(6) Heading marks
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 008)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 009)
**ON A/C ALL
Provided that the pitch angle, roll angle and magnetic heading information is valid, magnetic heading graduations are constantly displayed just under the horizon line every 10 degrees of heading. For high attitude values, when the horizon line disappears behind the upper sector or the lower one, the magnetic heading graduations remain in view. They are displayed below the sector line.
1EFF : ALL 1 31-64-00Page 25 1 1 Aug 01/05 1 1 1CES 1
(7) Attitude failure presentation
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 012)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 013)
**ON A/C ALL
In case of detected failure of the ADIRU (IRS) concerning the pitch and/or roll angle information, the whole attitude and guidance display is replaced by the ATT red flag (flashing for 9 s then steady). This ATT red flag disappears when the PFD is supplied again with healthy pitch and roll data, from another source or from the same source.
(8) Lateral acceleration A yellow trapezoidal index below the roll angle will represent the A/C lateral acceleration on the ground. It will be driven by the side slip information above 30 ft radio-altitude if this information is available.
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 014)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 015)
**ON A/C ALL
item (a).
If not, the index gives again an indication of A/C lateral
acceleration.
1EFF : ALL 1 31-64-00Page 26 1 1 Aug 01/05 1 1 1CES 1
PFD - Attitude Failure Display
Figure 012
R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page 27 1 1 Aug 01/05 1 1 1CES 1
PFD - Attitude Failure Display
Figure 013
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page 28 1201-299, 301-302, 1May 01/05 1 1 1CES 1
PFD - Slip Indication
Figure 014
R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page 29 1 1 Aug 01/05 1 1 1CES 1
PFD - Slip Indication
Figure 015
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page 30 1201-299, 301-302, 1May 01/05 1 1 1CES 1 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
In case of engine failure, at take off or go around the index changes to cyan color and becomes thicker.
R **ON A/C 106-149, 303-399, 401-499,
In case of engine failure, at take off or go around the index changes to cyan color.
**ON A/C ALL
It will then be animated by the difference:
(estimated side slip) minus (target side slip),
so that it will be centered if the pilot gives the proper rudder
control necessary to compensate for the engine failure.
In case of failure a SI red flag is presented at the symbol location R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 014)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 015)
**ON A/C ALL
item (b).
NOTE : As a safety precaution the SI flag like other red flags is
____ visible on the PFD, even in minimum brightness condition.
NOTE : A SI red flag is presented at the symbol location if any
____
reverse is deployed in flight.
1EFF : ALL 1 31-64-00Page 31 1 1 Aug 01/05 1 1 1CES 1
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(9) Guidance With the standard FD bars, either of these two modes of presentation of the Flight Director orders is available depending on the HDG V/S -TRK FPA choice (Ref. Fig. 016) item (a) :
-conventional crossed bars, pitch and roll (plus yaw bar for take off and land align and roll phases).
-Flight Path Director symbols in relation with the Flight Path
Vector, they give the orders in flight path and in track. The guidance orders are presented on a given PFD provided that the FD pushbutton switch light on the respective EFIS control section of the FCU is on, the on condition corresponds to the FD ON selection (Ref. Fig. 016) item (b). Moreover, at least one FD must be engaged. Provided that there is a value displayed in the FCU HDG/TRK counter and the FD is off, a cyan vertical bar on the horizon line indicates the selected heading or track.
R **ON A/C 106-149, 303-399, 401-499,
(9) Guidance With the standard FD bars, either of these two modes of presentation of the Flight Director orders is available depending on the HDG V/S -TRK FPA choice (Ref. Fig. 016) item (a) :
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