The table below gives the conditions of display of the FMA flags:
-------------------------------------------------------------------------------| FLAGS | DISPLAY | |--------------------|--------------------------------------------------------| | MAN PITCH TRIM ONLY| - Red flag in zone BC3 of FMA when pitch trim is only | | | by mechanical back up, before flight phase 4 or | | | after flight phase 5, flashing during 9s then | | | steady | |--------------------|--------------------------------------------------------| | USE MAN PITCH TRIM | - Amber message in zone BC3 of FMA when pitch trim is | | | only by direct law, pulsing during 9s then steady. |
G. ILS Guidance and Vertical Deviation When the pilot presses the LS pushbutton switch located on his EFIS control section, the Glide Slope and Localizer scales come into view on his PFD (as well as the ILS CRS symbol on the HDG scale).
(1) LS Approach
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 085)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 086)
**ON A/C ALL
In addition to the scales and the ILS CRS symbol, the LS identification (if available) frequency and the DME distance, in case of co-located DME, or the distance to threshold, in case of GLS approach (if available), are displayed on the PFD left bottom corner.
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 086)
1EFF : ALL 1 31-64-00Page A98 1 1 Aug 01/05 1 1 1CES 1
PFD - ILS Approach Display
Figure 085
R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page A99 1 1 Aug 01/05 1 1 1CES 1
PFD - ILS Approach Display
Figure 086
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page B0 1201-299, 301-302, 1May 01/05 1 1 1CES 1R **ON A/C 106-149, 303-399, 401-499,
item (A).
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
item (a).
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299,
If the LOC or G/S signals are in the F/W condition, the ILSX red flag
is displayed (ILS1 on CAPT PFD and ILS2 on F/O PFD)
(Ref. Fig. 086)
item (b).
(a)
Not Applicable
(b)
Not Applicable
(c)
Not Applicable
R **ON A/C 106-149, 301-399, 401-499,
** MLS or GLS option is not installed on MMR **
If the LOC or G/S signals are not valid, the ILS red flag is
displayed provided the L/S pushbutton switch is pressed on FCU.
It flashes during 9s then is steady.
** MLS or GLS option is installed on MMR **
(a) In case of an ILS approach: If the LOC or G/S signals are not valid or if the function ILS is selected but not active, a ILS red flag is displayed provided the LS pushbutton switch is pressed on EFIS control panel.It flashes 9s then is steady. If there is a discrepancy in the selected approach mode, a LS red flag is displayed provided LS pushbutton switch is pressed on EFIS control panel. It flashes 9s then is steady. The LS flag has priority on the ILS one.
1EFF : ALL 1 31-64-00Page B1 1 1 Aug 01/05 1 1 1CES 1
(b)
In case of an MLS approach: If the LOC or G/S signals are not valid or if the function MLS is selected but not active, a MLS red flag is displayed provided the LS pushbutton switch is pressed on EFIS control panel.It flashes 9s then is steady. If there is a discrepancy in the selected approach mode, a LS red flag is displayed provided LS pushbutton switch is pressed on EFIS control panel. It flashes 9s then is steady. The LS flag has priority on the MLS one.
(c)
In case of an GLS approach: If the LOC or G/S signals are not valid or if the function GLS is selected but not active, a GLS red flag is displayed provided the LS pushbutton switch is pressed on EFIS control panel.It flashes 9s then is steady. If there is a discrepancy in the selected approach mode, a LS red flag is displayed provided LS pushbutton switch is pressed on EFIS control panel. It flashes 9s then is steady. The LS flag has priority on the GLS one.
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 085)
R **ON A/C 106-149, 301-399, 401-499,
item (B).
R 1EFF : 106-149, 301-399, 401-499, 1 31-64-00Page B2 1 1 Aug 01/05 1 1 1CES 1R **ON A/C 106-149, 303-399, 401-499,
(2) Markers At the intersection of the G/S and LOC scales, the marker indication appears when the A/C overflies the corresponding beacon. These indications are respectively:
-OM for Outer Marker (cyan color)
(Ref. Fig. 087)
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