A newly-developed 
aviation electronic product hardware comprehensive FMECA method comprises the first step of defining a 
system to be analyzed, the second step of determining fault 
modes and reasons of appointed 
layers of a product based on a fault information 
database, fault mechanism analyzing and a fault module 
exposure test method, the third step of acquiring fault effects based on a fault 
simulation analytical method, the fourth step of carrying out the quantification 
hazard analysis, taking the 
multiple fault effects caused by the redundancy design into consideration and providing a quantification 
hazard analyzing method based on the 
multiple fault effects, and the fifth step of 
filling in an FMECA table and filling the fault 
modes, the reasons, the effect and the 
hazard degree all of which are acquired through analyzing into the FMECA table. The newly-developed 
aviation electronic product hardware comprehensive FMECA method is a hardware FMECA method based on the fault information 
database, fault mechanism analyzing, fault mode 
exposure testing, fault simulating and analyzing and the 
multiple fault effects, and is capable of providing more objective quantification for design and analyze workers and providing a basis for the 
design improvement on electronic products.