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时间:2011-03-25 12:26来源:蓝天飞行翻译 作者:admin
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 1EFF : 106-149, 303-399, 1 31-60-00Page 61 1 1 Config-3 Aug 01/05 1 1 1CES 1


 Automatic Advisory Mode
 Figure 032

 1EFF : 106-149, 303-399, 1 31-60-00Page 62 1 1 Config-3 Aug 01/05 1 1 1CES 1


 -Manual mode (or flight crew mode) In this mode, the crew selects manually the desired system page by means of the ECAM control panel related key, which comes on. This mode enables the crew to select any system page except the cruise page. In case of total loss of the ECAM CP, the ALL key enables the crew to have successively on display all the system pages and to stop on the desired system page. The pilot can obtain this sequencing of the system pages by successive pushes on the ALL key, or if he presses it continuously. In the latter case, all the system pages appear successively at approximately 1 s time intervals, up to the last one (CRUISE). The pilot must release the key to re-initialize the stack pointing device and to have the first system page (ENG). This ALL key feature is particularly useful in case of ECAM DU failure, and generally speaking whenever there is only one DU left for ECAM display (Mono mode).
 -Flight phase related mode (Ref. Fig. 033) This mode engages only when the other modes are not engaged. In this mode, a given page is automatically shown, according to the current flight phase.
 NOTE : The A/C system page corresponding key on the ECAM control
____ panel comes on only in the Advisory mode and in the manual mode. To press the key in this case removes the current A/C system page from the lower ECAM DU, and the flight phase related A/C system page replaces it.
 NOTE : The flight crew can at any time select an A/C system page
____ if he presses the corresponding key, which then comes on. If the flight crew presses the on key, the A/C system page currently on display is replaced:
 -either by the one corresponding to the present warning, possibly and if the warning presentation sequence had not been cleared
 - or by the flight-phase related A/C system image.
 1EFF : 106-149, 303-399, 1 31-60-00Page 63 1 1 Config-3 Aug 01/05 1 1 1CES 1


 Automatic Mode Related to the Flight Phase
 Figure 033

 1EFF : 106-149, 303-399, 1 31-60-00Page 64 1 1 Config-3 Aug 01/05 1 1 1CES 1


 -Priority between the different modes Mode 1 : Automatic mode related to a failure. This mode has priority over all the others but can be superseded if a system page is called manually. It is disengaged if the warning message is cleared by means of the CLR key or if the failure conditions have disappeared. Mode 2 : Automatic advisory mode This mode has priority over modes 3 and 4. It is disengaged if the corresponding system key is pressed or if another system is called manually. A system page displayed in advisory mode and disengaged cannot be called again in advisory mode for the same parameter. However, if the parameter is still in the advisory range, it continues pulsing on the relevant page when this page is for instance called manually. Disengagement is automatic when a warning occurs or when the parameter is back to normal. Mode 3 : Manual mode This mode can be engaged at any time but is disengaged if mode 1 or 2 is engaged. Mode 4 : Automatic mode related to the flight phase This mode is automatically engaged if the other modes are not engaged.
 (4) System pages and associated list of parameters which are (or may be) displayed:
 -Permanent data indications
 1 - TAT/SAT indications
 2 - time indication
 3 - G LOAD indication
 4 - gross weight indication

 -AIR COND page indications (Ref. Fig. 034) 1 - Pack control mode (ALTN mode, Pack reg.) 2 - Compartment temperature (Cockpit, Fwd cabin, Aft cabin) 3 - Duct temperature (Cockpit, Fwd cabin, Aft cabin) 4 - Hot air valve position 5 - Hot air regulating valve position (Cockpit, Fwd cabin, Aft cabin) 6 - Recirculation air fan
 1EFF : 106-149, 303-399, 1 31-60-00Page 65 1 1 Config-3 Aug 01/05 1 1 1CES 1


 AIR COND Page Figure 034
 1EFF : 1 1 1CES  106-149, 303-399,  1 111 Page 6631-60-00 Config-3 Aug 01/05

 

 -AIR COND page indications (Ref. Fig. 035) 1 - Aft cargo temperature 2 - Aft cargo isolation valve 3 - Aft cargo duct temperature 4 - Aft cargo isolation valve 5 - Hot air valve position 6 - Aft cargo isolation valve position
 -ELEC page indications (Ref. Fig. 036) 1 - Bat bus 2 - Bat contactor 3 - Bat operation (voltage, current, off) 4 - DC Ess bus 5 - DC bus 6 - Ess transformer rectifier contactor 7 - Transformer rectifier operation (voltage, current, off) 8 - Emergency gen operation (voltage, current) 9 - AC bus 10- Emergency gen line contactor 11- Gen operation (load, voltage, frequency, off) 12- IDG operation (normal, LO PR, disc) 13- IDG outlet temperature 14- Ext power operation (voltage, frequency, standby) 15- APU operation (load, voltage, frequency, off) 16- Main galley shed 17- AC Ess bus 18- AC/Ess TR contactor 19- Ess transformer rectifier operation (voltage, current)
 
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