A320飞机维护手册 AMM 指示/记录系统 7(18)

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 -Flight phase related mode
R  (Ref. Fig. 036) 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. Pressing 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
____ by pressing 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.
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-60-00Page 69 1201-299, 301-302, 1Config-1 May 01/05 1 1 1CES 1

 Automatic Mode Related to the Flight Phase R Figure 036
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-60-00Page 70 1201-299, 301-302, 1Config-1 May 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 This mode has priority over all the others but can be superseded if a system page is called manually.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:
 -CRUISE page indications:
R  (Ref. Fig. 037) 1 - Engine oil quantity 2 - Engine fuel used 3 - Engine vibrations N1 N2 4 - Landing elevation indication 5 - Cabin vertical speed 6 - Cabin altitude 7 - Gross weight indication 8 - Time indication 9 - G. load or ALT Sel indication 10- TAT/SAT indications 11- Cargo compartment temperature 12- Cabin compartment temperature
 -Permanent data indications
 1 - TAT/SAT indications
 2 - time indication
 3 - G LOAD indication
 4 - gross weight indication

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-60-00Page 71 1201-299, 301-302, 1Config-1 May 01/05 1 1 1CES 1

 CRUISE Page R Figure 037
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-60-00Page 72 1201-299, 301-302, 1Config-1 May 01/05 1 1 1CES 1

R

R
R
-
AIR COND page indications (Ref. Fig. 038) 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

 -
AIR COND page indications (Ref. Fig. 039) 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

 -CAB PRESS page indications (Ref. Fig. 040) 1 - Cabin differential pressure (analog + digital) 2 - Landing elevation (suppressed in manual mode) 3 - Landing elevation manual selection (AUTO is replaced by MAN) 4 - Cabin vertical speed (analog + digital) 5 - Cabin altitude (analog + digital) 6 - Manual system selected (nothing in auto mode) 7 - Safety valve indication 8 - Safety valve position 9 - System in control (nothing displayed if system not active) 10- Pack 2 flow control valve 11- Outflow valve position 12- Avionics vent extract indication 13- Air extract valve position 14- Avionics vent system indication 15- Air inlet valve position 16- Pack 1 flow control valve 17- Avionics vent blower indication
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-60-00Page 73 1201-299, 301-302, 1Config-1 May 01/05 1 1 1CES 1

 AIR COND Page R Figure 038
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-60-00Page 74 1201-299, 301-302, 1Config-1 May 01/05 1 1 1CES 1

 AIR COND Page R Figure 039
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-60-00Page 75 1201-299, 301-302, 1Config-1 May 01/05 1 1 1CES 1
　
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