(Ref. Fig. 033)
**ON A/C ALL
(19) Side Stick Controller Order On the ground with one engine running, a white cross indicates the resulting side stick controller order from the Captain and the First Officer: up and rightfor an order controlling on A/C nose up and right movement. Four white corners show the limits of this cross in pitch (plus or minus 15.) and in roll (plus or minus 19.).
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 034)
**ON A/C ALL
(20) Attitude Protection Indication Two small green dashes on each side of the cut-sphere show that the roll protections are available (plus or minus 65.). Other green dashes on the pitch scale (on each side of the +30. and -15. graduations) show that the pitch protections are available: +30., -15.. If not (for pitch or roll, independently), the dashes are replaced by amber crosses.
1EFF : ALL 1 31-64-00Page 65 1 1 Aug 01/05 1 1 1CES 1
PFD - Radio Altitude Indication
Figure 033 (SHEET 1)
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page 66 1201-299, 301-302, 1May 01/05 1 1 1CES 1
PFD - Radio Altitude Indication
Figure 033 (SHEET 2)
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page 67 1201-299, 301-302, 1May 01/05 1 1 1CES 1
Side Stick Controller Order
Figure 034
R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page 68 1 1 Aug 01/05 1 1 1CES 1
R **ON A/C 106-149, 303-399, 401-499,
(21) System messages (feedback monitoring) (Ref. Fig. 035) A safety function is implemented in the EIS to monitor the critical parameters displayed on the PFD,such as PITCH, ROLL. When a discrepancy occurs between an incoming parameter (at the DMC input) and the same parameter ready to be drawn on the relevant DU (inside the DU), then a feedback message is generated on the DUs which monitor the faulty DU.
(a)
Some of the feedback messages are displayed above the attitude zone: CHECK PFD CAPT (amber) CHECK PFD FO (amber) CHECK EWD (amber) DISPLAY SYSTEM VERSION INCONSISTENCY (amber) DU NOT MONITORED (amber)
(b)
Some of the feedback messages are displayed above the heading scale: CHECK ND CAPT (amber) CHECK ND FO (amber) CHECK SD (amber)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(22) The table below gives the conditions of display of the attitude information:
-------------------------------------------------------------------------------| PARAMETERS | DISPLAY | |--------------------|--------------------------------------------------------| | A/C symbol | - Valid attitude. | | | - Yellow (normal brightness) : take-off or heading/V/S | | | mode. | | | - Yellow (dimmed) : TRK-FPA mode. | |--------------------|--------------------------------------------------------| | Scale | - Valid attitude. | |--------------------|--------------------------------------------------------| | Lateral | - Yellow if attitude information is valid. | | acceleration | - On the ground : presents valid acceleration. | | | - In flight : presents estimated side slip, if valid, | | | otherwise, presents lateral acceleration. | |--------------------|--------------------------------------------------------|
1EFF : ALL 1 31-64-00Page 69 1 1 Aug 01/05 1 1 1CES 1
PFD-System Messages Figure 035
R 1EFF : 1 1 1CES 106-149, 303-399, 401-499, 1 111 31-64-00 Page 70 Aug 01/05
-------------------------------------------------------------------------------
| PARAMETERS | DISPLAY | |--------------------|--------------------------------------------------------| | Rising runway | - Valid attitude. | | | - Valid radio altitude. | | | - Radio altitude above 50ft. | |--------------------|--------------------------------------------------------| | FD bars | - Valid and not excessive attitude. | | | - Heading / V/S mode. | | | - FD engaged (green light on). | | | - Roll FD and pitch FD from FMGC valid. | |--------------------|--------------------------------------------------------| | Flight path vector | - Valid atttude. | | | - Valid drift angle and flight path angle. | | | - TRK-FPA mode selected on FCU. | |--------------------|--------------------------------------------------------| | Flight path | - Valid and not excessive attitude. | | director | - FD1 or FD2 engaged. | | | - Roll FD and pitch FD from FMGC valid. | |--------------------|--------------------------------------------------------| | Heading marks | - Valid attitude. | | | - Valid magnetic heading. | |--------------------|--------------------------------------------------------| | Selected HDG/track | - FD off. | | | - Valid attitude and magnetic heading. | | | - Selected track in TRK/FPA mode, selected heading in | | | HDG/V/S mode. | |--------------------|--------------------------------------------------------| | Radio altitude | - Green, size 3mm : radio altitude between 400 and | | | 2500ft. | | | - Green, size 4mm : under 400ft., above DH+100ft. | | | - Amber, size 4mm : either RA under DH+100ft., either | | | invalid DH and RA under 400ft. | | | - Not excessive attitude condition. | |--------------------|--------------------------------------------------------| | Decision height | - DH amber flashing when radio altitude goes under | | (DH) | decision then steady. | |--------------------|--------------------------------------------------------| | Yaw bar | - On the ground, at least one engine running. | | | - Roll and pitch command position valid. | |--------------------|--------------------------------------------------------| | Protection marks | - Only if valid attitude. | | | - Green dashes when roll protection in normal law. | |--------------------|--------------------------------------------------------| | Target side slip | - Cyan trapezo]dal index below the roll angle in case | | | of engine failure, presenting the difference between | | | estimated side slip and target side slip. |
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM 指示/记录系统 8(15)
