Publication: Magyar Közlöny
Issue: MK-2007-70 (Year: 2007, Number: 70)
Era: 2004-2010
Section: Melléklet a 2007. évi XLVI. törvényhez
Paragraph Index: 2853

g) likely structural repairs. Note.— Guidance material concerning the expression “extremely remote” is contained in the Airworthiness Manual (Doc 9760), Volume II, Part A. C.9 Lightning protection The aeroplane shall be protected against catastrophic effects of lightning. Due account shall be taken of the materials used in the construction of the aeroplane. 2007/70/II. szám ANNEX 8 IIIB-D-1 2/3/04 SUB-PART D. DESIGN AND CONSTRUCTION D.1 General D.1.1 Details of design and construction shall be such as to give reasonable assurance that all aeroplane parts will function effectively and reliably in the anticipated operating conditions. They shall be based upon practices that experience has proven to be satisfactory or that are substantiated by special tests or by other appropriate investigations or both. They shall also observe Human Factors principles. Note.— Guidance material on Human Factors principles can be found in the Human Factors Training Manual (Doc 9683). D.1.2 Substantiating tests The functioning of all moving parts essential to the safe operation of the aeroplane shall be demonstrated by suitable tests in order to ensure that they will function correctly under all operating conditions for such parts. D.1.3 Materials All materials used in parts of the aeroplane essential for its safe operation shall conform to approved specifications. The approved specifications shall be such that materials accepted as complying with the specifications will have the essential properties assumed in the design. The effect of the materials on the occupants of the aeroplane and other persons on the ground, and the environment in general, in normal and emergency situations, shall be taken into account. D.1.4 Fabrication methods The methods of fabrication and assembly shall be such as to produce a consistently sound structure which shall be reliable with respect to maintenance of strength in service. D.1.5 Protection The structure shall be protected against deterioration or loss of strength in service due to weathering, corrosion, abrasion, or other causes, which could pass unnoticed, taking into account the maintenance the aeroplane will receive. D.1.6 Inspection provisions Adequate provision shall be made to permit any necessary examination, replacement, or reconditioning of parts of the aeroplane that require such attention, either periodically or after unusually severe operations. D.2 Systems design features Special consideration shall be given to design features that affect the ability of the flight crew to maintain controlled flight. This shall include at least the following:

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