W DOC AIRBUS | AMM A320F

Detailed Inspection of the LH and RH Wing Leading-Edge Overheat-Sensing- Elements


TASK 36-22-16-200-803-A
Detailed Inspection of the LH and RH Wing Leading-Edge Overheat-Sensing- Elements


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: 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.
WARNING: DO NOT TOUCH THE COMPONENT UNTIL IT IS SUFFICIENTLY COOL TO PREVENT BURNS.
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
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)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
191CT, 191EB, 192CT, 192EB, 521AB, 521BB, 521BT, 521CB, 521EB, 521GB, 522AT, 522CB, 522EB, 522FB, 522XB, 522YB, 621AB, 621BB, 621BT, 621CB, 621EB, 621GB, 622AT, 622CB, 622EB, 622FB, 622XB, 622YB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 20-28-00-912-802-A
Electrical Bonding - General Maintenance Procedure
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 32-00-00-481-001-A
Installation of the Safety Devices on the Landing Gears
TASK 53-35-11-000-001-A
Removal of the Wing-to-Fuselage Fairings
TASK 53-35-11-400-001-A
Installation of the Wing-to-Fuselage Fairings
TASK 53-35-13-000-002-A
Removal of the Quick-Release Access Panels from the Belly Fairing Structure
TASK 53-35-13-400-002-A
Installation of the Quick-Release Access Panels on the Belly Fairing Structure
TASK 57-41-37-000-003-A
Removal of the Access Panel
TASK 57-41-37-000-004-A
Removal of the Pressure Relief Panels
TASK 57-41-37-000-005-A
Removal of the NACA Duct Panel
TASK 57-41-37-000-006-A
Removal of the Access 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 57-41-37-000-012-A
Removal of the Access Panel
TASK 57-41-37-400-002-A
Installation of the Pressure Relief Panels
TASK 57-41-37-400-003-A
Installation of the Access Panel
TASK 57-41-37-400-005-A
Installation of the NACA Duct Panel
TASK 57-41-37-400-006-A
Installation of the Access 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 57-41-37-400-012-A
Installation of the Access Panel
3. Job Set-up
Subtask 36-22-16-941-067-A
A. Safety Precautions
   (1) Put the SAFETY BARRIER(S) in position.
   (2) Put a WARNING NOTICE(S) in position in the cockpit to tell persons not to operate the slat controls.
   (3) Make sure that the ground safety locks are installed on the landing gear (Ref. AMM TASK 32-00-00-481-001).
Subtask 36-22-16-860-084-A
B. Aircraft Maintenance Configuration
   (1) Extend the slats fully (Ref. AMM TASK 27-80-00-866-004).
Subtask 36-22-16-865-084-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
49VUAIR BLEED/ENG 2/MONG3HA2D12
49VUAIR BLEED/ENG 1/CTL2HA1D11
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
122VUAIR BLEED/ENG 1/MONG3HA1Z23
122VUAIR BLEED/ENG 2/CTL2HA2Z22
Subtask 36-22-16-010-060-B 4. Procedure
Subtask 36-22-16-220-051-A
A. Inspection of the Overheat Sensing Elements
   (1) Make sure that the clearance between the sensing elements and the duct is a minimum of 12.7 mm (0.50 in.), measured along the full length of the sensing element.
   (2) Do an inspection of the elements to make sure that they are installed out of the insulation.
   (3) Make sure that the clearance between the elements and the duct insulation is the same as at the mounting brackets.
   (4) Make sure that the sensing elements are installed with the permitted tolerance.
   (5) Make sure that each clamp has a silicon rubber grommet.
   (6) Make sure that each mounting bracket, installed directly on the duct, has a spacer.
   (7) Make sure that the elements are installed correctly.
   (8) Make sure that each mounting clamp is in the correct condition and has no corrosion.
   (9) Make sure that the bonding straps are correctly installed (Ref. AMM TASK 20-28-00-912-802).
   (10) Make sure that the lockwires are correctly installed on the connections of the sensing elements.
   (11) Make sure that the duct insulation is in the correct condition and correctly installed.
   (12) Make sure that the sensing elements have no cracks, nicks, sharp edges, bonds chafing or corrosion.
5. Close-up
Subtask 36-22-16-410-061-B Subtask 36-22-16-865-085-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
49VUAIR BLEED/ENG 2/MONG3HA2D12
49VUAIR BLEED/ENG 1/CTL2HA1D11
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
122VUAIR BLEED/ENG 1/MONG3HA1Z23
122VUAIR BLEED/ENG 2/CTL2HA2Z22
Subtask 36-22-16-860-085-A
C. Aircraft Maintenance Configuration
   (1) Retract the slats fully (Ref. AMM TASK 27-80-00-866-005).
Subtask 36-22-16-942-060-A
D. Removal of Equipment
   (1) Remove the safety barriers.
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the access platform(s).
   (4) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
[Rev.10 from 2021] 2026.04.01 01:17:19 UTC