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j) new provisions concerning the carriage of airborne collision avoidance
(ACAS) systems and pressure-altitude reporting transponders; and
k) new provisions concerning Human Factors.
a) Change of terminology from "cabin attendant" to "cabin crew";
b) revised definitions;
C) new provisions concerning the mandatory carriage of ELTs operating on
406 MHz and 121.5 MHz, the addition of a predictive terrain hazard warning
function to the ground proximity warning system (GPWS) and the
introduction of an implementation date for the recording of digital
communications.
15 March 1999
19 July 1999
4 November 1999
a) Revised definitions; and 15 March 2000
17 July 2000
b) introduction of requirements for the provision of RVR and criteria for 2 November 2000
instrument approach operations, and revision of the duties of the pilot-incommand.
a) Update the provisions pertaining to flight recorders, including the recording 9 March 2001
of digital communications; FDR requirements for new aircraft; revised 16 July 2001
parameter listings; introduction of two-hour duration CVRs; 1 November 2001
b) new provisions pertaining to flight data analysis programmes;
c) amendment of the classification of instrument approach and landing
operations;
d) new provisions pertaining to approach with vertical guidance (APV)
operations;
e) new definitions and update of provisions pertaining to maintenance-related
requirements; and
f) translation into English of documents attesting noise certification.
a) Revised requirements for the ground proximity warning system (GPWS) and 15 March 2002
forward looking terrain avoidance function; and 15 July 2002
28 November 2002
b) new and revised requirements for the incorporation of security into aircraft
design.
2811 1/02
No. 27
Chapter 6 Annex 6 - Operation of Aircraft
weather radar, ma). be exp~ctedto exist along the route either
at night or under instr~~memnte teorological conditions.
6.12 All aeroplanes operated
above 15 000 m (49 000 ft) -
radiation indicator
All aeroplanes intended to be operated above 15 000 m
(49 000 ft) shall carry equipment to measure and indicate
continuously the dose rate of total cosmic radiation being
received (i.e. the total of ionizing and neutron radiation of
galactic and solar origin) and the cumulative dose on each
flight. The display unit of the equipment shall be readily
visible to a flight crew member.
Note.- The equipment is calibrated on the basis of
assumptions acceptable to the appropriate national
authorities.
6.13 All aeroplanes complying with
the noise certification Standards
in Annex 16, Volume I
An aeroplane shall cany a document attesting noise
certification. When the document, or a suitable statement
attesting noise certification as contained in another document
approved by the State of Registry, is issued in a language other
than English, it shall include an English translation.
Note.- The attestation may be contained in any document,
carried on board, approved by the State of Registry.
6.14 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.
to carry more than 30 passengers, for which the individual
certificate of airworthiness is first issued on or after 1 January
2001, shall be equipped with a ground proximity warning
system which has a forward looking terrain avoidance
function.
6.15.3 From 1 January 2003, all turbine-engined
aeroplanes of a maximum certificated take-off mass in excess
of 15 000 kg or authorized to cany more than 30 passengers
shall be equipped with a ground proximity warning system
which has a forward looking terrain avoidance function.
6.15.4 All turbine-engined aeroplanes of a maximum
certificated take-off mass in excess of 5 700 kg or authorized
to carry more than nine passengers, for which the individual
certificate of airworthiness is first issued on or after 1 January
2004, shall be equipped with a ground proximity warning
system which has a forward looking terrain avoidance
funcdon.
6.15.5 From 1 January 2007, all turbine-engined
aeroplanes of a maximum certificated take-off mass in excess
of 5 700 kg or authorized to carry more than nine passengers,
shall be equipped with a ground proximity warning system
which has a forward looking terrain avoidance function.
6.15.6 Recommendation.- All turbine-engined aeroplanes
of a maximum certi$icated take-off mass of 5 700 kg or
　
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