R 1EFF : 106-149, 221-299, 301-399, 401-499, 1 34-52-00Page 18 1 1 Aug 01/05 1 1 1CES 1 B. Transponder output buses
----------------------------------------------------------------------------| DESTINATION | LABEL | PARAMETER | ----------------------------------------------------------------------------| TCAS | 271 | TCAS coordination data 1 | | | 272 | TCAS coordination data 2 | | | 273 | Mode S ground uplink | | | 203 | Barometric altitude | | | 275 | Mode S adress part 1 | | | 276 | Mode S adress part 2 | | | 277 | Acknowledgement | | | 274 | Lock confirmation | | | 204 | Baro corrected altitude | | | 013 | TCAS display control | | | 015 | Display altitude limit | | | 016 | TCAS/ATC control | | | 210 | Airspeed | | | 212 | Altitude rate | | | 350 | Maintenance word | ----------------------------------------------------------------------------| CFDIU | 356 | Normal mode | ----------------------------------------------------------------------------
**ON A/C ALL
6. Component Description
_____________________
R **ON A/C 001-049, 101-105, 151-199,
A. ATC Transponder
(1) External description (Ref. Fig. 005) The face of the transponder is fitted with a handle, two attaching parts, a TEST pushbutton switch and ten LEDs. The name, color and function of the ten LEDs are as follows:
-
TPR (green) indicates that no faults are detected during the reply
-
TPR (red) indicates fault of ATC function
-
ANT TOP (red) indicates that the top antennas are incorrectly connected or are failed
-
ANT BOT (red) indicates that the bottom antennas are incorrectly connected or are failed
-ALT (red) indicates that the altitude is not in correct format
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ATC - Transponder Figure 005
R 1EFF : 1 1 1CES 001-049, 101-105, 151-199, 1 111 34-52-00 Page 20 May 01/05
- DATA IN (red) indicates that the data input is not in correct
format
- TCAS (red) indicates that the data input from the TCAS is abnormal
- MAINTENANCE (red) indicates that the maintenance data are abnormal
- RESERVED (red) are reserved for future use.
The back of the transponder contains an ARINC 600, shell size
connector to provide electrical connections to the aircraft wiring
via mount.
Contact grouping is as follows:
- Top contact set - ATE interface
- Center contact set - System interconnections
- Bottom contact set - Power supply and bonding.
(2) Not Applicable
R **ON A/C 051-099,
R A. ATC Transponder
R (1) External description
R (Ref. Fig. 005A)
R The face of the transponder is fitted with a handle, two attaching
R parts, a PUSH TO TEST pushbutton switch, six LEDs and a DATA LOADER
R plug.
R The PUSH TO TEST pushbutton switch is used to initiate the LED test
R and transponder self-test. All LEDs are on for approximately three
R seconds following self-test initiation. After three seconds, the
R front panel LEDs indicate the current condition of the unit.
R If the PUSH TO TEST pushbutton switch is not pushed again, the LEDs
R go off.
R If the PUSH TO TEST pushbutton switch is pushed while the LEDs are
R still on, the next previous flight leg is displayed.
R The transponder has the capability to store 10 flight legs. To
R display all stored flight legs, the PUSH TO TEST pushbutton switch
R must be pushed when the previous flight leg is being displayed. When
R all flight legs are displayed, all LEDs flash to indicate the end of
R the routine. All LEDs go off within 10 s after self-test is
R completed.
R The functions of the LEDs are indicated on the table below:
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 34-52-00Page 21 1 1 May 01/05 1 1 1CES 1
R ATC - Transponder
R Figure 005A
R 1EFF : 051-099, 1 34-52-00 Page 22
1 1 May 01/05
1 1
1CES 1
-------------------------------------------------------------------------| LEDs | FUNCTION | -------------------------------------------------------------------------| XPDR PASS (green) | On after test indicates normal operation. | |----------------------|------------------------------------------------| | XPDR FAIL (red) | On after test indicates malfunction. | |----------------------|------------------------------------------------| | CNTL PNL (red) | On after test indicates abnormal input of 429 | | | word data from control unit, or associated | | | circuitry. | |----------------------|------------------------------------------------| | TOP ANT (red) | Indicates that the upper antennas are | | | incorrectly connected or are failed (comes on | | | during BITE self-test). | |----------------------|------------------------------------------------| | BOT ANT (red) | Indicates that the lower antennas are | | | incorrectly connected or are failed (comes on | | | during BITE self-test). | |----------------------|------------------------------------------------| | ALT SIG (red) | On after test indicates abnormal input from | | | ALT data system bus, or associated circuitry. | |----------------------|------------------------------------------------| 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM NAVIGATION 導航4(100)
