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Looking at the diagram of the instrument layout in
this glider, it would appear that the total energy tube was connected to the fuselage statics and then in turn to all the pressure instruments. I would guess that effect of the total energy tube on the ASI would therefore be greatly reduced due to leakage through the normal static holes. Derek Copeland At 10:06 18 October 2006, Phil Collin wrote: For the full report see the following URL http://www.aaib.dft.gov.uk/publicati...ptember_2006/g laser_dirks_dg600_glider__bga_3445__tail_number_ 656_.cfm Bert Willing wrote: Doug, the reading of an ASI is very rarely connected to winch launch accidents, and certainly not in the initial climb. Sliding back in the seat (or movement of a seatpan) during initial rotation has already claimed a number of lives. Bert 'Doug Haluza' wrote in message oups.com... Derek Copeland wrote: Wouldn't the exact effect depend on the relative areas of the pot pitot and the usually very small holes in the T.E. probe? The AAIB are normally very thorough in their investigations, so I am happy to believe them, and that this error was not the primary cause of the accident. Neither am I recommending that you should connect your instruments up in this way. No, the area of the openings would not matter, unless there was a significant leak. If your description is correct, then I would not assume that the primary cause was the straps, which as you point out could not be conclusively determined due to post impact damage. Can you check the report again and make sure you have correctly reported the results? -- Phil Collin Partner Manager T: 0870 861 0 300 E: W: www.voicehost.co.uk |
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