INTENTIONALLY BLANK
1 1
31-64-00Page 2
1 1 Feb 01/98 1 1 1CES 1
PFD - Component Location
Figure 001
R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page 3/4 1 1 Aug 01/05 1 1 1CES
1
PFD - Component Location
Figure 002
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page 5/6 1201-299, 301-302, 1May 01/05 1 1 1CES 3. System Description
__________________
The PFD image is divided in 9 zones
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 003)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 004)
**ON A/C ALL
The PFD image presents the main information necessary for the control of the A/C, arranged in the basic T configuration.
A grey background is permanently present on the screen.
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
If the SDAC detects AVIONICS VENT EXTRACT FAULT and AVIONICS VENT BLOWER FAULT conditions it sends a discrete signal to the DMCs which command the PFDs to suppress the grey background. This limits tube consumption and thus prevents them overheating. Tube operation is certified for 30 minutes without ventilation.
1EFF : ALL 1 31-64-00Page 7 1 1 Aug 01/05 1 1 1CES 1
PFD - Zones Figure 003
R 1EFF : 1 1 1CES 106-149, 303-399, 401-499, 1 111 31-64-00 Page 8 Aug 01/05
PFD - Zones Figure 004
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1201-299, 301-302, 1 1CES 1 111 31-64-00 Page 9 May 01/05
**ON A/C ALL
A. Attitude Data R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 005)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 006)
**ON A/C ALL
The aircraft attitude (pitch and roll) is indicated in the center part of the image by a cut-sphere shaped window which features a conventional ADI.
(1) Aircraft symbol R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 005)
**ON A/C ALL
The fixed symbol is in yellow color, it comprises 3 parts: two simplified wing/landing gear parts plus a center part.
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
It provides the pilot with a quick glance attitude information, both in pitch and roll with respect to the attitude sphere. When the pilot selects the TRK FPA mode on the FCU instead of the HDG V/S mode, the A/C symbol is dimmed (except at take off).
1EFF : ALL 1 31-64-00Page 10 1 1 Aug 01/05 1 1 1CES 1
PFD - Aircraft Attitude Display
Figure 005
R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page 11 1 1 Aug 01/05 1 1 1CES 1
PFD - Aircraft Attitude Display
Figure 006
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page 12 1201-299, 301-302, 1May 01/05 1 1 1CES 1R **ON A/C 106-149, 303-399, 401-499,
It provides the pilot with a quick glance attitude information, both in pitch and roll with respect to the attitude sphere.
**ON A/C ALL
(2) Pitch angle information
R **ON A/C 106-149, 303-399, 401-499,
(Ref. Fig. 005)
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
(Ref. Fig. 006)
**ON A/C ALL
The A/C present pitch angle is given by the vertical displacements of the pitch attitude scale with respect to the center of the A/C symbol. The scale moves behind the cut-sphere shaped window, limited by the lines of an upper and a lower sector. The scale rotates around the center of the A/C symbol in accordance with the A/C present roll angle.
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
The pitch scale comprises white reference lines and associated pitch angle values. The lines are given every 2.5 degrees from 0 to 10 degrees, then for the 15 degrees, 20 degrees, 30 degrees, 50 degrees and 80 degrees values. Beyond 30 degrees, red large arrow heads (V-shaped) indicate an excessive attitude and the direction to follow in order to reduce it. (Ref. Fig. 007)
1EFF : ALL 1 31-64-00Page 13 1 1 Aug 01/05 1 1 1CES 1
PFD - Pitch Scale
Figure 007
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page 14 1201-299, 301-302, 1May 01/05 1 1 1CES 1R **ON A/C 106-149, 303-399, 401-499, 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(9)
