W DOC AIRBUS | AMM A320F

Adjustment of the Locking Hooks

TASK 52-22-00-820-803-A
Adjustment of the Locking Hooks

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.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
NOTE: Two persons are necessary for this procedure.
1. Reason for the Job
To adjust the locking hooks of the overwing emergency-exit doors immediately after you have replaced the doors or if there is a door malfunction.
NOTE: The values given in this procedure are not applicable to the general inspection/check.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE
No specific
1
CALIPER
No specific
1
GAGE - FEELER
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
1
WARNING NOTICE(S)
No specific
Torque wrench: range to between 1.38 and 1.06 m.daN (122.12 and 93.81 lbf.in ) T
98D27803000000
1
LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.04SAB2)
Varnish Polyurethane-- Marking Structure
(Material No.06AAC1)
Polysulfide Sealant-General Purpose Interfay -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
833, 834, 843, 844
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 12-00-00-481-002-A
Installation of the Wingrip
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 25-23-47-000-803-A
Removal of the Door Lining from the Overwing Emergency Exit
TASK 25-23-47-400-803-A
Installation of the Door Lining on the Overwing Emergency Exit
TASK 25-62-00-081-001-A
Special Precautions after Work on the Offwing Escape-Slide Systems
TASK 25-62-00-481-001-A
Special Precautions before Work on the Offwing Escape-Slide Systems
TASK 25-80-00-000-001-A
Removal of the Insulation Blankets
TASK 25-80-00-400-001-A
Installation of the Insulation Blankets
TASK 27-00-00-080-002-A
Removal of the Flap/Slat Control-Lever Locking Tool (98D27803000000)
TASK 27-00-00-480-002-A
Installation of the Flap/Slat Control-Lever Locking Tool (98D27803000000)
TASK 52-22-00-410-802-A
Closing of the Overwing Emergency-Exit Door from the Passenger Compartment
F Adjustment of the Locking Hooks
3. Job Set-up
Subtask 52-22-00-860-115-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (2) Install the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION on the flap/slat control lever (Ref. AMM TASK 27-00-00-480-002).
   (3) Do the special precaution before you work on the offwing escape-slide system (Ref. AMM TASK 25-62-00-481-001).
   (4) In the cockpit, put the WARNING NOTICE(S) in position to tell persons not to operate the flight controls.
Subtask 52-22-00-865-073-A ** ON A/C NOT FOR ALL
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB02
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
105VUFLT CTL/SEC1/STBY SPLY22CEB01
121VUEIS/SLIDES/ARM AND WARN/FLT15WNP11
121VUEIS/SLIDES/ARM AND WARN/GND13WNP10
121VUEIS/SDAC1 AND 2/DOOR/DET/PAX48WVP05
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
122VUFLIGHT LOCK OWD40WNU16
Subtask 52-22-00-010-089-A ** ON A/C NOT FOR ALL
C. Get Access
F Adjustment of the Locking Hooks ** ON A/C NOT FOR ALL
   (1) Remove the lining of overwing emergency-exit door 833 ( 843) or 834 ( 844) (Ref. AMM TASK 25-23-47-000-803).
   (2) Remove cover 241ADW(242ADW) or 241AEW(242AEW) (3) (Ref. AMM TASK 25-23-47-000-803).
   (3) Make sure that overwing emergency-exit door 833 ( 843) or 834 ( 844) is closed (Ref. AMM TASK 52-22-00-410-802).
   (4) Remove the applicable insulation (Ref. AMM TASK 25-80-00-000-001).
   (5) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position near overwing emergency-exit door 833 ( 843) or 834 ( 844).
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.
   (6) Put on a safety harness:
  • On the THS or in the rear fuselage
  • On top of the wings or pylons.
     (a) Install the individual pad system (Ref. AMM TASK 12-00-00-481-002).
     (b) Put on and attach a safety harness before you start work in the work area.
4. Procedure
Subtask 52-22-00-820-069-A ** ON A/C NOT FOR ALL
A. Adjustment of the Hooks
NOTE: The most FWD and most AFT hooks (1) must touch the rear of the rollers (2). The clearance A between the middle hooks and the rear of the rollers is 0 -0 mm or +0.25 mm (0.0000 +0.0000 in. or +0.0098 in.).
   (1) Measure clearances A, B and C with CALIPER and GAGE - FEELER:
  • Clearance A must be 0 -0 mm or +0.25 mm (0.0000 +0.0000 in. or +0.0098 in.)
  • Clearances B and C must be 2 mm (0.0787 in.) minimum.
   (2) Measure skin offset S4 and make sure that its value is 0.4 -0.8 mm or +0.8 mm (0.0157 -0.0315 in. or +0.0315 in.).
   (3) If the value of skin offset S4 is different, do the steps that follow:
     (a) Record the delta value of the new measurement (measured between the necessary value and the new value).
     (b) Make sure that:
  • One person holds the emergency-exit door in the closed position.
  • The second person sets the latch handle to the DOOR OPEN position.
     (c) Unlock the door.
     (d) Loosen the bolts (4) and the nuts (6).
     (e) Remove the Varnish Polyurethane-- Marking Structure (Material No.04SAB2) from the heads of the bolts (4) and the nuts (6).
     (f) Remove the layer of Polysulfide Sealant-General Purpose Interfay - (Material No.06AAC1) from the edge of the hook (1) and the plate (5).
     (g) Adjust the locking hook in the Y direction with the delta value of the measurement.
   (4) Adjust the hook (1) until it aligns with the notch of the plate (5).
NOTE: The adjustment space between the position of the plate (5) and the structure (7) is 1 mm (0.04 in.).
NOTE: The adjustment space between the position of the hook (1) and the plate (5) is 0.75 mm (0.03 in.).
   (5) Install the bolts (4) and the nuts (6).
   (6) TORQUE the bolts (4) and the nuts (6) to between 1.38 and 1.06 m.daN (122.12 and 93.81 lbf.in ) T.
   (7) Apply Varnish Polyurethane-- Marking Structure (Material No.04SAB2) to the heads of the bolts (4) and the nuts (6).
   (8) Apply a layer of Polysulfide Sealant-General Purpose Interfay - (Material No.06AAC1) around the edge of the hook (1) and the plate (5).
   (9) Close and lock the door:
  • One person holds the emergency-exit door in the closed position.
  • The second person sets the latch handle to the DOOR CLOSED position.
   (10) Measure clearances A, B and C again and make sure that they are correct.
   (11) Measure skin offset S4 again and make sure that its value is correct.
5. Close-up
Subtask 52-22-00-410-078-A ** ON A/C NOT FOR ALL
A. Close Access
F Adjustment of the Locking Hooks ** ON A/C NOT FOR ALL
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the access platform(s).
   (3) Make sure that overwing emergency-exit door 833 ( 843) or 834 ( 844) is closed (Ref. AMM TASK 52-22-00-410-802).
   (4) Install the removed insulation (Ref. AMM TASK 25-80-00-400-001).
   (5) Close overwing emergency-exit door 833 ( 843) or 834 ( 844) (Ref. AMM TASK 52-22-00-410-802).
   (6) Install cover 241ADW(242ADW) or 241AEW(242AEW) (3) (Ref. AMM TASK 25-23-47-400-803).
   (7) Install the lining of overwing emergency-exit door 833 ( 843) or 834 ( 844) (Ref. AMM TASK 25-23-47-400-803).
Subtask 52-22-00-865-074-A ** ON A/C NOT FOR ALL
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SEC1/NORM/SPLY21CE1B03
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB02
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
105VUFLT CTL/SEC1/STBY SPLY22CEB01
121VUEIS/SLIDES/ARM AND WARN/FLT15WNP11
121VUEIS/SLIDES/ARM AND WARN/GND13WNP10
121VUEIS/SDAC1 AND 2/DOOR/DET/PAX48WVP05
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
121VUFLIGHT CONTROLS/SEC3/SPLY21CE3Q19
121VUFLIGHT CONTROLS/SEC2/SPLY21CE2Q18
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
122VUFLIGHT LOCK OWD40WNU16
Subtask 52-22-00-860-116-A ** ON A/C NOT FOR ALL
C. Aircraft Maintenance Configuration
   (1) Remove the WARNING NOTICE(S).
   (2) Do the special precaution after you work on the offwing escape-slide system (Ref. AMM TASK 25-62-00-081-001).
   (3) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the flap/slat control lever (Ref. AMM TASK 27-00-00-080-002).
   (4) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
[Rev.10 from 2021] 2026.04.02 06:27:38 UTC
"WTRUIB" 2025