Removal of the Transducer Units

TASK 27-92-41-000-002-A
Removal of the Transducer Units

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: 4CE1 ** ON A/C NOT FOR ALL
FIN: 4CE2 ** ON A/C NOT FOR ALL
FIN: 4CE3 ** ON A/C NOT FOR ALL
FIN: 4CE4 ** 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
Transducer Units

3. Job Set-up
Subtask 27-92-41-010-051-A

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

Subtask 27-92-41-480-052-A

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

4. Procedure
Subtask 27-92-41-020-051-A

A. Removal of the Side Stick Transducer-Unit
(1) Cut and discard the cotter pins (35) from the nuts (34).
(2) Remove the nuts (34), the washers (36).
(3) Remove the bolts (33).

NOTE: The bush is part of the bolt.

(4) Disconnect the rods (32).
(5) Remove the nuts (38)
or remove the bolts (46) and the washers (45).
(6) Remove the transducer unit (37).
(7) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.

[Rev.10 from 2021] 2026.03.31 23:59:01 UTC