R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 34-13-00Page 593 1201-299, 301-302, 1May 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
7.
Do the ADR3 test as specified in Same results on the CAPT side.
the para. 1 and 2.
8.
On the ADIRS CDU, push the ADR1 On the ADIRS CDU, the OFF legend of the pushbutton switch. ADR1 pushbutton switch goes off
9.
On the SWITCHING panel 8VU: On the CAPT PFD, the speed and altitude
-set the AIR DATA selector indications stay in view.
switch to NORM.
10.
On the ADIRS CDU, set the three
OFF/NAV/ATT selector switches to
OFF.
After the ADR3 test, set the AIR
DATA selector switch 15FP to
NORMAL.
R **ON A/C 106-149, 303-399, 401-499,
Subtask 34-13-00-740-050-B
A. INTERFACE TEST of the ADR
NOTE : - Ignore the warnings and indications (VLE, ...) which are not
____
related to this interface test.
-When you test the ADR3, set the AIR DATA selector switch 15FP, on the SWITCHING panel 8VU, to CAPT/3.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ADIRS CDU:
-Set the three OFF/NAV/ATT
selector switches to NAV
-
push the ADR1, ADR2 and ADR3 The OFF legend of the ADR1, ADR2 and pushbutton switches ADR3 pushbutton switches comes on.
-
push the ADR1 (ADR2) (ADR3, On the ADIRS CDU, the OFF legend of the only if the AIR DATA selector ADR pushbutton switch goes off
1EFF : ALL 1 34-13-00Page 594 1 1 Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
switch is to CAPT/3 or F/O/3) pushbutton switch again.
2. On the MCDU:
-
push the line key adjacent to the ADR1 (ADR2) (ADR3) indication
-
push the line key adjacent to the OUTPUT TESTS indication.
-
push the line key adjacent to the INTERFACE TEST indication
- on the keyboard push the NEXT PAGE function key.
-
push the line key adjacent to the START TEST indication
On the CAPT (F/O) PFD, the SPD and ALTflags go out of view. The speed and altitude indications (30 Kts and local altitude) are shown On the lower ECAM display unit, the local temperature values SAT and TAT are shown (only with ADR1 and/or ADR3 is set).
-
the ADR1 (ADR2) (ADR3) page comesinto view.
-
the ADR1 (ADR2) (ADR3) OUTPUT TESTSpage comes into view.
-
the ADR1 (ADR2) (ADR3) INTERFACE TEST1/2 page comes into view.
-
the ADR1 (ADR2) (ADR3) INTERFACE TEST2/2 page comes into view.
From 0 to 5 seconds:
- on the ADIRS CDU, the FAULT and OFF legends of the ADR1 (ADR2) (ADR3) pushbutton switch come on then go off
- on the CAPT (F/O) PFD, the symbols on the speed and altitude scale go out of view. The SPD and ALT warning flags flash for some seconds
- on the CAPT (F/O) ND, the TAS indication goes out of view From 5 to 10 seconds:
- on the CAPT (F/O) PFD, the warnings go out of view
- on the lower ECAM display unit, in the Inop System part, the message ADR 2 + 3 (ADR 1 + 3) (ADR 1 + 2) comes into view.
- on the CAPT (F/O) PFD, the altitude increases. After 10 seconds:
R 1EFF : 106-149, 303-399, 401-499, 1 34-13-00Page 595 1 1 Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-push the line key adjacent to the RETURN indication.
3.
On the ADIRS CDU, push the ADR2 pushbutton switch.
4.
Do the ADR2 test as specified in the para. 1 and 2.
5.
On the ADIRS CDU:
-push the ADR3 pushbutton switch
- on the CAPT (F/O) PFD, these values are shown: CAS: 367.7 Kts MACH: 0.66 M ALTITUDE: 10000 Ft
- on the CAPT (F/O) ND, this value is shown: TAS: 433 Kts
- on the lower ECAM display unit, (if ADR1 and/or ADR3 is set) these values are shown: TAT: + 35 deg. C SAT: + 10 deg. C
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2(11)
