(2)
After some seconds, on the ISIS Indicator, the INIT page comes into view.
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5. Close-up
________ Subtask 34-20-00-860-051
A. Put the aircraft back to its initial configuration.
(1) Do the ADIRS Stop procedure (Ref. TASK 34-10-00-860-005)
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________________________________________________________________
1. General
_______
R **ON A/C 001-049, 051-099, 101-105,
One standby airspeed indicator, one standby altimeter and one metric altimeter are directly connected to the standby pitot and static sources. Each indicator is contained in a 2 ATI case (ARINC 408) and installed on the center instrument panel. The standby circuit can be drained by means of a water drain.
**ON A/C 151-199, 201-212, 214-220,
One standby airspeed indicator and one standby altimeter are directly connected to the standby pitot and static sources. Each indicator is contained in a 2 ATI case (ARINC 408) and installed on the center instrument panel. The standby circuit can be drained by means of a water drain.
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-212, 214-220,
2. Component Location
__________________
R **ON A/C 001-049, 051-099, 101-105,
(Ref. Fig. 001)
**ON A/C 151-199, 201-212, 214-220,
(Ref. Fig. 001A)
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-212, 214-220,
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF.
-------------------------------------------------------------------------------3FN ALTM-STANDBY 4VU 211 831 34-21-22 9FN IND-STANDBY AIRSPEED 4VU 211 831 34-21-26
15FN ALTIMETER-METRIC 4VU 211 831 34-21-25
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Standby Data - Altitude and Airspeed - Component Location
Figure 001
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Standby Data - Altitude and Airspeed - Component Location
Figure 001A
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3. System Description__________________
R **ON A/C 001-049, 051-099, 101-105,
(Ref. Fig. 002)
**ON A/C 151-199, 201-212, 214-220,
(Ref. Fig. 002A)
R **ON A/C 001-049, 051-099, 101-105,
(Ref. Fig. 003)
**ON A/C 151-199, 201-212, 214-220,
(Ref. Fig. 003A)
R **ON A/C 001-049, 051-099, 101-105,
(Ref. Fig. 004)
**ON A/C 151-199, 201-212, 214-220,
(Ref. Fig. 004A)
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-212, 214-220,
A. Standby Altimeter The standby altimeter is supplied with static pressure by the standby air data system to indicate the barometric altitude of the aircraft in feet. The barometric altitude is displayed by means of: - a pointer (4) performing one revolution of the dial for 1000 feet - a display counter (5) made up of two drums displaying respectively the tens of thousands and the thousands of feet. When the altitude is below 10,000 feet, the figure zero of the left drum is replaced by black and white stripes. The figure nine is replaced by an orange fire stripped zone. the altitude dial (6) is calibrated from 0 to 1000 feet with 20 feet graduations
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Standby Data - Altitude and Airspeed - Pneumatic Circuit
Figure 002
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Standby Data - Altitude and Airspeed - Pneumatic Circuit
Figure 002A
R 1EFF : 151-199, 201-212, 214-220, 1 34-21-00Page 6 1 1 Nov 01/04 1 1 1CES 1 中國航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM NAVIGATION 導(dǎo)航2(97)
