Airbus A319-131, G-EUPO, 17 December 2010
Airbus A319-131, G-EUPO
Summary:
On approach to London Heathrow Airport, in IMC and icing conditions, there was a loss of communication between the Probe Heat Computers (PHC) and the Centralised Fault Display System (CFDS). 皇冠体育app associated Electronic Centralized Aircraft Monitoring (ECAM) actions required the crew to select ADR3 as the data source for the commander鈥檚 instruments.
Later on final approach to Runway 27L the aircraft suffered a loss of displayed airspeed information on both the commander鈥檚 and the standby flight instruments. 皇冠体育app crew carried out a go-around using the 鈥楿nreliable Speed Indication鈥� procedure from the Quick Reference Handbook (QRH).
皇冠体育app investigation concluded that the loss of displayed airspeed information resulted from a combination of:
- a loss of communication between the Probe Heat Computers (PHC) and the Centralised Fault Display System (CFDS),
- icing of the standby pitot probe resulting in the loss of indicated airspeed displayed on the commander鈥檚 and standby instruments.
One Safety Recommendation was made.
Download report:
(1,867.72 kb)