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are controlled before being incorporated in a finished aircraft,
aircraft engine or propeller;
(h) segregating, identifying, marking and disposing of rejected
materials and parts in a manner that precludes installation in the
finished aircraft, aircraft engine or propeller;
(i) a system for processing through the Materials Review Board any
materials and parts that are withheld because of departures from
design data or specifications, and that are to be considered for
installation in a finished aircraft, aircraft engine or propeller;
(j) a system for identifying and reinspecting materials and parts
determined by the Materials Review Board to be serviceable if
rework or repair is necessary;
(k) maintaining inspection records, identified with the finished
aircraft, aircraft engine or propeller where practicable, and
retaining them for at least 2 years.
Source FARs section 21.125 modified.
Civil Aviation Safety Regulations 1998 (CASR)
Office of Legal Counsel CASR
Civil Aviation Safety Authority 1st Edition – January 2003
Part 21 — 50
21.127 Tests: aircraft
(1) Each person manufacturing aircraft under a type certificate only must
establish an approved production flight test procedure and flight
check-off form, and in accordance with that form, flight test each
aircraft produced.
Penalty: 25 penalty units.
(1A) An offence against subregulation (1) is an offence of strict liability.
Note For strict liability, see section 6.1 of the Criminal Code.
(2) Each production flight test procedure must include the following:
(a) an operational check of the trim, controllability, or other flight
characteristics to establish that the production aircraft has the
same range and degree of control as the prototype aircraft;
(b) an operational check of each part or system operated by the crew
while in flight to establish that, during flight, instrument readings
are within normal range;
(c) a determination that all instruments are properly marked, and that
all placards and required flight manuals are installed after flight
test;
(d) a check of the operational characteristics of the aircraft on the
ground;
(e) a check on any other items peculiar to the aircraft being tested
that can best be done during the ground or flight operation of the
aircraft.
Source FARs section 21.127 modified.
21.128 Tests: aircraft engines
(1) Each person manufacturing aircraft engines that are not rocket
engines under a type certificate only must subject each engine to an
acceptable test run that includes the following:
(a) break-in runs that include a determination of fuel and oil
consumption and a determination of power characteristics at
rated maximum continuous power or thrust and, if applicable, at
rated take-off power or thrust;
(b) at least five hours of operation at rated maximum continuous
power or thrust, including, for engines having a rated take-off
power or thrust higher than rated maximum continuous power or
thrust, 30 minutes at rated take-off power or thrust.
Penalty: 25 penalty units.
(2) The test runs required by subregulation (1) may be made with the
engine appropriately mounted and using current types of power and
thrust measuring equipment.
Civil Aviation Safety Regulations 1998 (CASR)
CASR Office of Legal Counsel
1st Edition – January 2003 Civil Aviation Safety Authority
Part 21 — 51
(3) A person manufacturing rocket engines under a type certificate only
must establish a sampling technique for testing the engines.
Penalty: 25 penalty units.
(4) An offence against subregulation (1) or (3) is an offence of strict
liability.
Note For strict liability, see section 6.1 of the Criminal Code.
Source FARs section 21.128 modified.
21.129 Tests: variable pitch propellers
(1) Each person manufacturing variable pitch propellers under a type
certificate only must give each propeller an acceptable functional test
to determine if it operates properly throughout the normal range of
operation.
Penalty: 25 penalty units.
(2) An offence against subregulation (1) is an offence of strict liability.
Note For strict liability, see section 6.1 of the Criminal Code.
Source FARs section 21.129 modified.
21.130 Statement of conformity
(1) Each holder or licensee of a type certificate for a type of aircraft,
aircraft engine or propeller must give CASA a statement of
conformity, in a form acceptable to CASA, for each aircraft, aircraft
engine or propeller manufactured under the type certificate only:
(a) when the holder or licensee applies for the original issue of an
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