Removal of the Type B Actuators

TASK 27-84-49-000-002-A
Removal of the Type B Actuators

WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:

THE FLIGHT CONTROLS
THE FLIGHT CONTROL SURFACES
THE LANDING GEAR AND THE RELATED DOORS
COMPONENTS THAT MOVE.

MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE EQUIPMENT.

WARNING: MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.

ZONE: 522
ZONE: 622
FIN: 6033CM
FIN: 6037CM
FIN: 6041CM
FIN: 6083CM
FIN: 6087CM
FIN: 6091CM

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	ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE
No specific	AR	SAFETY BARRIER(S)
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	AR	WARNING NOTICE(S)
98D27504030001	2	LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
98D27803500001	1	LOCKING TOOL ZERO POS
98D27803500002	1	LOCKING TOOL ZERO POS
98D27804007000	AR	TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 5 TO 12)

B. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
522	OUTBOARD FIXED L.E STRUCTURE
622	OUTBOARD FIXED L.E STRUCTURE

C. Referenced Information

REFERENCE	DESIGNATION
TASK 24-41-00-861-002-A	Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01	Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02	Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A	De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01	De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02	De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 27-50-00-400-003-A	Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)
TASK 27-80-00-860-801-A	Readout of the Slat Position Pickoff Unit (PPU) Data
TASK 27-80-00-866-005-A	Retracting the Slats on the Ground
TASK 27-84-45-000-006-A	Removal of the Torque Shafts
TASK 27-84-45-000-011-A	Removal of the Torque Shaft
TASK 27-84-45-000-012-A	Removal of the Torque Shaft
Type B Actuators - Slat Power Transmission ** ON A/C NOT FOR ALL
Type B Actuators - Slat Power Transmission ** ON A/C NOT FOR ALL

3. Job Set-up
Subtask 27-84-49-941-053-A

A. Safety Precautions

WARNING: BEFORE YOU START WORK, YOU MUST PUT ON A SAFETY HARNESS AND ATTACH IT TO THE ACCESS PLATFORM. WITHOUT A SAFETY HARNESS, YOU CAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.

(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Put WARNING NOTICE(S) in the cockpit to tell persons not to operate the slat controls.

Subtask 27-84-49-860-051-A

B. Aircraft Maintenance Configuration

WARNING: MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.

(1) Retract the slats fully (Ref. AMM TASK 27-80-00-866-005).
(2) Install the 98D27803500001 LOCKING TOOL ZERO POS or 98D27803500002 LOCKING TOOL ZERO POS on the slat/flap control lever on panel 114VU.

Subtask 27-84-49-740-056-A

C. Readout of the PPU Data
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
(2) Do the readout of the PPU data (Ref. AMM TASK 27-80-00-860-801).

NOTE: Airbus recommends to do the readout and recording of the PPU angles before the maintenance action.
In case of a loss of the torque shaft fixture you can put the slat transmission system back to the initial condition (without a complete adjustment of the system).

(3) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).

Subtask 27-84-49-865-055-A

D. Open, safety and tag this(these) circuit breaker(s):

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1	5CV	B06
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1	5CV	B01
** ON A/C ALL
121VU	FLIGHT CONTROLS/SLT/CTL/SYS2	7CV	R21

Subtask 27-84-49-010-052-A

E. Get Access
(1) Put an ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable torque shaft.
(2) Remove the applicable torque shaft (3) (Ref. AMM TASK 27-84-45-000-006) and (Ref. AMM TASK 27-84-45-000-011):
(a) FOR [6037CM] (SLAT ACTUATOR TYPE B)
remove the torque shaft FIN 6036CM.
(b) FOR [6041CM] (SLAT ACTUATOR TYPE B)
remove the torque shaft FIN 6040CM.
(c) FOR [6087CM] (SLAT ACTUATOR TYPE B)
remove the torque shaft FIN 6086CM.
(d) FOR [6091CM] (SLAT ACTUATOR TYPE B)
remove the torque shaft FIN 6090CM.
(e) FOR [6033CM] (SLAT ACTUATOR TYPE B)
remove the torque shaft FIN 6032CM.
(f) FOR [6083CM] (SLAT ACTUATOR TYPE B)
remove the torque shaft FIN 6082CM.
(3) Remove the applicable torque shaft (1) (Ref. AMM TASK 27-84-45-000-012) and (Ref. AMM TASK 27-84-45-000-006):
(a) FOR [6033CM] (SLAT ACTUATOR TYPE B)
remove the torque shaft FIN 6034CM.
(b) FOR [6083CM] (SLAT ACTUATOR TYPE B)
remove the torque shaft FIN 6084CM.
(c) FOR [6037CM] (SLAT ACTUATOR TYPE B)
remove the torque shaft FIN 6038CM.
(d) FOR [6041CM] (SLAT ACTUATOR TYPE B)
remove the torque shaft FIN 6042CM.
(e) FOR [6087CM] (SLAT ACTUATOR TYPE B)
remove the torque shaft FIN 6088CM.
(f) FOR [6091CM] (SLAT ACTUATOR TYPE B)
remove the torque shaft FIN 6092CM.
(4) Make sure that a 98D27504030001 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed (Ref. AMM TASK 27-50-00-400-003) as follows:

On the torque shaft inboard of the removed component
On the torque shaft outboard of the removed component.

4. Procedure
Subtask 27-84-49-020-051-A

A. Removal of the Type B Actuators
(1) Hold the actuator (2) and remove the bolts (4) and washers (5).
(2) Remove the actuator (2).
(3) If you remove both actuators from a slat, install a 98D27804007000 TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 5 TO 12) in each pinion after each actuator (2) is removed or the slat will extend.

[Rev.10 from 2021] 2026.04.01 07:08:45 UTC