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effectively accomplish the purpose. The limitations and
information shall include at least those prescribed in 9.2, 9.3
and 9.4.
9.2 Operating limitations
Limitations which there is a risk of exceeding in flight and
which are defined quantitatively shall be expressed in suitable
units and corrected if necessary for errors in measurements so
that the flight crew can, by reference to the instruments
available to them, readily determine when the limitations are
reached.
9.2.1 Loading limitations
The loading limitations shall include all limiting masses,
centres of gravity positions, mass distributions and floor
loadings (see 1.2.2).
9.2.2 Airspeed limitations
The airspeed limitations shall include all speeds (see 3.2) that
are limiting from the standpoint of structural integrity or flying
qualities of the helicopter, or from other considerations. These
speeds shall be identified with respect to the appropriate helicopter
configurations and other pertinent factors.
9.2.3 Powerplant and power transmission
limitations
The powerplant limitations shall include all those established
for the various powerplant and transmission components as
installed in the helicopter (see 6.5 and 6.6).
9.2.4 Rotor limitations
Limitations on rotor speeds shall include maximum and
minimum rotor speeds for power-off (autorotation) and
power-on conditions.
9.2.5 Limitations on equipment
and systems
The limitations on equipment and systems shall include all
those established for the various equipment and systems as
installed in the helicopter.
9.2.6 Miscellaneous limitations
Miscellaneous limitations shall include any necessary limitations
with respect to conditions found to be prejudicial to the
safety of the helicopter (see 1.2.1).
9.2.7 Flight crew limitations
The flight crew limitations shall include the minimum number
of flight crew personnel necessary to operate the helicopter,
having regard, among other things, to the accessibility to the
appropriate crew members of all necessary controls and
instruments and to the execution of the established emergency
procedures.
Note.- See Annex 6 - Operation of Aircraft, Part 111, for
the circumstances in which the flight crew shall include
members in addition to the minimumflight crew defined in this
Annex.
9.3 Operating information and
procedures
9.3.1 Types of eligible operations
There shall be listed the particular types of operations, as may
be defined in Annex 6, Part III, or be generally recognized, for
which the helicopter has been shown to be eligible by virtue of
compliance with the appropriate airworthiness requirements.
9.3.2 Loading information
The loading information shall include the empty mass of the
helicopter, together with a definition of the condition of the
helicopter 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.
ANNEX 8 IVA-9-1 13/12/(n
Annex 8 - Airworthiness of Aircrafi Part ZVA
N o t e . 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 fixed ballast, unusable fiel
supply, undrainable oil, total quantity of engine coolant and
total quantity of hydraulic jluid.
9.3.3 Operating procedures
A description shall be given of normal and emergency operating
procedures which are peculiar to the particular helicopter
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 helicopter characteristics.
9.4 Performance information
The performance of the helicopter shall be scheduled in
accordance with 2.2. There shall be included information
regarding the various helicopter 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 Helicopter flight manual
A flight manual shall be made available. It shall identify
clearly the specific helicopter or series of helicopters 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
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附件8--航空器适航性 Airworthiness of Aircraft(51)
