Inspection After Impact on Sharklet

TASK 05-51-35-200-001-B
Inspection After Impact on Sharklet

WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN POSITION BEFORE YOU START A TASK ON OR NEAR:

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

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

ZONE: 534
ZONE: 634

1. Reason for the Job
This inspection is only applicable if the aircraft was stopped or in low speed movement.

NOTE: For all other conditions, it is necessary to refer to Airbus.

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

REFERENCE	QTY	DESIGNATION
No specific	AR	ACCESS PLATFORM 6M (20 FT) - ADJUSTABLE
No specific	AR	SAFETY BARRIER(S)
No specific	AR	WARNING NOTICE(S)
98D27803500001	1	LOCKING TOOL ZERO POS
98D27903500000	2	PIN-SIDE STICK LOCKING

B. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
534	WING TIP
634	WING TIP
197CB, 198CB, 534BB, 534DB, 560AB, 634BB, 634DB, 660AB

C. Referenced Information

REFERENCE	DESIGNATION
TASK 23-61-00-200-001-A	Resistance Check from the Tip to the Retainer and Bonding Check from the Retainer to the Aircraft Structure
TASK 23-61-41-000-001-A	Removal of the Static Discharger
TASK 23-61-41-400-001-A	Installation of the Static Discharger
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 33-41-00-710-001-A	Operational Test of the Navigation Lights
TASK 33-48-00-710-002-A	Operational Test of the Anti-Collision/Strobe Lighting
TASK 57-30-00-200-001-A	Detailed Inspection of Wing Tip, Bottom Skin Lower Surface Joint, Outboard of RIB27
TASK 57-31-23-000-801-A	Removal of the Sharklet
TASK 57-31-23-400-801-A	Installation of the Sharklet
TASK 57-37-13-000-801-A	Removal of the Navigation-Light Glazing Panel
TASK 57-37-13-000-802-A	Removal of the Strobe-Light Glazing Panel
TASK 57-37-13-400-801-A	Installation of the Navigation-Light Glazing Panel
TASK 57-37-13-400-802-A	Installation of the Strobe-Light Glazing Panel
NTM 511003
SRM 572111
SRM 573123
Wing Sharklet External Inspection ** ON A/C NOT FOR ALL
Inspection of RIB27 ** ON A/C NOT FOR ALL

3. Job Set-up
Subtask 05-51-35-941-051-A ** ON A/C NOT FOR ALL

A. Safety Precautions
(1) In the cockpit, put a:

98D27803500001 LOCKING TOOL ZERO POS on the flap/slat control lever
98D27903500000 PIN-SIDE STICK LOCKING in the Captain side-stick (on the LH lateral console)
98D27903500000 PIN-SIDE STICK LOCKING in the First Officer side-stick (on the RH lateral console)
WARNING NOTICE(S) in position to tell persons not to operate the flight controls
WARNING NOTICE(S) on the overhead panel, on the HYD section of panel 40VU (to tell persons not to pressurize the hydraulic system)
WARNING NOTICE(S) on panel 25VU to tell persons not to operate the navigation lights or the strobe lights.

(2) Put a WARNING NOTICE(S) in position on the ground service panel (access panel 197CB) to tell persons not to operate the Green hydraulic system.
(3) Put a WARNING NOTICE(S) in position on the ground service panel (access panel 198CB) to tell persons not to operate the Yellow hydraulic system.
(4) Put the SAFETY BARRIER(S) in position.
(5) Put an ACCESS PLATFORM 6M (20 FT) - ADJUSTABLE below the applicable wing-sharklet, zone 534(634).

Subtask 05-51-35-861-050-A ** ON A/C NOT FOR ALL

B. Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).

Subtask 05-51-35-865-052-A ** ON A/C NOT FOR ALL

C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/ELAC1/NORM/SPLY	15CE1	B11
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/ELAC1/NORM/SPLY	15CE1	B06
** ON A/C NOT FOR ALL
105VU	FLIGHT CONTROLS/ELAC2/STBY SPLY	16CE2	A02
105VU	FLT CTL/ELAC1/STBY SPLY	16CE1	A01
121VU	FLIGHT CONTROLS/ELAC2/NORM/SPLY	15CE2	R20
122VU	LIGHTING/EXT LT/NAV2/AND LOGO/LT	2LA	T02
122VU	LIGHTING/WING/STROBE	10LV	V05
** ON A/C NOT FOR ALL
122VU	LIGHT/EXT LT NAV1/AND LOGO/LT	1LA	T03
** ON A/C NOT FOR ALL
122VU	LIGHTING/EXT LT/NAV1/AND LOGO/LT	1LA	T03

4. Procedure
Subtask 05-51-35-210-051-A ** ON A/C NOT FOR ALL

A. Inspection of the wing sharklet after an impact

ITEM	INSPECTION TASKS	PHASE 1	PHASE 2	PHASE 3
1.	Inspections
A.	(1) Do a detailed visual inspection for signs of impact, distortion and pulled or loose fasteners on the items that follow: - The sharklet - The wing-to-sharklet panel - The upper surface joint - The lower-skin lower surface joint (Ref. AMM TASK 57-30-00-200-001). Wing Sharklet External Inspection ** ON A/C NOT FOR ALL	X
	(2) On the sharklet composite area, do an NDT inspection for delamination. Refer to the Non-destructive Testing Manual: NTM 511003.	X
B.	If you find damage on the sharklet (scratch, dent, deformation, delamination):
	- Refer to the SRM 573123 allowable damage.		X
	If the damage is more than the SRM allowable damage:
	(1) Remove the sharklet (Ref. AMM TASK 57-31-23-000-801).			X
	(2) Do an inspection of RIB27 (internal and external sides). Inspection of RIB27 ** ON A/C NOT FOR ALL			X
	(3) Contact Airbus for more instructions.			X
	(4) Install the sharklet: (Ref. AMM TASK 57-31-23-400-801).			X
C.	If you find damage (scratch, dent, deformation) on the wing-to-sharklet panels: Wing Sharklet External Inspection ** ON A/C NOT FOR ALL
	(1) Open the damaged access panels: 534BB and 534DB or 634BB and 634DB.		X
	(2) Refer to the SRM 573123 allowable damage.		X
	If the damage is more than the SRM allowable damage:
	(a) Repair or replace the damaged access panel SRM 573123.			X
	(b) Open access panel 560AB or 660AB.			X
	(c) Do a detailed visual inspection of the sharklet attachment fittings and internal structure at RIB27 SRM 573123. Inspection of RIB27 ** ON A/C NOT FOR ALL			X
	- If you find damage: Contact Airbus for more instructions.			X
	(d) Close access panel 560AB or 660AB.			X
	(3) Close the access panels: 534BB and 534DB or 634BB and 634DB.		X
D.	If you find damage on the wing external structure:
	- Refer to the SRM 572111 allowable damage.		X
	If the damage is more than the SRM allowable damage:
	- Contact Airbus for more instructions.			X
2.	Do a detailed visual inspection of the navigation-light and strobe-light glazing panel. Wing Sharklet External Inspection ** ON A/C NOT FOR ALL	X
A.	If you find damage: Replace the glazing panel.		X
	For the navigation-light glazing panel: (Ref. AMM TASK 57-37-13-000-801) and (Ref. AMM TASK 57-37-13-400-801).		X
	For the strobe-light glazing panel: (Ref. AMM TASK 57-37-13-000-802) and (Ref. AMM TASK 57-37-13-400-802).		X
	Do an operational test of the light with the replaced glazing panel.
	For the navigation-light: (Ref. AMM TASK 33-41-00-710-001).		X
	For the strobe-light: (Ref. AMM TASK 33-48-00-710-002).		X
3.	Examine the static dischargers and retainers for damage (Ref. AMM TASK 23-61-00-200-001).	X
A.	If you find damage: Replace the static dischargers (Ref. AMM TASK 23-61-41-000-001) and (Ref. AMM TASK 23-61-41-400-001). NOTE: 20% of the static dischargers can be unserviceable or missing on each wing.		X

5. Close-up
Subtask 05-51-35-865-053-A ** ON A/C NOT FOR ALL

A. 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/ELAC1/NORM/SPLY	15CE1	B11
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/ELAC1/NORM/SPLY	15CE1	B06
** ON A/C NOT FOR ALL
105VU	FLIGHT CONTROLS/ELAC2/STBY SPLY	16CE2	A02
105VU	FLT CTL/ELAC1/STBY SPLY	16CE1	A01
121VU	FLIGHT CONTROLS/ELAC2/NORM/SPLY	15CE2	R20
122VU	LIGHTING/EXT LT/NAV2/AND LOGO/LT	2LA	T02
122VU	LIGHTING/WING/STROBE	10LV	V05
** ON A/C NOT FOR ALL
122VU	LIGHT/EXT LT NAV1/AND LOGO/LT	1LA	T03
** ON A/C NOT FOR ALL
122VU	LIGHTING/EXT LT/NAV1/AND LOGO/LT	1LA	T03

Subtask 05-51-35-862-050-A ** ON A/C NOT FOR ALL

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

Subtask 05-51-35-942-051-A ** ON A/C NOT FOR ALL

C. Removal of Equipment
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Remove the SAFETY BARRIER(S).
(3) Remove the 98D27803500001 LOCKING TOOL ZERO POS from the flap/slat control lever.
(4) Remove the 98D27903500000 PIN-SIDE STICK LOCKING from the Captain side-stick (on the LH lateral console).
(5) Remove the 98D27903500000 PIN-SIDE STICK LOCKING from the First Officer side-stick (on the RH lateral console).
(6) Remove the WARNING NOTICE(S).
(7) Remove the access platform(s).
(8) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

[Rev.10 from 2021] 2026.03.31 22:51:56 UTC