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研究生: 姚雋偉
Yao, Chun-Wei
論文名稱: 尾風超限進場之風險分析
The Risk Analysis of Exceeding Tailwind-Limitation Approach
指導教授: 袁曉峰
Yuan, Hsiao-Feng
學位類別: 碩士
Master
系所名稱: 工學院 - 航空太空工程學系
Department of Aeronautics & Astronautics
論文出版年: 2006
畢業學年度: 94
語文別: 中文
論文頁數: 55
中文關鍵詞: 平飄時間過短落地點過長尾風通過跑道參考點時過高
外文關鍵詞: Tailwind, Short flare, Height high at threshold, Long touchdown
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  •   本研究使用國內某航空公司飛航操作品質保證系統所記錄之偏離標準飛行事件資料進行尾風超限進場之因素及風險分析,分析結果顯示造成尾風超限進場之因素可分為「塔台及組員」及「機場及跑道」這兩項,而機場盛行風之緣故導致在台北松山機場(6,7,8月)以及高雄小港機場(9,10,11月)發生尾風超限進場機率偏高。

      風險分析結果顯示航機於尾風超限進場時由於對地速度提升及操作難度增加,對落地點及減速滾行距離將產生直接影響,使得減速滾行距離較正常操作時增加11%~13%。而且尾風超限進場將可能導致其他偏離標準操作事件之發生,在尾風時進場可能發生「通過跑道參考點時過高」、「落地點過長」及「平飄時間過短」等偏離標準操作事件,而尾風對飛航組員造成的影響除了操控較為困難外,飛航組員可能為了避免某些較嚴重之偏離標準操作事件而使其決策能力受到干擾。

      初步分析結果顯示尾風確實影響飛行組員之操作精確度,建議飛行組員降落過程中遭遇尾風變化過大以及跑道狀況不良,飛行組員應考慮採取重飛動作以增進飛航安全。此外在尾風超限進場發生機率偏高之季節更需要提高警覺。

     This thesis research accessed the non-standard flight event data from the Flight Operation Quality Assurance (FOQA) system of a local airline to analyze the risk of the events of exceeding tailwind-limitation approach. 1,433 flights of a total 10,411 flights were recorded and analyzed with different degrees of exceeding tailwind limitations.

     The analysis showed that the major factors to incur the events of exceeding tailwind-limitation approach were ATC and flight crew’s decision making. And, the prevailing wind of the airports resulted a higher probability to have the exceeding events especially at Taipei Songshan Airport and Kaohsiung International Airport.

     The FOQA data indicated that airplane’s ground speed was higher and the difficulty of maneuvering the aircraft increased under tailwind. The touchdown distances were usually longer and an average increase of 11% to 13% of deceleration distances were shown. Accompanying the exceeding tailwind-limitation approach, the probabilities of having other non-standard flight events such as “height high at threshold”, “long touchdown”, and “short flare” also increased. In the approach process, the decision making of the pilots may be influenced under tailwind situation in order to avoid triggering the high-severity event of bounce landing.

     In this preliminary study, the data showed that the tailwind does have effects on the accuracy of aircraft maneuvering. It is suggested that flight crews should consider go-around under the situations of strong tailwind coupling with wet runway.

    中文摘要  Ⅰ 英文摘要  Ⅱ 致謝  Ⅲ 目錄  Ⅳ 表目錄  Ⅵ 圖目錄  Ⅶ 第一章 導論  1  1-1   前言  1  1-2   失事因素分析  2  1-3   研究動機  4 第二章 飛行操作品質保證系統  6  2-1   FOQA之基本概念  6  2-2   FOQA之法源依據  8   2-2.1  美國FOQA發展  8   2-2.2  英國FOQA發展  9   2-2.3  中國FOQA發展  10   2-2.4  台灣FOQA發展  11   2-2.5  小結  12  2-3   FOQA之實際應用  12   2-3.1  法國航空  12   2-3.2  英國航空  15 第三章 研究方法與工作流程  18  3-1   研究目的  18  3-2   研究方法  18  3-3   事項編號說明  20 第四章 研究結果與討論  22  4-1   尾風超限進場因素分析  22   4-1.1  航管與組員  22   4-1.2  機場與跑道  23   4-1.3  其他  24  4-2   尾風超限進場風險分析  25   4-2.1  滾行距離與跑道狀況  25   4-2.2  尾風與其他事項之關連  28  4-3   結論與建議  30 第五章 未來工作  33 參考文獻  34 表  36 圖  43 附錄  49 自述  55 表目錄 表一、載客用航空器發展  36 表二、西元2005年B型機機隊高度偏離事件排行  36 表三、西元2005年B型機機隊中度偏離事件排行  37 表四、事項1033於各機場及全年發生機率  37 表五:台北松山機場盛行風向季節性日變化分佈表  38 表六、高雄小港機場盛行風向季節性日變化分佈表  39 表七、A型機於台北松山機場降落後參數比較(乾跑道)  40 表八、B型機於高雄小港機場降落後參數比較  40 表九、B型機於台北松山機場降落後參數比較(乾、濕滑跑道)  40 表十、人工煞車實際煞車距離  41 表十一、自動煞車實際煞車距離  41 表十二、尾風其他事項之關連  42 表十三:不同機隊於台北松山機場之尾風與其他事項之關連  42 表十四:不同機隊於高雄小港機場之尾風與其他事項之關連  42 圖目錄 圖一、世界空中運輸成長預測  43 圖二、飛行器失事比例  43 圖三、失事主要原因比例  44 圖四、各飛行階段發生失事比例  44 圖五、尾風超限進場嚴重程度比例(A型機)  45 圖六、尾風超限進場嚴重程度分析(B型機)  45 圖七、風速與高度變化圖  46 圖七:台北松山機場事項1033季節分佈(A型機)  46 圖八:高雄小港機場事項1033季節分佈(A型機)  47 圖九:台北松山機場事項1033季節分佈(B型機)  47 圖十:高雄小港機場事項1033季節分佈(B型機)  48 圖十一、速度與有效煞車摩擦係數關係  48

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