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[Extra Quality] Download Norma Cei 82 25 Pdf

Download Norma Cei 82 25 Pdf ->->->->

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The airplane must be longitudinally, directionally, and laterally stable in accordance with the provisions of 25.173 through 25.177. In addition, suitable stability and control feel (static stability) is required in any condition normally encountered in service, if flight tests show it is necessary for safe operation.

Within the range of appropriate ground speeds and approved weights, the airplane structure and landing gear are assumed to be subjected to loads not less than those obtained when the aircraft is operating over the roughest ground that may reasonably be expected in normal operation.

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