CS-E 210 Failure Analysis

• ED Decision 2007/015/R found in: CS-E Amdt 5 - Engines (Dec 2018)

CS-E 210 Failure Analysis ED Decision 2007/015/R (See [AMC E 210](#_DxCrossRefBm1371447683)) (a) A Failure analysis of the Engine, including the control system for a typical installation must be made to establish that no single Fault, or double Fault if one of the Faults may be present and undetected during pre-flight checks, could lead to unsafe Engine conditions beyond the normal control of the flight crew. (b) In certain cases the Failure analysis will depend on assumed installed conditions. Such assumptions must be stated in the analysis. [Amdt. No.: E/1]