Cover Panel Figure 401A/TASK 27-92-41-991-001-A
R 1EFF : 106-149, 159-199, 211-299, 301-399, 1 27-92-41Page 405 1401-499, 1Aug 01/05 1 1 1CES 1

 Side Stick Assembly Figure 402/TASK 27-92-41-991-002-A
 1EFF : 1 1R 1CES  ALL  1 11 1 27-92-41 Page 406 May 01/03

 4. Procedure
_________
 (Ref. Fig. 402/TASK 27-92-41-991-002-A) Subtask 27-92-41-020-050
 A. Removal of the Side Stick Assembly (11).
 (1)
 Remove the screws (26) and the washers (25). Disengage the side stick assembly (11) from its support (12).

 (2)
 Disconnect the electrical connectors (13), (14), (15), (22), (23) and

 (24) and make a mark on them.

 (3)
 Remove the side stick assembly (11).

 (4)
 Put blanking caps on the electrical connectors (13), (14), (15), (16), (17), (18), (19), (20), (21), (22), (23) and (24).

 Subtask 27-92-41-010-060
 B. Removal of the Casing (If installed) NOTE : The removal of the casing is given to get access to the components
____
 (1)
 Remove the eight screws (28) and the washers (29).

 (2)
 Remove the casing assembly (27) and (30).

 1EFF : ALL 1 27-92-41Page 407 1 1 May 01/03R 1 1 1CES 1

 TASK 27-92-41-400-001
 Installation of the Side Stick Assembly 19VU (18VU)
 WARNING : MAKE SURE THAT THE SIDE STICK ASSEMBLY STAYS IN THE VERTICAL POSITION
_______
 DURING THE MAINTENANCE PROCEDURES.
 IF NOT THERE IS A RISK OF SKYDROL LEAKAGE.
 SKYDROL CAN CAUSE INJURY AND/OR DAMAGE.

 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice
 No specific access platform 1.6 m (5 ft. 3 in.)
 No specific Torque Wrench : range 0.00 to 1.20 m.daN

 (0.00 to 9.00 lbf.ft)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from the External Power 27-92-41-710-001 Operational Test of the Side Stick Assembly
 **ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
 27-92-41-991-001 Fig. 401
R **ON A/C 106-149, 159-199, 211-299, 301-399, 401-499,
 27-92-41-991-001-A Fig. 401A

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------

R **ON A/C ALL
 27-92-41-991-002-A Fig. 402
 27-92-41-991-013 Fig. 403

 3. Job Set-up
__________
 Subtask 27-92-41-861-053
 A. Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).
 Subtask 27-92-41-010-066
 B. Get Access
 (1)
 Make sure that the access platform is in position at the access door

 822.

 (2)
 Make sure that the access door 822 is open.

 (3)
 On the battery power center 105VU:

 -make sure that the protective cover is removed.
 Subtask 27-92-41-865-054
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU COM/AUDIO/ACP/F/O 5RN G07 49VU COM/AUDIO/ACP/CAPT 4RN G06 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU AUTO FLT/STICK/LOCK 13CA N16 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18

 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
 Subtask 27-92-41-860-050
 D. Aircraft Maintenance Configuration
 (Ref. Fig. 403/TASK 27-92-41-991-013)
　
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