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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,

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

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They provided information for maintenance personnel on the status orfunctioning <strong>of</strong> the aircraft’s systems. A class 1 message was usually associatedwith one or more cockpit effect messages that were presented to the <strong>flight</strong> crewduring the <strong>flight</strong>. A class 2 message was not associated with any messagesprovided to the <strong>flight</strong> crew. 54The PFR had a number <strong>of</strong> limitations, including:• it only recorded information to the nearest minute• it only showed the first occurrence <strong>of</strong> a cockpit effect or a maintenance faultmessage (that is, a repeat occurrence <strong>of</strong> the same message would not be shown)• a correlation function performed by the CMS grouped together all <strong>of</strong> themaintenance fault messages associated with the same system 55 at the same time(within 1 minute), and it would only record the first fault that was detected(along with a list <strong>of</strong> other systems that detected the fault).The PFR from the <strong>flight</strong> recorded 22 cockpit effect messages that were presented tothe crew during the period from 0440 until the end <strong>of</strong> the <strong>flight</strong>. 56 These included 21different ECAM messages and a ‘flag’ message. 57 All were caution messagesexcept the AUTO FLT AP OFF warning message.Appendix C provides the complete PFR from the <strong>flight</strong>.ADIRU fault messagesThe two types <strong>of</strong> caution messages that could be displayed to the <strong>flight</strong> crew aboutan ADIRU problem were a NAV IR [1, 2 or 3] FAULT and a NAV ADR [1, 2 or 3]FAULT. These messages could be generated by the ADIRU self-detecting a faultand transmitting that information to the FWS, by the FWS detecting that the IR orADR parts had stopped transmitting data (that is, the data was not ‘refreshed’), orby another ADIRU detecting a problem (for the ADR only) and transmitting thatinformation to the FWS.The PFR for the <strong>flight</strong> showed two caution messages associated with the operation<strong>of</strong> the ADIRUs:• NAV IR1 FAULT (at 0440). Given that ADIRU 1 consistently flagged the IRparameters as invalid, it is likely that it self-detected the problem.• NAV ADR 1 FAULT (at 0513). Subsequent analysis determined that thismessage was generated by the IR part <strong>of</strong> ADIRU 3 (section 1.12.6) and not byADIRU 1 itself.54555657A class 2 maintenance message was associated with one or more ‘maintenance status’ messages,which were placed in the ‘cockpit effects’ column <strong>of</strong> the PFR even though they were not presentedto the <strong>flight</strong> crew. Class 3 messages were not recorded on the PFR but could be obtained from theCMS or the relevant system’s BITE.Fault messages were grouped by the Air Transport Association (ATA) chapter reference, witheach chapter referring to a different system. This categorisation is widely used in aircraftdocumentation.The ‘cockpit effects’ column <strong>of</strong> the PFR also included six ‘maintenance status’ messages. Thesewere class 2 maintenance fault messages and were not presented to the crew during <strong>flight</strong>.A ‘flag’ was displayed on the <strong>flight</strong> crew’s <strong>flight</strong> displays. When a flag was displayed there wasno associated ECAM message.- 46 -

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