Search report text, read a short matching passage, then open the source page.
Exact phrases match first; otherwise all words must occur close together. Six excerpts maximum. Text extraction cannot search image-only charts. Warsaw uses a report transcription with missing figures and appendices.
5 matching PDF pages. Showing 5 short source excerpts. Open the document for full context.
Printed page 2. PDF page 22.
were fluctuating. No such fluctuations were occurring on the first officer's PFD or the standby flight instruments. The fluctuations on the captain's PFD appeared to be based on unreliable information, as there was no other indication that the aircraft wasOpen official document at PDF page 22ATSB AO-2008-070: In-flight upset, VH-QPA, 7 October 2008
Printed page 5. PDF page 25.
He then flew the aircraft without the autopilot or autothrust engaged, and using the standby instruments, for the remainder of the flight. The first officer returned to the flight deck at 0447:40, taking over from the second officer in theOpen official document at PDF page 25ATSB AO-2008-070: In-flight upset, VH-QPA, 7 October 2008
Printed page 21. PDF page 41.
information such as attitude, airspeed and altitude was also provided on the integrated standby instrument system (ISIS), mounted in the centre of the instrument panel (see to the left of the ECAM in Figure 10). Most of the information displayedOpen official document at PDF page 41ATSB AO-2008-070: In-flight upset, VH-QPA, 7 October 2008
Printed page 22. PDF page 24.
flight display (PFD), then a few moments later in the speed displayed on the integrated standby instrument system (ISIS). The flight control law reconfigured from normal to alternate. The Flight Directors (FD) were not disconnected by the crew, but theOpen official document at PDF page 24Final Report: Accident on 1st June 2009 to the Airbus A330-203 registered F-GZCP operated by Air France flight AF 447
Printed page 35. PDF page 37.
PHC's manages the Captain probes, another the First Officer probes and the third the standby probes (there is no TAT standby sensor). There are two function modes, ground and flight. On the ground, neither of the TAT sensors is heatedOpen official document at PDF page 37Final Report: Accident on 1st June 2009 to the Airbus A330-203 registered F-GZCP operated by Air France flight AF 447