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the i'jpe Certificate to include a derivative type design is
submitted to the appropriate national authority, consideration
should be given to reinforcing the flight crew compartment
bulkheadr, floors and ceilings so as to mist penetmtion by
small arms fire and grenade shrapnel and to mist forcible
intrusions, ifthese areas are accessible in flight to passengers
and cabin crew.
Note.- Standardr and Recommended Practices concerning
the requirements for the flight crew compartment door in all
commercial passenger-carrying aeroplanes are contained in
Annex 6, Part I, Chapter 13.
11.4 Interior design
For 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 the application for certification
was submitted on or after 12 March 2000, consideration shall
be given to design features that will deter the easy concealment
of weapons, explosives or other dangerous objects on
board aircraft and that will facilitate search procedures for
such objects.
ANNEX 8
PART IIIB. AEROPLANES OVER 5 700 KG FOR WHICH APPLICATION FOR
CERTIFICATION WAS SUBMITTED ON OR AETER 2 MARCH 2004
SUB-PART A. GENERAL
A.l Applicability
A. 1.1 The Standards of this part are applicable in respect
of all aeroplanes designated in A. 1.2 for which an application
for the issue of a Type Certificate is submitted to the appropriate
national authorities on or after 2 March 2004.
A.1.2 Except for those Standards and Recommended
Practices which specify a different applicability, the Standards
and Recommended Practices of this part shall apply to all
aeroplanes over 5 700 kg maximum certificated take-off mass
intended for the carriage of passengers or cargo or mail in
international air navigation.
Note I.- The aeroplanes described in A.1.2 are known in
some States as transport category aeroplanes.
Note 2.- The following Standad do not include quantitative
specifications comparable to those found in national
airworthiness codes. In accordance with 1.2.1 of Part 11, these
Standards are to be supplemented by requirements established,
adopted or accepted by Contracting States.
A. 1.3 The level of airworthiness defined by the appropriate
parts of the comprehensive and detailed national code
referred to in 1.2.1 of Part I1 for the aeroplanes designated in
A.1.2 shall be at least substantially equivalent to the overall
level intended by the broad Standards of this part.
A.1.4 Unless otherwise stated, the Standards apply to the
complete aeroplane including power-units, systems and
equipment.
A.2 Operating limitations
A.2.1 Limiting conditions shall be established for the
aeroplane, its power-units and its equipment (see (22).
Compliance with the Standards of this part shall be established
assuming that the aeroplane is operated within the limitations
specified. The limitations shall include a margin of safety to
render the likelihood of accidents arising therefrom extremely
remote.
Note.- Guidance material concerning the expmsion
"extremely remote" is contained in the Airworthiness Manual
(Doc 9760).
A.2.2 Limiting ranges of any parameter whose variation
may compromise the safe operation of the aeroplane, e.g.
mass, centre of gravity location, load distribution, speeds,
ambient air temperature and altitude or pressure-altitude, shall
be established within which compliance with all the pertinent
Standards in this part is shown.
Note.- Maximum operating mass may be limited by the
application of Noise Certifcation Standards (see Annex 16,
Volume I, and Annex 6, Parts I and II).
A3 Unsafe features and characteristics
Under all anticipated operating conditions, the aeroplane shall
not possess any feature or characteristic that renders it unsafe.
A.4 Proof of compliance
The means by which compliance with the appropriate airworthiness
requirements is demonstrated shall ensure that in
each case the accuracy achieved will be such as to provide
reasonable assurance that the aeroplane, its components and
equipment comply with the requirements and are reliable and
function correctly under the anticipated operating conditions.
ANNEX 8
SUB-PART B. FLIGHT
B.l General
B. 1.1 Compliance with the Standards prescribed in this
Sub-part shall be established by flight or other tests conducted
upon an aeroplane or aeroplanes of the type for which a Qpe
Certificate is sought, or by calculations based on such tests,
provided that the results obtained by calculations are equal in
accuracy to, or conservatively represent, the results of direct
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附件8--航空器适航性 Airworthiness of Aircraft(30)
