Original words, traceable pages

Search the evidence

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.

4 matching PDF pages. Showing 4 short source excerpts. Open the document for full context.

G-ONEE: electrical failures and unreliable airspeed

Printed page label not indexed. PDF page 4.

descent below seven” and shortly after declared a MAYDAY. The aircraft broke cloud at 6,000 ft and remained in clear air for the remainder of the flight. The main landing runway in use at Schiphol was 36R but ATC offered
Open official document at PDF page 4AAIB final report: G-ONEE

G-ONEE: electrical failures and unreliable airspeed

Printed page label not indexed. PDF page 6.

another crew who had recently departed from Schiphol where there was no cloud below 6,000 ft agl. This minimised the likelihood of flying an approach in icing conditions. The crew stated they discussed having sufficient fuel to fly to another
Open official document at PDF page 6AAIB final report: G-ONEE

G-ONEE: electrical failures and unreliable airspeed

Printed page 183. PDF page 185.

min 23 even though the aeroplane was already climbing rapidly with a vertical speed of 6,000 ft/min. These factors induced a rapid reduction in the kinetic energy and brought the aeroplane above its lift ceiling, at the Mach level at
Open official document at PDF page 185Final Report: Accident on 1st June 2009 to the Airbus A330-203 registered F-GZCP operated by Air France flight AF 447

G-ONEE: electrical failures and unreliable airspeed

Printed page label not indexed. PDF page 38.

increase in cabin altitude Normal operating range for the cabin altitude is between 6,000 and 8,000 ft. When it exceeds 8,500 ft the primary EICAS changes to display the current cabin altitude in amber. There are no other alerts until
Open official document at PDF page 38AAIB final report: G-ONEE