FAA | EASA |
Regulation/standard | |
CFR 14 25.1309 - Airworthiness standards equipment Failure condition: 1. Reducing ability of crew to cope with adverse operating conditions. ・ Improbable | CS 25.1309 - Equipment, systems and installation design requirements Failure condition: 1. Major ・ Remote 2. Hazardous ・ Extremely remote |
Guidance Material (Advisory Circular - CS AMC) | |
AC 25.1309-1A - Failure conditions 1. Minor: Crew actions well within capabilities - slight increase in workload - some inconvenience to occupants. ・ Probable ・ >1 × 10−5/fh 2. Major: - Conditions impairing crew efficiency or some discomfort to occupants; - Higher workload or physical distress such that crew can’t be relied upon to perform tasks accurately or completely. ・ Improbable ・ ≤1 × 10−5 - > 1 × 10−9/fh | AMC 25.1309 - Failure conditions 1. Minor: Crew actions well within capabilities-slight increase in workload - some physical discomfort to cabin crew or passengers. ・ Probable ・ >1 × 10−5/fh (Table 2) 2. Major: - Conditions impairing crew efficiency or discomfort to flight crew - Physical distress to cabin crew or passengers, possibly including injuries ・ Remote ・ ≤ 1 × 10−5 - > 1 × 10−7/fh. 3. Hazardous: excessive workload or physical distress such that flight crew can’t be relied upon to perform tasks accurately or completely - serious or fatal injury to a small number of occupants other than flight crew. ・ Extremely remote ・ ≤1 × 10−7 - > 1 × 10−9/fh |
Anticipation of failure conditions ・ Probable: One or more times during entire operational life of each aeroplane; ・ Improbable (FAA): Will not occur during entire operational life of a single random aeroplane - may occur occasionally during life of all aeroplanes of type; ・ Remote (EASA): Unlikely to occur to each aeroplane during its total life, but may occur several times during life of a number of aircraft of type; ・ Extremely remote (EASA): Will not occur to each aeroplane during its life but may occur a few times during total life of all aeroplanes of type. Compliance shown by analysis and where necessary, appropriate ground, flight or simulator tests. |