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recorders shall be deactivated upon completion of flight time
following an accident or incident. The flight recorders shall
not be re-activated before their disposition as determined in
accordance with Annex 13.
Note 1.- The need for removal of the flight recorder
records from the aircraf will be determined by the investigation
authority in the State conducting the investigation
with due regard to the seriousness of an occurrence and the
circumstances, including the impact on the operation.
Note 2.- The pilot-in-command's responsibilities
regarding the retention of flight recorder records are
contained in 6.10.9.
6.10.9 Flight recorder records
The pilot-in-command shall ensure, to the extent possible, in
the event the aeroplane becomes involved in an accident or
incident, the preservation of all related flight recorder records,
and if necessary the associated flight recorders, and their
retention in safe custody pending their disposition as
determined in accordance with Annex 13.
6.10.10 Flight recorders - continued
serviceability
Operational checks and evaluations of recordings from the
flight data and cockpit voice recorder systems shall be conducted
to ensure the continued serviceability of the recorders.
Note.- Procedures for the inspections of the flight data and
cockpit voice recorder systems are given in Attachment A.
6.11 Mach number indicator
All aeroplanes with speed limitations expressed in terms of
Mach number shall be equipped with a Mach number indicator.
Note.- This does not preclude the use of the airspeed
indicator to derive Mach number for ATS purposes.
6.12 Emergency locator
transmitter (ELT)
6.12.1 Except as provided for in 6.12.2, until
1 January 2005 all aeroplanes operated on extended flights
over water as described in 6.3.3 b) and when operated on
flights over designated land areas as described in 6.4 shall be
equipped with one ELT.
6.12.2 All aeroplanes for which the individual certificate
of airworthiness is first issued after 1 January 2002, operated
on extended flights over water as described in 6.3.3 b) and
when operated on flights over designated land areas as
described in 6.4 shall be equipped with one automatic ELT.
6.12.3 From 1 January 2005, all aeroplanes operated on
extended flights over water as described in 6.3.3 b) and when
operated on flights over designated land areas as described in
6.4 shall be equipped with one automatic ELT.
6.12.4 Recommendation.- All aeroplanes should carry
an automatic ELK
24/11105
No. 24
Annex 6 - Opemlion of Aircrafr Part ZI
6.12.5 ELT equipment carried to satisfy the requirements
of 6.12.1,6.12.2, 6.12.3 and 6.12.4 shall operate in accordance
with the relevant provisions of Annex 10, Volume III.
6.13 Aeroplanes required
to be equipped with a
pressure-altitude reporting transponder
6.13.1 From 1 January 2003, unless exempted by the
appropriate authorities, all aeroplanes shall be equipped with a
pressure-altitude reporting transponder which operates in
accordance with the relevant provisions of Annex 10.
Volume IV.
6.13.2 Recommendation.- All aeroplanes should be
equipped with a pressure-altitude reporting transponder which
operates in accordance with the relevant provisions of
Annex 10, Volume N.
Note.- The provisions in 6.13.1 and 6.13.2 are intended to
support the effectiveness of ACAS as well as to improve the
effectiveness of air traffic services. Effective dates for carriage
requirements of ACAS are contained in Annex 6, Part 1, 6.18.1
and 6.18.2. The intent is also for aircraf not equipped with
pressure-altitude reporting transponders to be operated so as
not to share airspace used by aircraft equipped with airborne
collision avoidance systems. To this end, exemptions from the
carriage requirement for pressure-altitude reporting transponders
could be given by designating airspace where such
carriage is not required.
6.14 Aeroplanes required to be equipped with an
airborne collision avoidance system (ACAS 11)
6.14.1 Recommendation.- All turbine-engined aeroplanes
of a maximum certificated take-off mass in excess of
15 000 kg, or authorized to carry more than 30 passengers, Jor
which the individual airworthiness certz$cate is first issued
afer 24 November 2005, should be equipped with an airborne
collision avoidance system (ACAS 11).
6.14.2 All turbine-engined aeroplanes of a maximum
certificated take-off mass in excess of 15 000 kg, or authorized
to carry more than 30 passengers, for which the individual
airworthiness certificate is first issued after 1 January 2007,
　
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