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passenger seating capacity;
c) revision of design, construction and security provisions in Annex 8,
Parts IIIA and IIIB with regard to aeroplanes of a maximum
certificated take-off mass in excess of 45 500 kg or with a passenger
seating capacity greater than 60 and for which an application for
certification was submitted on or after 12 March 2000 and
2 March 2004, respectively, and introduction of Recommended
Practices for aircraft of a maximum certificated take-off mass between
5 700 kg and 45 500 kg;
d) introduction of Recommended Practices regarding security provisions
for application to aeroplanes engaged in domestic commercial
operations;
e) introduction of security provisions for all aeroplanes which are
required by Annex 6 to have an approved flight crew compartment
door providing additional protection to also require additional
protection of the bulkheads, floors and ceilings; and
f) addition of provisions in Part IIIB for operating information and
procedures to require the identification of a least-risk bomb location.
100 First meeting of the
(10th Edition) Airworthiness Panel
a) new definitions of Category A, Category B, discrete source damage, 13 December 2004
engine, fireproof, fire resistant and satisfactory evidence, new note to 13 April 2005
critical power-unit; 13 December 2007
b) amendment to the definition of repair;
c) revision of the provisions of Part I1 to allow the introduction of new
parts in the Annex, amend Chapter 3 to clarify provisions relating to
the limiting conditions under which a damaged aircraft is permitted to
fly uncornmercially to an aerodrome where it can be restored to an
airworthy condition, and re-organize Chapter 4 to clarify States'
responsibilities;
d) revision of provisions in Part IIIA pertaining to applicability and
operating limitations, proof of compliance;
e) revision of provisions in Part IIIB pertaining to applicability,
operating limitations, performance, stability, structure, design and
construction, powerplant, operating limitations, crashworthiness and
cabin safety, operating environment and Human Factors;
f) restructuring of Part IV into Part IVA (same provisions as those
contained in Part IV of Annex 8, Ninth Edition including
Amendment 99, except for applicability clauses and cross-references)
and Part IVB (new);
g) introduction of new Part V - Small Aeroplanes, Part VI - Engines
and Part VII - Propellers.
INTERNATIONAL STANDARDS
AND RECOMMENDED PRACTICES
PART I. DEFINITIONS
When the following terms are used in the Standards for the
Airworthiness of Aircraft, they have the following meanings:
Aeroplane. A power-driven heavier-than-air aircraft, deriving
its lift in flight chiefly from aerodynamic reactions on
surfaces which remain fixed under given conditions of
flight.
Aircrafi. Any machine that can derive support in the atmosphere
from the reactions of the air other than the reactions
of the air against the earth's surface.
Anticipated operating conditions. Those conditions which are
known from experience or which can be reasonably
envisaged to occur during the operational life of the aircraft
taking into account the operations for which the aircraft is
made eligible, the conditions so considered being relative
to the meteorological state of the atmosphere, to the
configuration of terrain, to the functioning of the aircraft, to
the efficiency of personnel and to all the factors affecting
safety in flight. Anticipated operating conditions do not
include:
a) those extremes which can be effectively avoided by
means of operating procedures; and
b) those extremes which occur so infrequently that to
require the Standards to be met in such extremes would
give a higher level of airworthiness than experience has
shown to be necessary and practical.
Appropriate airworthiness requirements. The comprehensive
and detailed airworthiness codes established, adopted or
accepted by a Contracting State for the class of aircraft,
engine or propeller under consideration (see 3.2.2 of Part I1
of this Annex).
Approved Accepted by a Contracting State as suitable for a
particular purpose.
Category A. With respect to helicopters, means a multi-engine
helicopter designed with engine and system isolation
features specified in Part IVB and capable of operations
using take-off and landing data scheduled under a critical
engine failure concept which assures adequate designated
surface area and adequate performance capability for
continued safe flight or safe rejected take-off.
Category B. With respect to helicopters, means a single-engine
　
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