航空 发表于 2011-4-21 12:16:44

A320飞行操纵非正常操作A

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航空 发表于 2011-4-21 12:16:53

FLIGHT CONTROLS MENU Abnormal operation (A) 1/39<BR>FLIGHT CONTROLS MENU<BR>Abnormal operation (A) 2/39<BR>Let’s first see the redundancy aspects of the flight<BR>controls.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 3/39<BR>In case of a computer failure, the second computer of the<BR>same type takes over (ELAC, SEC and FAC cases).<BR>Note that SEC 3 is only used for spoiler control and does<BR>not participate (as SEC 1 and 2) in the flight control system<BR>reconfiguration.<BR>FAC 1<BR>FAC 2<BR>ELAC 1<BR>ELAC 2<BR>SEC 1<BR>SEC 2<BR>SEC 3<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 4/39<BR>Each primary flight control surface is supplied by 2<BR>(ailerons, elevators and stabilizer) or 3 (rudder) different<BR>hydraulic sources.<BR>Each control surface has an independent actuator for each<BR>hydraulic source.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 5/39<BR>Each actuator is controlled by a different computer.<BR>One actuator for each surface is always in active mode.<BR>The other stays in damping mode and is monitored by its<BR>associated computer.<BR>ELAC 1 ELAC 2<BR>AAccttiivveemmooddee<BR>DDaammppiinnggmmooddee<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 6/39<BR>We will demonstrate these points in the following ELAC 1<BR>failure.<BR>Assume, you are the PNF. You are in flight and everything<BR>is normal.<BR>AAccttiivveemmooddee<BR>DDaammppiinnggmmooddee<BR>Clliicckk oonn tthhee ffoorrwaarrdd aarrrroow ttoo aaccttiivvaattee tthhee ffaaiilluurree..<BR>ELAC 1 ELAC 2<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 7/39<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 8/39<BR>You hear the single chime and see<BR>the Master Caution light.<BR>No, to extinguish the Master Caution<BR>light, push the Master Caution pb sw.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 9/39<BR>You hear the single chime and see<BR>the Master Caution light.<BR>No, to extinguish the Master Caution<BR>light, push the Master Caution pb sw.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 10/39<BR>FLIGHT CONTROLS MENU<BR>Abnormal operation (A) 11/39<BR>Onn tthhee E//WD,, rreeaadd tthhee ttiittllee ooff tthhee ffaaiilluurree..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 12/39<BR>Observe ELAC indications on the ECAM F/CTL<BR>page.<BR>The “1” and the box of ELAC 1 are in amber.<BR>The “2” of ELAC<BR>2 remains in green<BR>indicating that<BR>ELAC 2 has taken<BR>over automatically.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 13/39<BR>Indications for aileron and<BR>elevator actuators, controlled<BR>by ELAC 1, are partially boxed<BR>in amber.<BR>This means that these<BR>actuators have automatically<BR>switched to damping mode.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 14/39<BR>Actuators controlled by ELAC<BR>2 have automatically switched<BR>from damping to active mode to<BR>control the ailerons and<BR>elevators.<BR>They are not boxed on the<BR>ECAM F/CTL page.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 15/39<BR>ELAC 1 FAULT light is illuminated on the FLT<BR>CTL panel.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 16/39<BR>We can see that the first action is to reset the<BR>faulty computer.<BR>The PF will ask you to perform the ECAM<BR>actions.<BR>PeerrffoorrmECAMaaccttiioonn..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 17/39<BR>Noo,, sswiittcchh ELLAC 11 OFFFF..<BR>We can see that the first action is to reset the<BR>faulty computer.<BR>The PF will ask you to perform the ECAM<BR>actions.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 18/39<BR>Noo,, sswiittcchh ELLAC 11 OFFFF..<BR>We can see that the first action is to reset the<BR>faulty computer.<BR>The PF will ask you to perform the ECAM<BR>actions.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 19/39<BR>ELLAC 11 iiss nnoow OFFFF..<BR>Coonnttiinnuuee ECAMaaccttiioonn..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 20/39<BR>ELLAC 11 iiss nnoow OFFFF..<BR>Noo,, sswiittcchh ELLAC 11 ON..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 21/39<BR>ELLAC 11 iiss nnoow OFFFF..<BR>Noo,, sswiittcchh ELLAC 11 ON..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 22/39<BR>ELAC 1 has not been successfully reset.<BR>The procedure requires you to switch ELAC 1<BR>OFF.<BR>Coonnttiinnuuee ECAMaaccttiioonn..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 23/39<BR>ELAC 1 has not been successfully reset.<BR>The procedure requires you to switch ELAC 1<BR>OFF.<BR>Noo,, sswiittcchh ELLAC 11 OFFFF..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 24/39<BR>ELAC 1 has not been successfully reset.<BR>The procedure requires you to switch ELAC 1<BR>OFF.<BR>Noo,, sswiittcchh ELLAC 11 OFFFF..<BR>FLIGHT CONTROLS MENU<BR>Abnormal operation (A) 25/39<BR>Afftteerr rreevviieew aanndd ccoonnffiirrmaattiioonn ffrroomtthhee PFF......<BR>Clleeaarr FF//CTTLL..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 26/39<BR>Afftteerr rreevviieew aanndd ccoonnffiirrmaattiioonn ffrroomtthhee PFF......<BR>Noo,, pprreessss eeiitthheerr CLLR kkeeyy..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 27/39<BR>Afftteerr rreevviieew aanndd ccoonnffiirrmaattiioonn ffrroomtthhee PFF......<BR>Noo,, pprreessss eeiitthheerr CLLR kkeeyy..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 28/39<BR>The STATUS page is displayed for review.<BR>A green message advises us that we have a<BR>degradation in approach capability.<BR>Note that there are loss of neither control<BR>surfaces nor maneuvering ability.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 29/39<BR>You can see, in the INOP SYS column, that<BR>ELAC 1 and CAT 3 DUAL are now inoperative.<BR>After review and confirmation from the PF...<BR>Clleeaarr STTATTUS..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 30/39<BR>You can see, in the INOP SYS column, that<BR>ELAC 1 and CAT 3 DUAL are now inoperative.<BR>After review and confirmation from the PF...<BR>Noo,, pprreessss tthhee STTS kkeeyy oorr eeiitthheerr CLLR kkeeyy..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 31/39<BR>You can see, in the INOP SYS column, that<BR>ELAC 1 and CAT 3 DUAL are now inoperative.<BR>After review and confirmation from the PF...<BR>Noo,, pprreessss tthhee STTS kkeeyy oorr eeiitthheerr CLLR kkeeyy..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 32/39<BR>ECAMaaccttiioonnss ccoompplleetteedd..<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 33/39<BR>We will now review the other redundancy<BR>features and protections we did not have the<BR>opportunity to see when performing the previous<BR>procedure.<BR>FLIGHT CONTROLS MENU<BR>Abnormal operation (A) 34/39<BR>ELAC 1<BR>ELAC 2 SEC 2<BR>In case of complete failure of ELAC computers, SEC 2<BR>computer takes over the control of the elevators and the THS.<BR>The roll function is still available via the spoilers. The<BR>ailerons are in damping mode.<BR>FLIGHT CONTROLS MENU<BR>Abnormal operation (A) 35/39<BR>SEC 2<BR>ELAC 1<BR>ELAC 2<BR>SEC 1<BR>In the very low probability of SEC 2 failure, it will be<BR>replaced by SEC 1.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 36/39<BR>Another case of failure is an elevator fault.<BR>In this case, the deflection of the remaining one is limited<BR>to avoid excessive asymmetrical loads on the tail or rear<BR>fuselage and to reduce the asymmetry effects .<BR>The remaining surface is sufficient to resume normal<BR>flight.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 37/39<BR>In case of total loss of normal control or hydraulic supply,<BR>the elevators are automatically set to and maintained in the<BR>neutral position.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 38/39<BR>Provided the appropriate<BR>Hydraulic systems are available:<BR>- Mechanical control of the THS<BR>is always available via the pitch<BR>trim wheels.<BR>- For the rudder, mechanical<BR>control via the rudder pedals is<BR>always available even in case of<BR>complete failure of FAC computers.<BR>This is called the mechanical<BR>backup.<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 39/39<BR>SUMMARY:<BR>• General rules:<BR>If a computer fails, the second computer of the same type takes over.<BR>Each primary flight control surface is supplied by at least 2 different hydraulic sources. An<BR>independent actuator is associated with each hydraulic source for each surface.<BR>Each actuator is controlled by a different computer. For a surface, one actuator is always in active<BR>mode while the other(s) are in damping mode.<BR>• Ailerons/Elevators/THS/Rudder:<BR>If both ELAC fail, SEC 2 controls the elevators and the THS. The ailerons are in damping mode. If<BR>SEC 2 fails, it will be replaced by SEC 1.<BR>In case of one elevator failure, the deflection of the remaining one is limited to avoid excessive<BR>loads on the tail and rear fuselage.<BR>Mechanical backup is always available using the rudder pedals and pitch trim wheels, provided the<BR>appropriate hydraulic systems are available.<BR>NEXT<BR>MMoodduullee ccoommpplleetteedd<BR>FLIGHT CONTROLS MENU Abnormal operation (A) 40/39<BR>LLIISSTTOOFFSSUUBBJJEECCTTSS<BR>EXIT<BR>AUDIO GLOSSARY FCOM<BR>RETURN<BR>EELLAACC11FFAAUULLTT<BR>CCOOMMPPUUTTEERRFFAAIILLUURREESS

bocome 发表于 2011-7-31 08:56:08

非正常操作

tissle 发表于 2014-4-17 11:30:53

好资料,学习了。。。

twn353091 发表于 2014-5-9 19:22:28

感謝分享, tks.

gordon525 发表于 2014-8-3 07:53:26

谢谢辛苦了 收藏一下

wsinglejoke 发表于 2016-1-23 11:30:24

666666666666666666666666666

diguo 发表于 2017-3-9 12:54:09

恩。好东西。好好学习一下。
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