I can understand why this would be priority for Airbus even without the incident of a flight losing altitude - recently read that a major philosophical difference between Airbus and Boeing is that Airbus prioritises the safety of the Aircraft through controls (hardware and software) where as Boeing believes a human should always be the final decision maker and be able to over ride any control. An Airbus rarely allows…
Didn’t workout with the Boeing 737 Max, did it?
Airbus A320 Fly by wire corrupted by radiation in flight
51–60 of 74 posts
Re: Airbus A320 Fly by wire corrupted by radiation in flight
#52Earlier quoted context omitted.
Where did you see that it didn't have ECC?
"As noted in section 3.5.2, the CPU module on units 4167 and 4122 did not incorporate EDAC, nor was it required by the aircraft manufacturer’s specification" It was apparently added in a later HW revision "The LTN-101 ADIRU’s CPU module was later redesigned to reduce costs and to include error detection and correction (EDAC). EDAC is used for detecting and correcting single-bit errors in RAM chips to give protection…
Re: Airbus A320 Fly by wire corrupted by radiation in flight
#53Earlier quoted context omitted.
"As noted in section 3.5.2, the CPU module on units 4167 and 4122 did not incorporate EDAC, nor was it required by the aircraft manufacturer’s specification" It was apparently added in a later HW revision "The LTN-101 ADIRU’s CPU module was later redesigned to reduce costs and to include error detection and correction (EDAC). EDAC is used for detecting and correcting single-bit errors in RAM chips to give protection…
Thanks; hmm but that means the version with EDAC has been in use since 2002, so is less likely related to todays update? (hth did they design stuff without protection back upto that point?)
"There was a limitation in the algorithm used by the A330/A340 flight control primary computers for processing angle of attack (AOA) data. This limitation meant that, in a very specific situation, multiple AOA spikes from only one of the three air data inertial reference units could result in a nose-down elevator command. [Significant safety issue]"
It's the only one marked "Significant safety issue" so my money is on that.
Re: Airbus A320 Fly by wire corrupted by radiation in flight
#54Earlier quoted context omitted.
Didn’t workout with the Boeing 737 Max, did it?
That was basically the first Boeing that went in the Airbus direction.
Airbus is much more transparent about its automation. Pilots even learn about the procedure to fly an A320 with a complete fly-by-wire outage using only mechanical emergency elevator controls and differential thrust.
Re: Airbus A320 Fly by wire corrupted by radiation in flight
#55Re: Airbus A320 Fly by wire corrupted by radiation in flight
#56Re: Airbus A320 Fly by wire corrupted by radiation in flight
#57Re: Airbus A320 Fly by wire corrupted by radiation in flight
#58https://en.wikipedia.org/wiki/Single-event_upset Apparently it has happened to an Airbus once before.
Re: Airbus A320 Fly by wire corrupted by radiation in flight
#59Re: Airbus A320 Fly by wire corrupted by radiation in flight
#60Earlier quoted context omitted.
"As noted in section 3.5.2, the CPU module on units 4167 and 4122 did not incorporate EDAC, nor was it required by the aircraft manufacturer’s specification" It was apparently added in a later HW revision "The LTN-101 ADIRU’s CPU module was later redesigned to reduce costs and to include error detection and correction (EDAC). EDAC is used for detecting and correcting single-bit errors in RAM chips to give protection…
Thanks; hmm but that means the version with EDAC has been in use since 2002, so is less likely related to todays update? (hth did they design stuff without protection back upto that point?)
The ELACs (controlling the elevator and aileron actuators according to the demands computed by other functions) are made by Thales specifically for this aircraft type and probably have a quite different design.