-------------------------------------------------------------------------------
1. At the SDAC 1 (1WV1) connector: On the digital multimeter display:
-
measure the voltage between pin - make sure that the voltage is AB/11D and AB/11C. 2,335V +/-0,025V.
-
measure the voltage between pin - make sure that the voltage is AE/11F and AE/11E. 2,600V +/-0,025V.
-
measure the voltage between pin - make sure that the voltage is AE/11H and AE/11G. 2,600V +/-0,025V.
NOTE : If the voltage values are not correct, possibly the accelerometer or
____ the aircraft is not in horizontal position. To adjust the accelerometer in the correct position, washers can be removed or be added. ________
5. Close-up
Subtask 31-33-00-420-051
A. Install the SDAC 1 (1WV1) (Ref. TASK 31-55-34-400-001).
1EFF : ALL 1 31-33-00Page 530 1 1 May 01/05R 1 1 1CES 1
Subtask 31-33-00-862-060
B. Put the aircraft back to its initial configuration.
(1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 31-33-00Page 531 1 1 May 01/05R 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-149, 151-199, 203-299, 301-399, 401-499,
R TASK 31-33-00-710-016 R Operational Test of the Three-Axis-Accelerometer via MCDU R 1. Reason for the Job
__________________ R Self Explanatory R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 08-21-00-200-001 R 24-41-00-861-002 R R 24-41-00-862-002 R R 31-36-00-740-008
R 3. Job Set-up
__________
R Subtask 31-33-00-861-065 Quick Leveling Using the Attitude Monitor Energize the Aircraft Electrical Circuits from the External Power De-energize the Aircraft Electrical Circuits Supplied from the External Power Access to the Parameter Call-Up Menus
R A. Aircraft Maintenance Configuration
R (1) Energize the aircraft electrical circuits
R (Ref. TASK 24-41-00-861-002).
R (2) Do the quick leveling procedure (Ref. TASK 08-21-00-200-001).
R NOTE : When the trim indicator shows the D4 position, it is not
____ R necessary to do the quick leveling procedure.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 31-33-00Page 532 1203-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1
R Subtask 31-33-00-865-078
R B. Make sure that this(these) circuit breaker(s) is(are) closed:
R -------------------------------------------------------------------------------
R PANEL DESIGNATION IDENT. LOCATION
R -------------------------------------------------------------------------------
R 121VU RCDR/ACCLRM 9TU K18
R 4. Procedure_________
R **ON A/C 001-049, 051-099, 101-105, 151-199, 203-210,
R Subtask 31-33-00-710-079
R A. Test of the Three-Axis-Accelerometer via MCDU
R (1) Get access to the ALPHA CALL up menu (Ref. TASK 31-36-00-740-008).
R (2) Make sure that these ALPHA CALL ups show the correct value:
R - LATA shows 0g +/- 0.2g
R - LONA shows 0g +/- 0.2g
R - VRTA shows 1g +/- 0.2g.
R NOTE : If the values of the ALPHA CALL ups are not correct, it is____
R possible that the accelerometer or the aircraft is not in a
R horizontal position. To adjust the accelerometer in the
R correct position, remove or add washers from or to the
R accelerometer fitting.
R **ON A/C 106-149, 211-299, 301-399, 401-499,
R Subtask 31-33-00-710-079-A
R A. Test of the Three-Axis-Accelerometer via MCDU
R (1) Get access to the ALPHA CALL up menu (Ref. TASK 31-36-00-740-008).
R (2) Make sure that these ALPHA CALL ups show the correct value:
R - LATA1 shows 0g +/- 0.2g
R - LONA1 shows 0g +/- 0.2g
R - VRTA1 shows 1g +/- 0.2g.
R NOTE : If the values of the ALPHA CALL ups are not correct, it is____
R possible that the accelerometer or the aircraft is not in a
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 31-33-00Page 533 1203-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1 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 指示/記錄系統 2(87)
