Removal of the No. 5 Slat

TASK 27-84-67-000-001-A
Removal of the No. 5 Slat

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.

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.

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.

CAUTION: THIS PART IS A REMOVABLE STRUCTURAL COMPONENT (RSC), WHICH CAN BE MOVED BETWEEN AIRCRAFT. THUS IT CAN HAVE DIFFERENT OPERATION CONDITIONS AND A DIFFERENT LIFE RECORD (FLIGHT HOURS/FLIGHT CYCLES/CALENDAR) FROM THE AIRCRAFT IT IS INSTALLED ON OR REMOVED FROM. THE OPERATOR IS RESPONSIBLE FOR THE SPECIFIC TRACKING AND CONTINUED AIRWORTHINESS OF REMOVABLE STRUCTURAL COMPONENTS. INCORRECT MAINTENANCE OF THESE COMPONENTS CAN CAUSE A RISK FOR THE FLIGHT SAFETY.

ZONE: 510
ZONE: 610

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 4M (13 FT)-ADJUSTABLE
No specific	AR	COVER - BLANKING, HYDRAULIC RESISTANT
No specific	AR	SAFETY BARRIER(S)
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	AR	SUPPORT STRUCTURE - FLAP
No specific	AR	WARNING NOTICE(S)
No specific	AR	WRENCH - PNEUMATIC
98D27504030001	1	LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
98D27803000000	1	LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
98D27804001000	1	ADAPTOR-DRIVE, SLAT (AND FLAP)
98D27804009001	1	SLATS - SLING
98F27508498000	AR	HOIST-R I,FLAP SLAT

B. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
510	LEFT WING SLATS
610	RIGHT WING SLATS
522NB, 622NB

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 27-50-00-000-003-A	Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)
TASK 27-50-00-400-003-A	Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)
TASK 27-80-00-000-001-A	Removal of the Hoisting Sling
TASK 27-80-00-400-001-A	Installation of the Hoisting Sling
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 27-84-45-000-004-A	Removal of the Torque Shafts 6010CM and 6060CM
TASK 27-84-69-000-001-A	Removal of the Closing Plates for the Slat Tracks 1 thru 12
TASK 57-41-37-000-006-A	Removal of the Access Panels
Slat-to-Slat Interface - Location
Slat Attachment at the No. 11 Slat Track ** ON A/C NOT FOR ALL
Slat Attachment at the No. 12 Slat Track ** ON A/C NOT FOR ALL
Slat Attachment at the No. 11 Slat Track ** ON A/C NOT FOR ALL
Slat Attachment at the No. 12 Slat Track ** ON A/C NOT FOR ALL
Slat Attachment at the No. 11 Slat Track - Detail

3. Job Set-up
Subtask 27-84-67-941-050-A

A. Safety Precautions
(1) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.
(2) Retract the slats:

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.

(a) Make sure the slats are fully retracted (Ref. AMM TASK 27-80-00-866-005).
(3) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the flap/slat control lever on panel 114VU.
(4) Put WARNING NOTICE(S) in position to tell persons not to operate the slat controls.

Subtask 27-84-67-860-055-A

B. 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 27-84-67-865-050-A

C. 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/WTB/SLT/SYS2	11CV	P19
121VU	FLIGHT CONTROLS/SLT/CTL/SYS2	7CV	R21
122VU	FLIGHT CONTROLS/WTB/SLT/SYS1	9CV	S06

Subtask 27-84-67-010-050-A

D. Get Access
(1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE below the zone 510(610).
(2) Remove the applicable access panel (Ref. AMM TASK 57-41-37-000-006):
(a) For the left wing, remove access panel 522NB.
(b) For the right wing, remove access panel 622NB.
(3) Remove the applicable torque shaft (Ref. AMM TASK 27-84-45-000-004):
(a) For the left wing, remove: [6010CM]
(b) For the right wing, remove [6060CM]
(4) Install the 98D27804001000 ADAPTOR-DRIVE, SLAT (AND FLAP) and a WRENCH - PNEUMATIC on the applicable bevel gearbox:
(a) For the left wing, use [6010CM]
(b) For the right wing, use [6060CM]

NOTE: This will let you operate the slats manually.

(5) Remove the 98D27504030001 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT, installed outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. AMM TASK 27-50-00-000-003).
(6) Fully extend the slats:

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.

(a) Manually extend the slats to the fully extended position.
(7) Install the 98D27504030001 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT outboard of the removed torque shaft FIN 6010CM(6060CM) (Ref. AMM TASK 27-50-00-400-003).
(8) Remove the slat track closing plates (28) and (53) (Ref. AMM TASK 27-84-69-000-001).

Subtask 27-84-67-480-051-A

E. Installation of the Support Equipment
(1) Install the 98D27804009001 SLATS - SLING (Ref. AMM TASK 27-80-00-400-001) or the 98F27508498000 HOIST-R I,FLAP SLAT.

4. Procedure
Subtask 27-84-67-020-051-B

A. Removal of the No. 5 Slat
(1) Lift the 98D27804009001 SLATS - SLING or the 98F27508498000 HOIST-R I,FLAP SLAT, until it has the weight of the slat.
(2) Disconnect the slat-to-track bonding strap at No. 11 slat track:
(a) Remove the nut (19), the washer (20) and the bonding strap (21) from the bolt (24). Do not remove the bolt (24).
(b) Install the washer (20) and the nut (19) on the bolt (24).
(3) Disconnect the slat-to-slat interface:
(a) Remove the nut (6), the bolt (9) and the washer (8). Then move the bonding strap (7) away from the bonding tag.
(b) Remove the screws (1) and the stops (3).
(c) Remove the weather seal (2).
(d) Loosen the clamps (5) and then remove the flexible tube (4) and the clamps (5).
(e) Install COVER - BLANKING, HYDRAULIC RESISTANT on the open ends of the anti-icing ducts.
(4) At the Nos. 11 and 12 slat tracks:
(a) Remove and discard the cotter pins (27) from the nuts (35), (47), (46) and (45).
(b) Loosen the nuts (35), (47), (46) and (45), but do not remove them.
(c) Remove and discard the cotter pins (27) from the nuts (26), (31), (43) and (44).
(d) Remove the items that follow, the:

nuts (26), (31), (43) and (44)
washers (25), (30), (51) and (52)
bolts (18), (32), (48) and (56)
bush (29).

NOTE: The bush (29) is a part of the slat track and the slat track linkage assembly.

(e) Make sure that when the nut (31) is removed, the head of the bolt (32) is in contact with the web of the lug. If not damage can occur to the anti-rotation.

Slat Attachment at the No. 11 Slat Track - Detail

(5) Lift the slat ( 30 kg (66.14 lb)) from the slat tracks.
(6) Move the slat with the hoist and lower it onto the SUPPORT STRUCTURE - FLAP.

Subtask 27-84-67-860-053-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.

CAUTION: MAKE SURE THAT THE SLAT TRACK LINKS DO NOT TOUCH THE WING, IF YOU RETRACT THE SLAT SYSTEM AFTER A SLAT HAS BEEN REMOVED.

(1) If you install a new slat, remove the 98D27804009001 SLATS - SLING (Ref. AMM TASK 27-80-00-000-001) or the 98F27508498000 HOIST-R I,FLAP SLAT.

[Rev.10 from 2021] 2026.03.31 23:58:14 UTC