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Norway
Papua New Guinea
Sweden
United States
United Kingdom
United States
Australia
United States
Georgia
Papua New Guinea
Georgia
Norway
Australia
Georgia
Papua New Guinea
United States
Georgia
Chapter 8
8.1 Georgia
New Zealand
8.1.1 United Kingdom
8.1.3 Argentina
France
8.2 Georgia
New Zealand
8.2.1 United Kingdom
8.2.2 Argentina
New Zealand
Sweden
United States
New Zealand
Papua New Guinea
Sweden
Georgia
United Kingdom
Chapter 9 -
General United States
9.1 Denmark
Georgia
New Zealand
9.2 Georgia
Appendix Georgia
Norway
SUPPLEMENTTO ANNEX 6, PART (SIXTHE DITION) ARGENTINA1
CHAPTER 3
Definitions Aerodrome operating minima. The former definition has been retained for subparagraph c).
Approach and landing operations using instrurnentapproachprocedures. The fomer definition has been
retained.
Decision altitude (DA) or decision height (DM.Th e former definition has been retained.
Flight time - aeroplanes. The former definition has been retained.
CHAPTER 6
6.10.1.7 The Argentine Republic does not require the installation of a Type 1A recorder.
6.10.1.7.1 The Argentine Republic only requires recording of the following parameters: pressure altitude; speed;
heading: normal acceleration; longitudinal acceleration; and time.
6.10.1.7.2 The Argentine Republic only requires recording of h e following parameters: pitch attitude and roll
attitude.
6.10.1.7.3 Thc Argentine Republic only requires recording of thrust.
6.10.1.7.4 The Argentine Republic only requires recording of h e pitch trim surface position.
6.10.1.7.5 The Argentine Republic does not apply this requirement.
6.10.4 The Argentine Republic requires cockpit voice recorders to record only 11 parameters.
CHAPTER S
8.1.3
8.2.2
In the Argentine Republic, only an approved maintenance organization may issue a maintenance release.
Maintenance records that attest to the completion of maintenance must be kept for five years after the
signing of the maintenance release.
CHAPTER l
Definitions Approach andlanding operations using instrument approachprocedures. Australian legislation docs no1
define approach and landing operations with vertical guidance. Australiadoes not yet have any instrument
approach procedures that utilize GPSD data for vertical guidance.
CHAPTER 4
4.6.1
CHAPTER 6
6.1.3.1.1
6.2.2*
Australia places the decision-making responsibility on the pilocin-command for commencement and
continuation of a flight.
There is no requirement to maintain two-way cominunications between the aeroplane and the ground crew
while refuelling with passengers on board.
The requirements for carriage of first-aid kits and fire extinguishers are not implemented as prescribed.
Australian lcgislation does not base the requirement to be equipped in accordance with 6.6 on whether
the flight is a controlled flight or not.
The sound signal requirement is not implemented.
There is no requirement for the carriage of a noise certificate in an aeroplane.
Australia does not require fitment of GPWS to any piston-engincd aeroplanes, whether above or below
5 700 kg MCTOM.
Australia will apply this requirement to all turbine-powered aeroplanes greater than 15 000 kg MCTOM
or carrying 10 or more passengers in passenger transport operations under the IFR from 1 July 200.5.
Australian lcgislation does not refer lo FDRs by Type, but specifies the parameters to bc recorded.
Metal foil FDRs are still permitted.
Current legislation specifies that analogue recorders will not be approved for fitment to aircraft which
receive their initial use Certificate of Airworthiness afer 1 January 1984.
Photographic film recorders are not approvcd.
Currently there are no legislative requirements to give effect to these standards.
Auslralian lcgislation does not refer to combination recorders
"Recommended Practice
2 AU~~RALIA SUPPLE MEW^ TO ANNEX 6, PART1 1 (SIXTHE DITION)
6.10.1.7 Australian legislation does no1 refer to FDRs by Type. Parameters currently required to be recorded are
6.10.1.7.1 to less comprehensive than the Annex Standards.
6.10.1.7.5
6.10.3.1 Australian legislation does no^ mention FDR by Typc and establishes the weight break at 29 000 kg.
6.10.3.2"
6.10.4
CHAPTER 7
The weight break is established at 29 000 kg rather than 27 000 kg.
Australia does not require non-turbine aircraft certificated before 1 July 1965 to be fitted with a CVR.
Australian legislation requires only a thirty-minute duration.
　
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