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In-flight upset - 154 km west of Learmonth, WA, 7 October 2008,

In-flight upset - 154 km west of Learmonth, WA, 7 October 2008,

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Table 22: Probability levels described in ACJ No. 1 to JAR 25.1309ProbabilitylevelQualitative definition Quantitative description 92Probable 93Remote(category <strong>of</strong>improbable)Extremelyremote(category <strong>of</strong>improbable)Extremelyimprobablemay occur once or several times during thetotal operational life <strong>of</strong> each aeroplane <strong>of</strong>the same typeunlikely to each aeroplane during its totaloperational life but which may occurseveral times when considering the totaloperational life <strong>of</strong> a number <strong>of</strong> aeroplanes<strong>of</strong> the same typeunlikely to occur when considering thetotal operational life <strong>of</strong> all aeroplanes <strong>of</strong>the same type, but nevertheless, has tobe considered as being possibleso extremely remote that it does not haveto be considered as possible to occur> 10 -5 per <strong>flight</strong> hour10 -5 to 10 -7 per <strong>flight</strong> hour10 -7 to 10 -9 per <strong>flight</strong> hour< 10 -9 per <strong>flight</strong> hour2.3.4 United States Advisory Circular 25.1309-1AThe FAA released Advisory Circular 25.1309-1A (System design and analysis) inJune 1988. When it was released, it provided more detailed guidance than the ACJregarding the methods that could be used to satisfy the requirements <strong>of</strong>FAR 25.1309. The background section <strong>of</strong> the document noted that there had been‘an increase in the degree <strong>of</strong> system complexity and integration, and in the number<strong>of</strong> safety critical functions performed by systems’ in the years prior to the AC’srelease. It also stated that due to difficulties in assessing hazards for such systems,more structured approaches were being used for such assessments, which thereforerequired more detailed guidance.Some key features <strong>of</strong> the AC included the following:• It provided the same guidance as the European ACJ on the concept <strong>of</strong> an inverserelationship between the severity <strong>of</strong> the effects <strong>of</strong> a failure condition and theprobability <strong>of</strong> its occurrence, and this concept was illustrated with the diagramshown in Figure 33. However, the AC used the term ‘major’ to refer to both the‘hazardous’ and ‘major’ effect levels described in the ACJ, and it occasionallyused the term ‘severe major’ to refer to more serious conditions within thismajor level.• It used the term ‘fail-safe design’, which meant that no single failure shouldresult in a catastrophic failure condition. Although the European ACJ current atthe time did not include this term, the FAA and the European Aviation SafetyAgency (EASA) 94 advised that it was a commonly held principle in both theFAA and the European certifying authorities at the time. 9592939495For example, a value <strong>of</strong> 10 -3 per <strong>flight</strong> hour equated to once every 1,000 <strong>flight</strong> hours, and a value<strong>of</strong> 10 -7 per <strong>flight</strong> hour equated to once per 10,000,000 <strong>flight</strong> hours.The range for ‘probable’ was also split into two, with ‘frequent’ described as more than 10 -3 per<strong>flight</strong> hour and ‘reasonably probable’ described as 10 -3 to 10 -5 per <strong>flight</strong> hour.EASA took over the role <strong>of</strong> aircraft certification in Europe in 2003.The fail-safe design principle was explicitly stated in later versions <strong>of</strong> the European ACJ.- 86 -

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