W DOC AIRBUS | AMM A320F

Removal of the Overheat Sensing Elements


TASK 36-22-16-000-006-A
Removal of the 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.
ZONE: 500
ZONE: 600
FIN: 22HF
FIN: 28HF
FIN: 38HF
FIN: 44HF
FIN: 49HF
FIN: 55HF
FIN: 65HF
FIN: 71HF
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 3M (10 FT)
No specific
AR
CAP - BLANKING
No specific
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
500
LEFT WING
600
RIGHT WING
FOR [22HF] (SNSG ELEM-OVHT, L WING LOOP A)
FOR [28HF] (SNSG ELEM-OVHT, L WING LOOP A)
FOR [49HF] (SNSG ELEM-OVHT, L WING LOOP B)
FOR [55HF] (SNSG ELEM-OVHT, L WING LOOP B)
521AB, 521BB, 521BT, 521CB, 521EB, 521GB
FOR [38HF] (SNSG ELEM-OVHT, R WING LOOP A)
FOR [44HF] (SNSG ELEM-OVHT, R WING LOOP A)
FOR [65HF] (SNSG ELEM-OVHT, R WING LOOP B)
FOR [71HF] (SNSG ELEM-OVHT, R WING LOOP B)
621AB, 621BB, 621BT, 621CB, 621EB, 621GB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 27-80-00-866-004-A
Extending the Slats on the Ground
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
3. Job Set-up
Subtask 36-22-16-941-055-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.
Subtask 36-22-16-860-062-A
B. Aircraft Maintenance Configuration
   (1) Extend the slats fully (Ref. AMM TASK 27-80-00-866-004).
   (2) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the flap/slat control lever on panel 114VU.
Subtask 36-22-16-865-055-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 1/CTL3HA1D12
49VUAIR BLEED/ENG 1/MONG2HA1D11
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUAIR BLEED/ENG 2/MONG3HA2D12
49VUAIR BLEED/ENG 1/CTL2HA1D11
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 2/CTL3HA2Z23
122VUAIR BLEED/ENG 2/MONG2HA2Z22
** ON A/C NOT FOR ALL
122VUAIR BLEED/ENG 1/MONG3HA1Z23
122VUAIR BLEED/ENG 2/CTL2HA2Z22
Subtask 36-22-16-010-055-A
D. Get Access
   (1) Put an ACCESS PLATFORM 3M (10 FT) in position below the applicable access panel.
   (2) Remove the applicable access panels (Ref. AMM TASK 57-41-37-000-004) (Ref. AMM TASK 57-41-37-000-005):
     (a) FOR [28HF] (SNSG ELEM-OVHT, L WING LOOP A), [49HF] (SNSG ELEM-OVHT, L WING LOOP B), [22HF] (SNSG ELEM-OVHT, L WING LOOP A), [55HF] (SNSG ELEM-OVHT, L WING LOOP B)
remove 521AB 521BB 521CB 521EB 521GB 521BT
     (b) FOR [44HF] (SNSG ELEM-OVHT, R WING LOOP A), [65HF] (SNSG ELEM-OVHT, R WING LOOP B), [38HF] (SNSG ELEM-OVHT, R WING LOOP A), [71HF] (SNSG ELEM-OVHT, R WING LOOP B)
remove 621AB 621BB 621CB 621EB 621GB 621BT.
4. Procedure
Subtask 36-22-16-020-055-A
A. Removal of the Overheat Sensing Elements
WARNING: USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
CAUTION: REMOVE OR INSTALL THE SENSING ELEMENTS CAREFULLY. DO NOT TWIST, BEND OR CAUSE KINKS IN THE SENSING ELEMENTS. IF YOU DO, YOU CAN CAUSE DAMAGE TO THEM.
   (1) Release the quick-release fasteners (27) and open the clamps (25). Retain the protective sleeves (26).
   (2) Remove the nut (35) and the bolt (33) from the fairlead (34). Retain the removable part of the fairlead (34) and the protective sleeves (26).
   (3) Remove and discard the lockwire from the connectors (19) and (22) and the nut (20).
   (4) Disconnect the connector (19) from the connector (22).
   (5) Remove the nut (20) from the connector (22) and remove the connector (22) from the flanged attachment (21).
   (6) Put CAP - BLANKING on all the disconnected connectors.
   (7) Remove the applicable overheat sensing element (5), (6), (7) or (8) and retain the applicable grommets (36).
[Rev.10 from 2021] 2026.04.01 01:17:14 UTC