Component Location - Cockpit
Figure 006
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Indication - Lower Ecam Display Unit
Figure 007
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B. Temperature Indication A Temperature Sensor is installed at the precooler outlet to get the temperature. It has two platinum resistance wires. Each wire transmits a signal to the BMCs. The BMCs monitor the temperature of the system. The BMCs prepare the data for the Built In Test Equipment (BITE). Additionally the BMCs send ARINC data to the SDACs for preparation of ECAM display information. The lower ECAM display unit shows the temperature on the BLEED page in green. If the temperature is too high, it is shown in amber.
LEAK DETECTION - DESCRIPTION AND OPERATION
__________________________________________
_______
1. General
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 001)
**ON A/C 301-399,
(Ref. Fig. 001A)
**ON A/C ALL
This continuous monitoring system is designed to detect, by means of detection loops, any ambient overheat. This is to protect the structures and components near the hot air ducts in the fuselage, pylons and wings, against possible leaks or bursts.
2. Component Location
__________________
(Ref. Fig. 002)
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 003)
**ON A/C 301-399,
(Ref. Fig. 003A)
**ON A/C ALL
A. Wing Section R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 003)
Leak Detection Loops - General Schematic
Figure 001
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 36-22-00Page 2 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R Leak Detection Loops - General Schematic R Figure 001A
R 1EFF : 301-399, 1 36-22-00Page 3/4 1 1 May 01/04 1 1 1CES
Sensing Element Typical
Figure 002
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INTENTIONALLY BLANK
1 1
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Component Location
Figure 003
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 36-22-00Page 7/8 1201-299, 401-499, 1Aug 01/05 1 1 1CES R Component Location R Figure 003A
R 1EFF : 301-399, 1 36-22-00Page 9/10 1 1 May 01/04 1 1 1CES R **ON A/C 301-399,
R (Ref. Fig. 003A)
R **ON A/C ALL
R (Ref. Fig. 004)
-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF. -------------------------------------------------------------------------------
LOOP A LH WING 21HF CABLE-CONNECTING 521 521EB 36-22-16 22HF ELEMENT-OVERHEAT SENSING 521 521EB 36-22-16 23HF ELEMENT-OVERHEAT SENSING 521 521AT 36-22-16 24HF CABLE-CONNECTING 521 521AT 36-22-16 25HF CABLE-CONNECTING 522 522AB 36-22-16 26HF ELEMENT-OVERHEAT SENSING 522 522AB 36-22-16 27HF ELEMENT-OVERHEAT SENSING 521 521AT 36-22-16 28HF ELEMENT-OVERHEAT SENSING 521 521EB 36-22-16 29HF ELEMENT-OVERHEAT SENSING 521 521AB 36-22-16
LOOP B LH WING 49HF ELEMENT-OVERHEAT SENSING 521 521EB 36-22-16 50HF ELEMENT-OVERHEAT SENSING 521 521AT 36-22-16 51HF CABLE-CONNECTING 521 521AT 36-22-16 52HF CABLE-CONNECTING 522 522AB 36-22-16 53HF ELEMENT-OVERHEAT SENSING 522 522AB 36-22-16 54HF ELEMENT-OVERHEAT SENSING 521 521AT 36-22-16 55HF ELEMENT-OVERHEAT SENSING 521 521EB 36-22-16 56HF ELEMENT-OVERHEAT SENSING 521 521AB 36-22-16 77HF CABLE-CONNECTING 521 521AB 36-22-16
LOOP A RH WING 37HF CABLE-CONNECTING 621 621EB 36-22-16 38HF ELEMENT-OVERHEAT SENSING 621 621EB 36-22-16 39HF ELEMENT-OVERHEAT SENSING 621 621AT 36-22-16 40HF CABLE-CONNECTING 621 621AT 36-22-16 41HF CABLE-CONNECTING 622 622AB 36-22-16 42HF ELEMENT-OVERHEAT SENSING 622 622AB 36-22-16 43HF ELEMENT-OVERHEAT SENSING 621 621AT 36-22-16 44HF ELEMENT-OVERHEAT SENSING 621 621EB 36-22-16 45HF ELEMENT-OVERHEAT SENSING 621 621AB 36-22-16 48HF CABLE-CONNECTING 192 192EB 36-22-16
LOOP B RH WING 64HF CABLE-CONNECTING 621 621EB 36-22-16
R 1EFF : ALL 1 36-22-00Page 11 1 1 May 01/04 1 1 1CES 1
Component Location - Wing Figure 004
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-------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF. ------------------------------------------------------------------------------- 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 PNEUMATIC 氣源 2(109)
