R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 019)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 020)
**ON A/C ALL
This symbol (which consists of 2 triangles facing each other and linked by a thin line whose the middle is indicated by a small point) has 3 degrees of freedom:
-lateral displacements (parallel to the horizon line),
-longitudinal displacements (parallel to the pitch scale),
-rotation around its middle.
It follows the lateral and longitudinal displacements of the FPV and
gives the pitch and roll orders respectively through its longitudinal
and rotation movements with respect to the Flight Path Vector symbol.
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In case of failure of the guidance signals a red FD Flag is displayed (when FD pushbutton switch is pressed). R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 021)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 022)
**ON A/C ALL
item (a).
If the track angle or flight path angle signal or both are wrong, the
red FPV signal is displayed (when the TRK-FPA pushbutton switch mode
is selected).
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 021)
**ON A/C ALL
item (b).
1EFF : ALL 1 31-64-00Page 43 1 1 Aug 01/05 1 1 1CES 1
PFD - FD and FPV Failure Display
Figure 021
R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page 44 1 1 Aug 01/05 1 1 1CES 1
PFD - FD and FPV Failure Display
Figure 022
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page 45 1201-299, 301-302, 1May 01/05 1 1 1CES 1
(13) Yaw Bar
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 023)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 024)
**ON A/C ALL
This symbol provides the pilot with flight director yaw orders.
When in RWY mode, during take off, this symbol remains presented
until the A/C reaches the altitude of 30 ft.
When in ROLL OUT mode this symbol appears, when in descent the A/C
reaches 30 ft. just before landing.
R **ON A/C 106-149, 303-399, 401-499,
(14) Tailstrike indication (Ref. Fig. 025) The tailstrike indication is an amber "V", it is submitted to the roll angle, it is positioned on the pitch scale according to the following principle: the tailstrike angle is reached when the lower tip of the "V" contacts to the aircraft reference.
**ON A/C ALL
ITEM LIST
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 023)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 024)
1EFF : ALL 1 31-64-00Page 46 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL
------------------------------------------------------------------------------ITEM PARAMETER EQUIPMENT LABEL COLOUR ------------------------------------------------------------------------------1 YAW FD FMGC 143 Green 2 RADIO ALTITUDE RADIO ALTI 164 Green
or amber 3 ROLL ANGLE ADIRU IRS 325 YELLOW 4 PITCH ANGLE ADIRU IRS 324 YELLOW
(15) Excessive Attitude Presentation
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 023)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 024)
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 026)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 027)
**ON A/C ALL
In case of excessive attitude:
-pitch angle more than +25 degrees or less than -13 degrees or
-absolute value of roll angle more than 45 degrees The display of several zones is cleared from the PFD for better legibility: FMA, guidance symbols (FD or FPD). The affected information is back on display when the pitch angle and roll angle become "normal" again:
-pitch angle less than 22 degrees or more than -10 degrees
-absolute value of roll angle less than 40 degrees.
1EFF : ALL 1 31-64-00Page 47 1 1 Aug 01/05 1 1 1CES 1
PFD - Yaw, FD, Radio Alt, Roll and Pitch Angle Parameters
Figure 023 (SHEET 1)
R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page 48 1 1 Aug 01/05 1 1 1CES 1
PFD - Yaw, FD, Radio Alt, Roll and Pitch Angle Parameters
Figure 023 (SHEET 2)
R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page 49 1 1 Aug 01/05 1 1 1CES 1 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM 指示/記錄系統 8(13)
