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(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.
42C Maintenance schedule: approved system of maintenance
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.
42CA Maintenance schedule—primary, intermediate, restricted or
limited category aircraft
(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, 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.
Civil Aviation Regulations 1988 79
Amended CAR – 2nd Ed Legal Services Group
August 2003 Civil Aviation Safety Authority
42CB Maintenance—experimental 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.
42D Can there be more than one maintenance schedule?
If, apart from this subregulation, 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 given 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.
42E Elections
(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.
42F Effect of change of holder of certificate of registration
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.
Replacement Page Amdt No. 8
December 2004
80 Civil Aviation Regulations 1988
Legal Services Group Amended CAR – 2nd Ed
Civil Aviation Safety Authority August 2003
Subdivision 3 Miscellaneous
42G Flight control system: additional requirements
(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;
　
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