SUB-PART G. G.1
OPERATING LIMITATIONS AND INFORMATION
General
G.2.6
The operating limitations within which compliance with the Standards of this Annex is determined, together with any other information necessary to the safe operation of the aeroplane, shall be made available by means of a flight manual, markings and placards, and such other means as may effectively accomplish the purpose. The limitations and information shall include at least those prescribed in this sub-part.
G.2 Operating limitations G.2.1 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. --`,,```,,,,````-`-`,,`,,`,`,,`---
G.2.2
Miscellaneous limitations shall include any necessary limitations with respect to conditions found to be prejudicial to the safety of the aeroplane (see A.2.1).
G.2.7 Flight crew limitations The flight crew limitations shall include the minimum number of flight crew personnel necessary to operate the aeroplane, 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, Parts I and II, for the circumstances in which the flight crew shall include members in addition to the minimum flight crew defined in this Annex.
Loading limitations
The loading limitations shall include all limiting masses, centres of gravity positions, mass distributions and floor loadings (see A.2.2). G.2.3
G.3
The powerplant limitations shall include all those established for the various powerplant components as installed in the aeroplane (see E.3.1 and E.3.5.3). 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 aeroplane.
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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.
G.3.2 Loading information
G.2.4 Powerplant limitations
ANNEX 8
Operating information and procedures
G.3.1 Types of eligible operations
Airspeed limitations
The airspeed limitations shall include all speeds (see C.5) that are limiting from the standpoint of structural integrity or flying qualities of the aeroplane, or from other considerations. These speeds shall be identified with respect to the appropriate aeroplane configurations and other pertinent factors.
G.2.5
Miscellaneous limitations
The loading information shall include the empty mass of the aeroplane, together with a definition of the condition of the 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 fixed ballast, unusable fuel supply, undrainable oil, total quantity of engine coolant and total quantity of hydraulic fluid.
V-G-1
Not for Resale
13/12/07