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installed in the aeroplane. aeroplane, together with a definition of the condition of the
ANNEX 8 IIIA-9-1 13/12/07
Annex 8 -Airworthiness of Aircmfi
aeroplane at the time of weighing, the corresponding centre of
gravity position, and the reference points and datum lines to
which the centre of gravity limits are related.
Note.- Usually the empty mass excludes the mass of the
crew and payload, the usable &el supply and the drainable
oil; it includes the mass of all fured ballart, unusable &el
supply, undrainable oil, total quantity of engine coolant and
total quantity of hydraulic fluid.
9.3.3 Operating procedures
A description shall be given of normal and emergency
operating procedures which are peculiar to the particular
aeroplane and necessary for its safe operation. These shall
include procedures to be followed in the event of failure of one
or more power-units.
9.3.4 Handling information
Sufficient information shall be given on any significant or
unusual features of the aeroplane characteristics. Those stalling
speeds or minimum steady flight speeds required to be
established by 2.3.4.3 shall be scheduled.
9.3.5 Least-risk bomb location
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, a least-risk location
on the aeroplane shall be identified where a bomb or other
explosive device may be placed to minimize the effects on the
aeroplane in the case of detonation.
9.4 Performance information
The performance of the aeroplane shall be scheduled in
accordance with 2.2. There shall be included information
regarding the various aeroplane configurations and powers
involved and the relevant speeds, together with information
that would assist the flight crew in attaining the performance
as scheduled.
9.5 Aeroplane flight manual
A flight manual shall be made available. It shall identify
clearly the specific aeroplane or series of aeroplanes to which
it is related. The flight manual shall include at least the limitations,
information and procedures specified in this chapter.
9.6 Markings and placards
9.6.1 Markings and placards on instruments, equipment,
controls, etc., shall include such limitations or information as
necessary for the direct attention of the flight crew during
flight.
9.6.2 Markings and placards or instructions shall be
provided to give any information that is essential to the ground
crew in order to preclude the possibility of mistakes in ground
servicing (e.g. towing, refuelling) that could pass unnoticed
and that could jeopardize the safety of the aeroplane in
subsequent flights.
CHAPTER 10. CONTINUING AIRWORTHINESS -
MAINTENANCE INFORMATION
10.1 General 103 Maintenance programme
information
Information for use in developing procedures for maintaining
the aeroplane in an airworthy condition shall be made avail- Maintenance programme information shall include the mainable.
The information shall include that described in 10.2, 10.3 tenance tasks and the recommended intervals at which these
and 10.4. tasks are to be performed.
10.2 Maintenance information 10.4 Maintenance information resulting from
the type design approval
Maintenance information shall include a description of the
aeroplane and recommended methods for the accomplishment Maintenance tasks and frequencies that have been specified as
of maintenance tasks. Such information shall include guidance mandatory by the State of Design in approval of the type
on defect diagnosis. design shall be identified as such.
ANNEX 8
CHAPTER 1 1. SECURITY
11.1 Aeroplanes used for domestic
commercial operations
Recommendation.- International Standards and Recommended
Practices set forth in this chapter should be applied by
all Contracting States for aeroplanes engaged in domestic
commercial operations (air services).
11.2 Least-risk bomb location
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 during the design of the aeroplane to the provision of
a least-risk bomb location so as to minimize the effects of a
bomb on the aeroplane and its occupants.
11.3 Protection of the flight crew compartment
Recommendation.- In all aeroplanes, which are required by
Annex 6, Part I, Chapter 13 to have an approvedflight crew
compartment dool; and for which an application for amending
　
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