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Printed page 5. PDF page 19.
for increased thrust from the autothrottle and manual movement of the thrust levers to fully forward. The airspeed reduced as the autopilot attempted to maintain the ILS glide slope. When the airspeed reached 115 kt the ‘airspeed low' warning wasOpen official document at PDF page 19Aircraft Accident Report 1/2010: Boeing 777-236ER, G-YMMM, London Heathrow Airport, 17 January 2008
Printed page 43. PDF page 57.
Air Accident Report: 1/2010 G-YMMM EW/C2008/01/01 fully forward, the flight crew briefly retarded the thrust levers, to a position corresponding to a thrust level above that which was being delivered, before placing them fully forwardOpen official document at PDF page 57Aircraft Accident Report 1/2010: Boeing 777-236ER, G-YMMM, London Heathrow Airport, 17 January 2008
Printed page 81. PDF page 95.
ATP and were assessed as being in good condition. The forward cross‑feed valve did not fully achieve the requirements for the two thermal relief valves identified as First and Second port. However, it was assessed that the slightly early operationOpen official document at PDF page 95Aircraft Accident Report 1/2010: Boeing 777-236ER, G-YMMM, London Heathrow Airport, 17 January 2008