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时间:2011-03-25 12:29来源:蓝天飞行翻译 作者:admin
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 Figure 072

R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page A64 1 1 Aug 01/05 1 1 1CES 1


 PFD - TCAS Indications - Preventive Resolution Advisories
 Figure 073

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page A65 1201-299, 301-302, 1May 01/05 1 1 1CES 1


 PFD - TCAS Indications - Corrective Resolution Advisories
 Figure 074

R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page A66 1 1 Aug 01/05 1 1 1CES 1


 PFD - TCAS Indications - Corrective Resolution Advisories
 Figure 075

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page A67 1201-299, 301-302, 1May 01/05 1 1 1CES 1 **ON A/C ALL


 The pilot's task is to maneuver the aircraft promptly to keep the needle out of the red sector and place it in the adjacent green "Fly-to" sector. The vertical speed indication is red-colored when the vertical speed is within the forbidden sector whereas it becomes green when the vertical speed enters the authorized sector. The preventive resolution advisories advise the pilot to avoid vertical speeds that could lead to a hazardous situation.

R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 072)
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
 (Ref. Fig. 073)
 **ON A/C ALL
 They are represented by one or two red zones on the scale.The pilot must keep the aircraft vertical speed outside these zones. If the aircraft can neither climb nor descend, then two red sectors appear on the vertical speed scale and a range sector (+/- 250 ft ) around the zero figure is left uncolored. This uncolored area around the zero figure informs the pilot to maintain the aircraft at its current level.
R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 076)
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
 (Ref. Fig. 077)
 1EFF : ALL 1 31-64-00Page A68 1 1 Aug 01/05 1 1 1CES 1


 PFD - TCAS Indications
 Figure 076

R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page A69 1 1 Aug 01/05 1 1 1CES 1


 PFD - TCAS Indications
 Figure 077

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page A70 1201-299, 301-302, 1May 01/05 1 1 1CES 1 **ON A/C ALL


 In case of system or TCAS computer failure, the NAV TCAS FAULT message generated by the FWC appears in the warning section of the upper ECAM DU.

R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 078)
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
 (Ref. Fig. 079)
 **ON A/C ALL
 If this message is generated further to a failure of the TCAS computer, an amber TCAS flag also appears next to the vertical speed scale.

R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 069)
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
 (Ref. Fig. 080)
 **ON A/C ALL
 NOTE : When the resolution advisories are no longer displayed, the
____ shape and color of the vertical speed scale return to initial configuration. On a detection of a ventilation failure (DUs no longer cooled), the grey background colored areas of PFD image might be removed, except for the V/S scale when TCAS information is displayed on it.
 1EFF : ALL 1 31-64-00Page A71 1 1 Aug 01/05 1 1 1CES 1


 PFD - TCAS Failure Message
 Figure 078

R 1EFF : 106-149, 303-399, 401-499, 1 31-64-00Page A72 1 1 Aug 01/05 1 1 1CES 1


 PFD - TCAS Failure Message
 Figure 079

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page A73 1201-299, 301-302, 1May 01/05 1 1 1CES 1


 PFD - TCAS Flag Indication
 Figure 080

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 31-64-00Page A74 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,


 NOTE : When the resolution advisories are no longer displayed, the
____ shape and color of the vertical speed scale return to initial configuration. On a detection of a ventilation failure (DUs no longer cooled), the grey background colored areas of PFD image might be removed, except for the V/S scale when TCAS information is displayed on it.

R **ON A/C 106-149, 303-399, 401-499,
 NOTE : When the resolution advisories are no longer displayed, the
____ shape and color of the vertical speed scale return to initial configuration.
 **ON A/C ALL
 F. Flight Mode Annunciator

R **ON A/C 106-149, 303-399, 401-499,
 (Ref. Fig. 081)
 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
 (Ref. Fig. 082)
 **ON A/C ALL
 (1) Description of the Different Zones The FMA zones are divided into zones which are referenced with their line number (1, 2, 3) and their column letter (A, B, C, D, E). The columns are separated by vertical bars (the second one may cover 2 or 3 FMA lines depending on the annunciations and messages to be written).
 
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