Special Detailed Inspection of Outer Wing, Fixed Leading Edge Pinion Fitting Bolting and Actuator Bolting Lower Bolt Holes on Ribs 2, 3, 5, 6, 7, 8....

TASK 57-41-00-200-017-A
Special Detailed Inspection of Outer Wing, Fixed Leading Edge Pinion Fitting Bolting and Actuator Bolting Lower Bolt Holes on Ribs 2, 3, 5, 6, 7, 8....

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: 540
ZONE: 640

1. Reason for the Job
Refer to the MPD TASK: 574114-01
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, FIXED LEADING EDGE PINION FITTING BOLTING AND ACTUATOR BOLTING LOWER BOLT HOLES ON RIB 2,3,5,6,7,8,9,10,11 AND 12

NOTE: The effectivity of this task is ALL. To know if this task is applicable for your aircraft, refer to the MPD task applicability and the weight variant data given in the SRM introduction.

2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	1	ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE
No specific	AR	SAFETY BARRIER(S)
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	1	WARNING NOTICE(S)

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.08BAA9)	Non Aqueous Cleaner-General - -
(Material No.14SBA1)	Textile-Lint free Cotton -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
540	FUEL TANK
640	FUEL TANK
521CB, 521EB, 522CB, 522FB, 522KB, 522LB, 522NB, 522QB, 522SB, 522UB, 621CB, 621EB, 622CB, 622FB, 622KB, 622LB, 622NB, 622QB, 622SB, 622UB
522AB, 622AB
522XB, 522YB, 622XB, 622YB

D. Referenced Information

REFERENCE	DESIGNATION
TASK 27-80-00-866-004-A	Extending the Slats on the Ground
TASK 27-80-00-866-005-A	Retracting the Slats on the Ground
TASK 57-41-37-000-004-A	Removal of the Pressure Relief Panels
TASK 57-41-37-000-006-A	Removal of the Access Panels
TASK 57-41-37-400-002-A	Installation of the Pressure Relief Panels
TASK 57-41-37-400-006-A	Installation of the Access Panels
NTM 574114
SRM 574000	(for corrective action)
Access Panels - Wing Lower Leading-Edge ** ON A/C NOT FOR ALL
Access Panels - Wing Lower Leading-Edge ** ON A/C NOT FOR ALL
Location and Details of the Bolt Holes of the Leading Edge Pinion Fitting and Actuator Fitting (Tracks 2, 3 and 5 thru 12)

3. Job Set-up
Subtask 57-41-00-941-063-A

A. Safety Precautions
(1) Put a WARNING NOTICE(S) in the cockpit to tell persons not to operate the flaps or slats.
(2) As necessary, use the applicable SAFETY BARRIERS, specified by the operator's instructions and your local regulations.

Subtask 57-41-00-860-072-A

B. Aircraft Maintenance Configuration
(1) Fully extend the slats (Ref. AMM TASK 27-80-00-866-004).
(2) Make sure the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is installed on the flap/slat control lever.

Subtask 57-41-00-865-074-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/SLT/CTL/SYS2	7CV	R21

Subtask 57-41-00-010-055-A ** ON A/C NOT FOR ALL

D. Get Access
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position below the applicable wing leading edge at the zones 521(621) and 522(622).

Access Panels - Wing Lower Leading-Edge ** ON A/C NOT FOR ALL

(2) Remove the applicable access panels (Ref. AMM TASK 57-41-37-000-004) and (Ref. AMM TASK 57-41-37-000-006):

For the left wing: 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB, 522NB, 522QB, 522SB and 522UB
For the right wing: 621CB, 621EB, 622AB, 622CB, 622FB, 622KB, 622LB, 622NB, 622QB, 622SB and 622UB.

Subtask 57-41-00-010-055-B ** ON A/C NOT FOR ALL

D. Get Access
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position below the applicable wing leading edge at the zones 521(621) and 522(622).

Access Panels - Wing Lower Leading-Edge ** ON A/C NOT FOR ALL

(2) Remove the applicable access panels (Ref. AMM TASK 57-41-37-000-004) and (Ref. AMM TASK 57-41-37-000-006):

For the left wing: 521CB, 521EB, 522XB, 522YB, 522CB, 522FB, 522KB, 522LB, 522NB, 522QB, 522SB and 522UB
For the right wing: 621CB, 621EB, 622XB, 622YB, 622CB, 622FB, 622KB, 622LB, 622NB, 622QB, 622SB and 622UB.

4. Procedure
Subtask 57-41-00-110-061-A

A. Preparation for Inspection
(1) Use a Textile-Lint free Cotton - (Material No.14SBA1) , made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) to clean the pinion-fitting and the actuator-fitting bolt holes.

Subtask 57-41-00-280-050-A

B. Inspection
(1) Do a special detailed inspection of the outer wing fixed leading edge pinion fitting bolting and the actuator fitting lower bolt holes NTM 574114.

NOTE: If necessary, refer to the ASRM SRM 574000 for the correct repair procedure. If the defect is not included in this repair, you must request a procedure from AIRBUS.

5. Close-up
Subtask 57-41-00-410-055-A ** ON A/C NOT FOR ALL

A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the applicable access panels (Ref. AMM TASK 57-41-37-400-002) and (Ref. AMM TASK 57-41-37-400-006):

For the left wing: 521CB, 521EB, 522AB, 522CB, 522FB, 522KB, 522LB, 522NB, 522QB, 522SB and 522UB
For the right wing: 621CB, 621EB, 622AB, 622CB, 622FB, 622KB, 622LB, 622NB, 622QB, 622SB and 622UB.

Subtask 57-41-00-410-055-B ** ON A/C NOT FOR ALL

For the left wing: 521CB, 521EB, 522XB, 522YB, 522CB, 522FB, 522KB, 522LB, 522NB, 522QB, 522SB and 522UB
For the right wing: 621CB, 621EB, 622XB, 622YB, 622CB, 622FB, 622KB, 622LB, 622NB, 622QB, 622SB and 622UB.

Subtask 57-41-00-865-075-A

B. Remove the safety clip(s) and the tag(s) and close 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 57-41-00-860-073-A

C. Aircraft Maintenance Configuration
(1) Remove the access platform(s).
(2) Retract the slats (Ref. AMM TASK 27-80-00-866-005).

Subtask 57-41-00-942-068-A

D. Removal of Equipment
(1) Remove the WARNING NOTICE(S).
(2) Remove the safety barriers.
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

[Rev.10 from 2021] 2026.04.02 06:30:58 UTC