W DOC AIRBUS | AMM A320F

Removal of the Overheat Sensing Elements


TASK 36-22-16-000-001-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.
ZONE: 190
ZONE: 500
ZONE: 600
FIN: 29HF
FIN: 45HF
FIN: 56HF
FIN: 72HF
FIN: 80HF
FIN: 81HF
FIN: 82HF
FIN: 83HF
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)- ADJUSTABLE
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
190
BELLY FAIR, AIR CONDITIONING & HYD COMPT
500
LEFT WING
600
RIGHT WING
FOR [29HF] (SNSG ELEM-OVHT, L WING LOOP A)
191BB, 191BT, 191CT, 191EB, 521AB, 521BB, 521CB
FOR [45HF] (SNSG ELEM-OVHT, R WING LOOP A)
191BB, 192BT, 192CT, 192EB, 621AB, 621BB, 621CB
FOR [56HF] (SNSG ELEM-OVHT, L WING LOOP B)
191BB, 191CT, 191EB, 521AB, 521BB, 521CB
FOR [72HF] (SNSG ELEM-OVHT, R WING LOOP B)
191BB, 192CT, 192EB, 621AB, 621BB, 621CB
FOR [80HF] (SNSG ELEM-OVHT, R WING LOOP A)
192CT, 192EB, 621AB, 621BB, 621CB
FOR [81HF] (SNSG ELEM-OVHT, L WING LOOP A)
191CT, 191EB, 521AB, 521BB, 521CB
FOR [82HF] (SNSG ELEM-OVHT, R WING LOOP B)
192BT, 192CT, 192EB, 621AB, 621BB, 621CB
FOR [83HF] (SNSG ELEM-OVHT, L WING LOOP B)
191BT, 191CT, 191EB, 521AB, 521BB, 521CB
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 27-80-00-866-004-A
Extending the Slats on the Ground
TASK 36-22-16-000-002-A
Removal of the Cables
TASK 53-35-11-000-001-A
Removal 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 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 36-22-16-941-050-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 36-22-16-860-057-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 36-22-16-865-050-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 36-22-16-010-050-A
D. Get Access
   (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the applicable access panels.
   (2) Remove the applicable access panels, (Ref. AMM TASK 53-35-13-000-002), (Ref. AMM TASK 53-35-11-000-001), (Ref. AMM TASK 57-41-37-000-004), (Ref. AMM TASK 57-41-37-000-005):
     (a) FOR [56HF] (SNSG ELEM-OVHT, L WING LOOP B)
     (b) FOR [81HF] (SNSG ELEM-OVHT, L WING LOOP A)
     (c) FOR [72HF] (SNSG ELEM-OVHT, R WING LOOP B)
     (d) FOR [80HF] (SNSG ELEM-OVHT, R WING LOOP A)
     (e) FOR [29HF] (SNSG ELEM-OVHT, L WING LOOP A)
     (f) FOR [83HF] (SNSG ELEM-OVHT, L WING LOOP B)
     (g) FOR [45HF] (SNSG ELEM-OVHT, R WING LOOP A)
     (h) FOR [82HF] (SNSG ELEM-OVHT, R WING LOOP B)
4. Procedure
Subtask 36-22-16-020-050-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) Remove the sensing elements 29HF(45HF) (1) and 56HF(72HF) (8):
     (a) Release the quick-release fasteners (27) and open the clamps (25). Retain the protective sleeves (26).
     (b) Remove and discard the lockwire from the connectors (19) and (22) and the nut (20).
     (c) Disconnect the connector (19) from the connector (22).
     (d) Remove the nut (20) from the connector (22).
     (e) Remove the connector (22) from the flanged attachment (21).
     (f) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
     (g) Remove a sufficient amount of the cables 21HF(37HF) (40) and 77HF(64HF) (44) (Ref. AMM TASK 36-22-16-000-002) to let you remove the overheat sensing element 56HF(72HF) (8).
   (2) Remove the sensing elements 83HF(82HF) (2) and 81HF(80HF) (7):
     (a) Release the quick-release fasteners (27) and open the clamps (25). Retain the protective sleeves (26).
     (b) Remove and discard the lockwire from the connectors (19), (22), (23) and (24), and the nuts (20).
     (c) Disconnect the connectors (19) and (24) from the connectors (22) and (23).
     (d) Remove the nut (20) from the connectors (22) and (23).
     (e) Remove the connectors (22) and (23) from the flanged attachment (21).
     (f) Put the CAP-BLANKING on each disconnected electrical connector and receptacle.
     (g) Remove a sufficient amount of the cables 21HF(37HF) (40) and 77HF(64HF) (44) (Ref. AMM TASK 36-22-16-000-002) to let you remove the overheat sensing element 81HF(80HF) (7).
   (3) Remove the applicable overheat sensing element (1), (2), (7) or (8).
[Rev.10 from 2021] 2026.04.01 01:17:01 UTC