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<SDOBI lang="en"><B000><eptags><B001EP>......DE....FRGB..IT......SE........................................................................</B001EP><B003EP>*</B003EP><B005EP>J</B005EP><B007EP>DIM360 Ver 2.15 (14 Jul 2008) -  2999001/0</B007EP></eptags></B000><B100><B110>1960262</B110><B120><B121>CORRECTED EUROPEAN PATENT SPECIFICATION</B121></B120><B130>B8</B130><B132EP>B1</B132EP><B140><date>20091223</date></B140><B150><B151>W1</B151><B153>73</B153><B155><B1551>de</B1551><B1552>Bibliographie</B1552><B1551>en</B1551><B1552>Bibliography</B1552><B1551>fr</B1551><B1552>Bibliographie</B1552></B155></B150><B190>EP</B190></B100><B200><B210>06829535.1</B210><B220><date>20061212</date></B220><B240><B241><date>20080415</date></B241></B240><B250>en</B250><B251EP>en</B251EP><B260>en</B260></B200><B300><B310>102005059370</B310><B320><date>20051213</date></B320><B330><ctry>DE</ctry></B330></B300><B400><B405><date>20091223</date><bnum>200952</bnum></B405><B430><date>20080827</date><bnum>200835</bnum></B430><B450><date>20091104</date><bnum>200945</bnum></B450><B452EP><date>20090804</date></B452EP><B480><date>20091223</date><bnum>200952</bnum></B480></B400><B500><B510EP><classification-ipcr sequence="1"><text>B64C   9/32        20060101AFI20070814BHEP        </text></classification-ipcr><classification-ipcr sequence="2"><text>B64C  23/06        20060101ALI20070814BHEP        </text></classification-ipcr></B510EP><B540><B541>de</B541><B542>SEITENRUDER FÜR EIN VERKEHRSFLUGZEUG</B542><B541>en</B541><B542>RUDDER OF A COMMERCIAL AIRCRAFT</B542><B541>fr</B541><B542>GOUVERNE DE DIRECTION D'UN AERONEF COMMERCIAL</B542></B540><B560><B561><text>EP-A- 1 527 992</text></B561><B561><text>EP-A1- 1 149 761</text></B561><B561><text>GB-A- 722 842</text></B561><B561><text>US-A- 2 643 833</text></B561><B561><text>US-A- 4 290 612</text></B561><B562><text>KIRIL DIMITROV SAKALIYSKI: "Aeroacoustics of Perforated Drag Plates for Quiet Transport Aircraft" THESIS (S.M.), DEPT. OF AERONAUTICS AND ASTRONAUTICS, MASSACHUSETTS INSTITUTE OF TECHNOLOGY, [Online] 19 August 2005 (2005-08-19), XP009081776 Retrieved from the Internet: URL:http://hdl.handle.net/1721.1/33212&gt; [retrieved on 2007-04-03]</text></B562><B562><text>DATABASE WPI Week 200012 Derwent Publications Ltd., London, GB; AN 2000-137368 XP002429977 &amp; WO 00/02775 A2 (CENT AEROHYDRODYNAMIC INST) 20 January 2000 (2000-01-20)</text></B562></B560></B500><B700><B720><B721><snm>BENDER, Klaus</snm><adr><str>Ottenser Hauptstr. 14</str><city>22765 Hamburg</city><ctry>DE</ctry></adr></B721></B720><B730><B731><snm>Airbus Operations GmbH</snm><iid>10205140</iid><irf>A 10064 / KK</irf><adr><str>Kreetslag 10</str><city>21129 Hamburg</city><ctry>DE</ctry></adr></B731></B730><B740><B741><snm>Maiwald Patentanwalts GmbH</snm><iid>00118401</iid><adr><str>Elisenhof 
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