing the individual parts of an aircraft component
supplied as a bench tested component where the subsequent functioning of the
component can only be proved by the use of test equipment additional to the
equipment used for normal functional checks and trouble shooting checks.
1.3 Maintenance involving the use of non-destructive testing methods, but not
including the use of aerosol packed materials in conducting liquid penetrant
inspections.
1.4 Maintenance involving the complete jacking of an aircraft.
1.5 Maintenance involving the use of jigs, but not including the use of control rigging
devices.
Part 2—Maintenance of airframes
2.1 The repair or modification of:
(a) the primary structure of an aircraft; or
(b) the seat support structure of an aircraft.
2.2 Welding, brazing, heat treating or metalizing of or on the primary structure of an
aircraft.
2.3 Riveting, gluing or bonding joints in the primary structure of an aircraft.
2.4 Bolting joints in the airframe of an aircraft, where the bolting requires the use of
special techniques.
2.5 Replacing a complete fabric covering of a fuselage, aerofoil or flying surface.
2.6 Balancing flying control surfaces.
2.7 Balancing main or tail rotor assemblies.
2.8 Refurbishing the interior of an aircraft.
2.9 Repainting that might affect the balance of flying control surfaces.
Part 3—Maintenance of engines
3.1 Disassembly or assembly of a crankcase of a reciprocating engine.
3.2 Disassembly or assembly of a crankshaft of a reciprocating engine (including
removal and replacement of a connecting rod).
3.3 Disassembly or assembly of a rotor housing of a rotary engine.
3.4 Disassembly or assembly of a rotor assembly of a rotary engine.
3.5 Disassembly or assembly of a main casing of a turbine engine.
3.6 Disassembly or assembly of a rotating assembly of a turbine engine.
3.7 Balancing of rotating assemblies of engines.
3.8 Welding, brazing, heat treating or metalizing, but not including minor repairs to
exhaust pipes .
3.9 Machining, other than machining using standard hand tools or valve refacing
equipment.
Scheds — 30 Civil Aviation Regulations 1988
Legal Services Group Amended CAR – 2nd Ed
Civil Aviation Safety Authority August 2003
3.10 Removal or replacement of reduction gears or accessory drive gears that are not
attached to an accessory.
3.11 Balancing of propellers.
3.12 Disassembly and assembly of propeller hubs.
3.13Straightening of propeller blades.
Part 4—Maintenance on electrical, instrument and radio systems
4.1 Maintenance of operational software and automatic test equipment software.
4.2 Initial installation of an electrical, instrument or radio system.
Part 5—Specific maintenance on manned balloons and hot air airships
5.1 In relation to a manned balloon or a hot air airship:
(a) the replacement of one or more panels in the upper half of the envelope; or
(b) the replacement of 4 or more panels in the lower half of the envelope; or
(c) the repair or replacement of load tape; or
(d) the repair of the suspension system; or
(e) the repair of the burner system, other than seal replacement or the cleaning
of jets .
NOTE: For maintenance of engines of hot air airships see Part 3.
Civil Aviation Regulations 1988 Scheds — 31
Amended CAR – 2nd Ed Legal Services Group
August 2003 Civil Aviation Safety Authority
SCHEDULE 8 Paragraph 42ZC (4) (d)
MAINTENANCE THAT MAY BE CARRIED OUT ON A CLASS B AIRCRAFT
BY A PILOT ENTITLED TO DO SO UNDER SUBREGULATION 42ZC (4)
1. Removal or installation of landing gear tyres, but only if the removal or
installation does not involve the complete jacking of the aircraft.
2. Repair of pneumatic tubes of landing gear tyres.
3. Servicing of landing gear wheel bearings.
4. Replacement of defective safety wiring or split pins, but not including wiring or
pins in control systems.
5. Removal or refitting of a door, but only if:
(a) no disassembly of the primary structure or operating system of the aircraft is
　
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