W DOC AIRBUS | AMM A320F

GENERAL VISUAL INSPECTION OF INBOARD FIXED LEADING EDGE STRUCTURE (EWIS)


TASK 05-25-20-200-001-A
GENERAL VISUAL INSPECTION OF INBOARD FIXED LEADING EDGE STRUCTURE (EWIS)


WARNING: DO NOT EXTEND THE SLATS AND FLAPS WHEN THE THRUST REVERSER COWLS ARE DEPLOYED IN THE 45 DEG. POSITION.
ZONE: 521
ZONE: 621
1. Reason for the Job
Refer to the MPD TASK: ZL-521-01
GENERAL VISUAL INSPECTION OF INBOARD FIXED LEADING EDGE STRUCTURE (EWIS)
NOTE: This is an EWIS (Electrical Wiring Interconnection System) procedure. EWIS is defined in ESPM 20-33-11.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 3M (10 FT)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
521
INBOARD FIXED L.E STRUCTURE
621
INBOARD FIXED L.E STRUCTURE
521AB, 521AT, 521BT, 521CB, 521EB, 521GB, 521HB, 621AB, 621AT, 621BT, 621CB, 621EB, 621GB, 621HB
 C. 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 57-41-37-000-009-A
Removal of the Access Panel
TASK 57-41-37-000-010-A
Removal of the Access Panel
TASK 57-41-37-000-011-A
Removal of the Access Panel
TASK 57-41-37-000-802-A
Removal of the Access Panel 521AT(621AT)
TASK 57-41-37-400-002-A
Installation of the Pressure Relief Panels
TASK 57-41-37-400-009-A
Installation of the Access Panel
TASK 57-41-37-400-010-A
Installation of the Access Panel
TASK 57-41-37-400-011-A
Installation of the Access Panel
TASK 57-41-37-400-802-A
Installation of the Access Panel 521AT(621AT)
3. Job Set-up
Subtask 05-25-20-866-050-A
A. Aircraft Maintenance Configuration
   (1) Extend the slats (Ref. AMM TASK 27-80-00-866-004).
Subtask 05-25-20-010-050-A 4. Procedure
Subtask 05-25-20-210-050-A
A. Inspection
   (1) Do a general visual inspection of the structure of the inboard fixed leading edge.
   (2) Make sure that there are no signs of corrosion, cracks or damage.
   (3) Make sure that all the installations (wiring, ducting, piping) are attached correctly.
5. Close-up
Subtask 05-25-20-410-050-A Subtask 05-25-20-866-051-A
B. Aircraft Maintenance Configuration
   (1) Fully retract the slats (Ref. AMM TASK 27-80-00-866-005).
[Rev.10 from 2021] 2026.03.31 22:50:09 UTC