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satisfactory performance of the flight crews' duties.
F.5 Electromagnetic interference protection
Aircraft electronic systems, particularly flight-critical and
flight-essential systems, shall be protected as appropriate
against electromagnetic interference from both internal and
external sources.
ANNEX 8 IVB-F-1
Annex 8 - Airworthiness of Aircraft
F.6 Ice protection
If certification for flight in icing conditions is required, the
helicopter shall be shown to be able to operate safely in all
icing conditions likely to be encountered in all anticipated
operating environments.
Part IVB
SUB-PART G. OPERATING LIMITATIONS AND INFORMATION
G1 General G2.6 Limitations on equipment and systems
The operating limitations within which compliance with the The limitations on equipment and systems shall include all
Standards of this Annex is determined, together with any other those established for the various equipment and systems as
information necessary to the safe operation of the helicopter, installed in the helicopter.
shall be made available by means of a flight manual, markings
and placards, and such other means as may effectively
accomplish the purpose. G2.7 Miscellaneous limitations
6 2 Operating limitations
Miscellaneous limitations shall include any necessary limitations
with respect to conditions found to be prejudicial to the
safety of the helicopter (see A.2.1).
G2.1 Limitations which might be exceeded in flight and
which are defined quantitatively shall be expressed in suitable G.2.8 Flight crew limitations
units. These limitations shall be corrected if necessary for
errors in IIleaSU~ementSS O that the flight crew can, by refer- The flight crew limitations shall include the number
mce to the instruments available to them, readily determine of flight crew personnel necessary to operate the helicopter,
when the limitations are reached. 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
G.2.2 Loading limitations procedures.
The loading limitations shall include all limiting masses, Note.- See Annex 6 - Operation of Aircraft, Part 111, for
centres of gravity positions, mass distributions and floor the circumstances in which theflight crew includes members in
loadings (see A.2.2). addition to the minimum jlight crew defined in this Annex.
G.2.3 Airspeed limitations
G3 Operating information and procedures
The airspeed limitations shall include all speeds (see C.5.2)
that are limiting from the standpoint of structural integrity or
flying qualities of the helicopter, or from other considerations. G3.1 Types of eligible operations
These speeds shall be identified with respect to the appropriate
helicopter configurations and other pertinent factors. The particular types of operations for which the helicopter has
been shown to be eligible by virtue of compliance with the
appropriate airworthiness requirements shall be listed.
G2.4 Powerplant limitations
The powerplant limitations shall include all those established G3.2 Loading information
for the various powerplant components as installed in the
helicopter (see E.2.5 and E.2.8.3). 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
G.2.5 Rotor limitations gravity position, and the reference points and datum lines to
which the centre of gravity limits are related.
Limitations on rotor speeds shall include maximum and
minimum rotor speeds for power-off (autorotation) and power- Note.- Usually the empty mass excludes the mass of the
on conditions. crew and paybad, and the usable fuel supply; it includes the
ANNEX 8 IVB-G-1 13/12/07
Annex 8 - Airworthiness of Aircraft Part IVB
mass of all fixed ballast, unusable fuel supply and total
quantity of oil, engine coolant and hydraulic fluid.
G3.3 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 engines.
G3.4 Handling information
Sufficient information shall be given on any significant or
unusual features of the helicopter characteristics.
G4 Performance information
The performance of the helicopter shall be scheduled in
accordance with B.2. There shall be included information
regarding the various helicopter configurations and powers
involved and the relevant speeds, together with information
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附件8--航空器适航性 Airworthiness of Aircraft(60)
