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|    AVIATION    |    Aviation echo, airline-related news    |    717 messages    |
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|    Message 426 of 717    |
|    Ward Dossche to Vincent Coen    |
|    Re: AF447 ... the public prosecuter appe    |
|    03 May 23 13:28:39    |
      MSGID: 2:292/854 131f0436       REPLY: 2:250/1@fidonet 644bfbe3       TZUTC: 0200       Vince,               VC> My opinion, but only based on the raw info, is that, yes the crew screwed       VC> up - bad pitot tubes / non heating etc allowed. Poor training, rating       VC> renewals both for a/c type and not.               VC> Flying a light twin, such as a Cessna C340P I have access to such       VC> secondary instrumentation when using even sat navigation, let alone the       VC> other tools at my disposal.               VC> A qualified UK, USA and others, license holder.               You remind me of my friend Luc, former Fido-sysop, who had an ULM. Flew some       200 hours on it and on several occasions tried to overrule professional pilots       with 10.000+ hours.               When commenting on a case like this, you need to read up on it and familiarise       yourself with the details. For starters, the full incident-report by the BEA       (the French authority which examines aitcraft accidents) and the cockpit-voice       recorder transcript are available online. Simply google for it, you have not       done that.               You make it appear that the 3 cockpit crew were novices with hardly experience.               The captain had 10,988 commercial flying hours, of which 6,258 were as       captain, including 1,700 hours on the Airbus A330.               The co-pilot had 2,936 commercial flight hours, of which 807 hours were on the       Airbus A330.               The relief co-pilot had 6,547 commercial flying hours, of which 4,479 were on       the Airbus A330.               In other words, pretty experienced people.               You need to go back to the moment of the incident … 2009 ... 14 years.               Pitot-tube heating was "on". Simple. What was the trouble was ice crystals       forming on the pitot-tubes caused by high-altitude freezing rain altering the       airflow enough to cause false speed readings and indicating an 'overspeed'       condition. To correct that overspeed the nose was lifted a bit, although there       was no overspeed. The plane climbed as a result in the beginning but the       overspeed stayed, which made the co-pilot, who was in command, lift the nose       even higher (the captain at that moment was in the crew rest compartment) and       reduce power. As a result the aircraft turned into an aerodynamic stall at       high altitude and the stick-shaker started rattling.               Here you have two different instruments giving contrary information: one       saying you are going too fast, the other saying you are going too slow and       about to lose lift. What do you do? In the middle of the night? No visual       reference... The cockpit crew (co-pilot right seat [pilot in command], relief       co-pilot left seat [pilot monitoring]) decided to lift the nose even higher to       reduce speed. This worsened the stall condition. The nose 16 degrees up while       the engines had been reduced to "flight idle". The flight parameters at that       point were so bad that the Flight Management System disconnected and the       screens went blank. No more readings were processed and the stick-shaker also       disconnected. They figured the stall was solved while in fact it went from bad       to horrific.               Here you have a wide-bodied airliner in an aerodynamic stall, falling out of       the sky, in the pitchdark of the night with no visual reference and not a       single instrument indicating anything.               The relief co-pilot called "my plane", confirmed by the co-pilot "your       plane"... Pushed the nose down, revved-up the engines and increased the       airflow over the wing surfaces. This started to provide correct information       again to the flight management system which moved through the zone where the       stick-shaker is active, which activated the stick shaker again and suddenly       the pitot tubes started providing false information again.               So here you have a situation where by pushing the nose down and increasing       speed, you are getting a warning that you are stalling. It didn't make sense,       plus they got again an overspeed warning. Important to understand, under those       conditions the auto-pilot disconnected and they were flying by hand ... with       faulty instrumentation ... and no visual reference.               To overcome the new overspeed condition, the co-pilot again pulled his stick,       while the relief co-pilot was pushing his stick not understanding what was       happening as he thought he was in control...               They had alerted the captain who exited from the crew rest and saw the       instrumentation. He did not demand his left-hand seat but strapped in the 3rd       seat. He went through manuals, tried to coach the people in the left hand and       right hand seats. He quickly figured out that the co-pilot never released the       control stick and actually was flying instead of the relief co-pilot.               They had been stalling now for minutes and losing a lot of altitude. By the       time the condition was discovered, they were too low to lower the nose and       speed-up the engines to recover from the stall. The co-pilot realised it       suddenly and is heard saying on the CVR in French "But, but ... we are going       to crash then?" seconds before impact. At no point during the descent had they       been aware.               The relief pitot-tubes for this particular aircraft were in Paris and were       going to installed after the plane arrived.               Discussion erupted later about could this accident have happened with a       Boeing? The answer is a painful "no" because the control columns in Boeing       aircraft are interconnected and the relief co-pilot would have noticed       immediately the co-pilot was still pulling and intervened. The joysticks of       Airbus aircraft operate independently so they can be used differently with the       left seat having priority, but when the left seat is not handling the joystick       and the right seat is pulling in a cramp ... the nose goes up ... and       remember, your artificial horizon is gone because of the lack of       instrumentation.              --- DB4 - 20230201        * Origin: AVIATION ECHO HQ (2:292/854)       SEEN-BY: 1/123 15/0 80/1 90/1 105/81 106/201 123/131 129/305 153/7715       SEEN-BY: 221/1 226/30 227/114 229/110 112 113 307 317 400 426 428       SEEN-BY: 229/470 664 700 280/464 282/1038 292/854 8125 301/1 317/3       SEEN-BY: 320/219 322/757 335/364 342/200 396/45 460/58 633/280 712/848       PATH: 292/854 229/426           |
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