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aeroplane (see E.3.1 and E.3.5.3). The particular types of operations for which the aeroplane has
been shown to be eligible by virtue of compliance with the
appropriate airworthiness requirements shall be listed.
G2.5 Limitations on
equipment and systems
(23.2 Loading information
The limitations on equipment and systems shall include all
those established for the various equipment and systems as The loading information shall include the empty mass of the
installed in the aeroplane. aeroplane, together with a definition of the condition of the
ANNEX 8 IIIB-G-1 13/12/07
Annex 8 - Ainvorfhiness of Aircrajl Part ZZZB
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 fuel supply and the drainable
oil; it includes the mass of all fined ballast, unusable fuel
supply, undrainable oil, total quantity of engine coolant and
total quantity of hydraulic fluid.
G3.3 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.
G6 Markings and placards
G6.1 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.
G6.2 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.
G7 Continuing airworthiness -
maintenance information
G3.4 Handling information G7.1 General
Sufficient information shall be given on any significant or Information for use in developing procedures for maintaining
unusual features of the aeroplane characteristics. Those stall- the aeroplane in an airworthy condition shall be made
ing speeds or minimum steady flight speeds required to be available. The information shall include that described in
established by B.4.2.3 shall be scheduled. G7.2, G7.3 and G7.4.
G3.5 Least-risk bomb location G7.2 Maintenance information
For aeroplanes of a maximum certificated take-off mass in ~ ainformatioin shall incl~ude a descr~iption of th~e ~ excess of 45 500 kg or with a Passenger seating capacity aeroplane and recommended methods for the accomplishment
greater than 60, a least-risk location on the be of maintenance tasks, Such infomation shall include guidance
identified where a bomb or other explosive device may be on defect diagnosis.
placed to minimize the effects on the aeroplane in the case of
detonation.
G7.3 Maintenance programme
information
G4 Performance information
Maintenance programme information shall include the mainl-
he perfomance of the aeroplane shall be scheduled in tenance tasks and recommended intervals at which these tasks
accordance with B.2. There shall be included information are to be performed.
regarding the various aeroplane configurations and powers or
thrusts involved and the relevant speeds, together with Note.- The development of initial maintenance programme
infomation that would assist the fight crew in attaining the information at the time of aeroplane type certijkation is some
performance as scheduled. times referred to as the Maintenance Review Board (MRB)
process.
G5 Flight manual G7.4 Mandatory maintenance requirements
resulting from the type design approval
A flight manual shall be made available. It shall identify
clearly the specific aeroplane or series of aeroplanes to which Mandatory maintenance requirements that have been specified
it is related. The flight manual shall include at least the by the State of Design as part of the approval of the type
limitations, information and procedures specified in G.2, G.3, design shall be identified as such and included in the
G.4 and G.6.1. maintenance information of G.7.3.
Sub-part G Annex 8 - Airworthiness of Aircraft
Note.- Mandatory requirements identified as part of the
type design approval are often referred to as Certification
Maintenance Requirements (CMRJ andor airworthiness
limitations.
SUB-PART H. SYSTEMS SOFTWARE
All systems software shall be designed and validated such as
to ensure that the systems in which software is used perform
their intended functions with a level of safety that complies
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附件8--航空器适航性 Airworthiness of Aircraft(40)
