(5)
Install the bonding strip (15) and the washer (16) (Ref. TASK 20-28-00-912-004).
(6)
Install the four nuts (3). Tighten the nuts which are diagonally opposite (X sequence) and TORQUE them to 0.1 m.daN (8.84 lbf.in).
(7)
Install a new packing (4).
(8)
Install the union (2).
(9)
Remove the blanking plug from the nut (1).
(10)
Install the static line (13).
(11)
Connect the nut (1).
(12)
Install the lugs (9) on the terminals (14) with the bolts (11), the washers (10) and the nuts (8).
NOTE : The covers (12) of the static probe (8DA2) must not touch the
____ static line. Thus, make sure that the lugs (9) connected to the terminals (14) are correctly installed as shown in the figure given in this procedure.
(13) Install the covers (12).
R 1EFF : 106-149, 221-228, 231-299, 301-399, 1 34-11-16Page 411 1401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C ALL
Subtask 34-11-16-865-056
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
R 5SQ1, 5SQ2 FOR 7DA1, 8DA1 1DA1, 2DA1, 3DA1, 4DA1, 5DA1 FOR 7DA2, 8DA2 1DA2, 2DA2, 3DA2, 4DA2, 5DA2 FOR 7DA3, 8DA3 2DA3, 3DA3, 4DA3, 5DA3
Subtask 34-11-16-790-051
C. Leak Test
NOTE : The leak test is mandatory if you disconnect/connect components of
____
two static systems.
(1)
Do a leak test of the main static system (Ref. TASK 34-13-00-790-002).
(2)
Do a leak test of the standby static system
(Ref. TASK 34-21-00-790-001).
Subtask 34-11-16-710-052
D. Do an operational test of the Static Probe with the CFDS:
Do the operational test of the Probe Ice Protection
(Ref. TASK 30-31-00-710-001).
NOTE : As an alternative procedure, you can do this operational test
____
without the CFDS
(Ref. TASK 34-11-16-710-001).
1EFF : ALL 1 34-11-16Page 412 1 1 May 01/05 1 1 1CES 1
5. Close-up
________ Subtask 34-11-16-410-051
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the access door :
FOR 7DA1, 8DA1, 7DA2, 8DA2
824 (Ref. TASK 52-41-00-410-002).
FOR 7DA3, 8DA3
811
(3)
Remove the access platform(s).
1EFF : ALL 1 34-11-16Page 413 1 1 May 01/05 1 1 1CES 1 PROBE - STATIC (7DA1,7DA2,7DA3,8DA1,8DA2,8DA3) - ADJUSTMENT/TEST
________________________________________________________________
TASK 34-11-16-710-001
Test of the Static Probe (7DA1,8DA1,7DA2,8DA2,7DA3,8DA3) without the CFDS.
CAUTION : REMOVE THE PROTECTIVE COVERS FROM THE PROBES BEFORE YOU DO THE TEST.
_______
CAUTION : DO NOT CONTINUE THE TEST FOR MORE THAN ONE MINUTE TO PREVENT DAMAGE
_______ TO THE PROBES.
WARNING : DO NOT TOUCH THE PROBES IMMEDIATELY AFTER THE TEST.
_______ THEY ARE HOT AND CAN BURN YOU.
1. Reason for the Job__________________
Do this test after the removal/installation of the Static Probe
(7DA1,8DA1,7DA2,8DA2,7DA3,8DA3) when the CFDS is unserviceable.
2. Job Set-up Information______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 31-60-00-860-001 EIS Start Procedure 34-10-00-860-002 ADIRS Start Procedure 34-10-00-860-005 ADIRS Stop Procedure
3. Job Set-up
__________ Subtask 34-11-16-860-050
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Do the EIS start procedure (ECAM only) (Ref. TASK 31-60-00-860-001).
1EFF : ALL 1 34-11-16Page 501 1 1 Feb 01/98 1 1 1CES 1 1EFF : ALL 1 34-11-16Page 502 1 1 May 01/00 1 1 1CES 1
(3) Do the ADIRS start procedure for the related system: For 7DA1,8DA1 ADIRU1 For 7DA2,8DA2 ADIRU2 For 7DA3,8DA3 ADIRU3 (Ref. TASK 34-10-00-860-002).
Subtask 34-11-16-865-054
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------
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 NAVIGATION 導航1(80)
