飛機(jī)航線常見故障解析-資料下載頁(yè)
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【正文】 辦法防止反推手柄的運(yùn)動(dòng)(如用保險(xiǎn)絲將反推手柄固定在前推手柄上等)。 700/800： 1．解除相應(yīng)反推的工作并固定好(AMM 780000/901)。 注：反推鎖在關(guān)位時(shí)，若已證實(shí)同步鎖在鎖定位則一個(gè)或兩個(gè)同步鎖皆可失效。 (a) For Engine 1, open this circuit breaker and install safety lock:CAPT Electrical System Panel, P182Row Col Number NameB 7 C01266 ENGINE 1 THRUST REVERSER SYNC LOCK(b) For Engine 2, open this circuit breaker and install safety lock:F/O Electrical System Panel, P62Row Col Number NameC 5 C01267 ENGINE 2 THRUST REVERSER SYNC LOCK.1) For Engine 1, open this circuit breaker and install safety lock:CAPT Electrical System Panel, P182Row Col Number NameB 5 C00276 ENGINE 1 THRUST REVERSER CONT2) For Engine 2, open this circuit breaker and install safety lock:F/O Electrical System Panel, P62Row Col Number NameC 7 C00277 ENGINE 2 THRUST REVERSER CONT2．用適當(dāng)?shù)霓k法防止反推手柄的運(yùn)動(dòng)(如用保險(xiǎn)絲將反推手柄固定在前推手柄上等)。 飛 行(O) 注：參考AMM 解除反推工作，當(dāng)重新按壓主警戒燈時(shí)，會(huì)導(dǎo)致主警戒燈和發(fā)動(dòng)機(jī)指示燈(ENG)點(diǎn)亮。 反推失效： 1．應(yīng)該發(fā)展非對(duì)稱反推的飛機(jī)操縱技術(shù)并用于訓(xùn)練。 2．對(duì)700/800，濕跑道/越障限重以及與減重有關(guān)的V1 值必須減少以滿足反推失效時(shí)的需要。參考飛行計(jì)劃和性能手冊(cè)，起飛及著陸章節(jié)中有關(guān)性能減載的內(nèi)容。：OIL FILTER CLOGGING WARNING SYSTEM DESCRIPTION AND OPERATION1 . Oil Differential Pressure Switch(Ref. Fig. 001) The oil differential pressure switch is located above the scavenge filter.Lines are routed to the switch from bosses on the scavenge filter. Actuation of the differential pressure switch is at: psid ( bar) plus or minus 1 psid ( bar) increasing pressure22 psid ( bar) decreasing pressure.2 . Oil Filter Clogging Indication(Ref. Fig. 002, 003)An oil differential pressure switch (also named clogging indicatortransmitter) is installed on the lubrication unit. The pressure switchsignal is used by the ECAM system to generate the main oil filter clogindication when the oil differential pressure across this filter isprised between 29 psig (2 bar) and 33 psig ( bar).In result: the MASTER CAUT light (amber) es on ENG page on the lower display unit of the ECAM appears with OIL FILTERCLOG indication (White and Amber) instructions appear on the upper display unit the audio warning (single chime) sounds.3 . Enginemounted visual indication system, associated with the master magnetic chip detector (MCD)(Ref. Fig. 004, 005, 006)A. GeneralThe oil (scavenge) system is equipped with a fan inlet caseinstalledvisual indication system which serves to directly see and check if theoil system is contamined by magnetic particles/chips, or not.A popout type visual indicator, installed just above the oil tank,permits this visual check, each time the nacelle access door to the oiltank is opened during normal line maintenance (oil tank servicing forexample)(Ref. Fig. 004)B. Description(Ref. Fig. 004, 007, 008, 009)From front to rear, the visual indication system consists of the itemswhich follow: the handremovable probe of the master magnetic chip detector (MCD) a twowire, shielded electrical cable (DPM cable) a popout type visual indicator_________________________________________________AMM7 9 3 5 0 0 Page 1 20090713僅供培訓(xùn)使用，維護(hù)以各航空公司手冊(cè)為準(zhǔn) 第 29 頁(yè) 共 29 頁(yè) 2009年7月
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