Removal of the Solenoid

TASK 27-92-41-000-004-A
Removal of the Solenoid

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.

NOTE: This task is not applicable for the new-generation side-stick unit. For the new-generation side-stick unit, refer to the procedure (Ref. AMM TASK 27-92-41-000-802). To know if the side-stick installed on the aircraft is a new-generation side-stick unit, refer to the procedure (Ref. AMM TASK 27-92-41-860-801).

ZONE: 211
ZONE: 212
FIN: 12CA1 ** ON A/C NOT FOR ALL
FIN: 12CA2 ** ON A/C NOT FOR ALL

1. Reason for the Job
Self Explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	CAP - BLANKING
98D27303001001	1	HOLDER - SIDE STICK

B. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
211	COCKPIT
212	COCKPIT

C. Referenced Information

REFERENCE	DESIGNATION
TASK 27-92-41-000-001-A	Removal of the Side Stick Assembly
Solenoid

3. Job Set-up
Subtask 27-92-41-010-053-A

A. Remove the side stick assembly (Ref. AMM TASK 27-92-41-000-001).

Subtask 27-92-41-480-054-A

B. Install the side stick assembly on the 98D27303001001 HOLDER - SIDE STICK.

4. Procedure
Subtask 27-92-41-020-053-A

A. Removal of the Side Stick Lock-Solenoid
(1) Disconnect the electrical connector (63) from the solenoid (64).
(2) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
(3) Cut and discard the lockwire from the screws (60).
(4) Remove the screws (60), the washers (61) and the solenoid (64).

[Rev.10 from 2021] 2026.03.31 23:59:08 UTC