W DOC AIRBUS | AMM A320F

Detailed Visual Inspection of the Door Locking Mechanism


TASK 52-11-21-220-001-A
Detailed Visual Inspection of the Door Locking Mechanism


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 4M (13 FT)-ADJUSTABLE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
831, 841
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
TASK 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
TASK 52-10-00-010-001-A
Opening of the Passenger/Crew Door
TASK 52-10-00-410-001-A
Closing of the Passenger/Crew Door
TASK 52-10-00-860-001-A
Special Precautions before Work on the Passenger/Crew Door
TASK 52-10-00-860-002-A
Special Precautions after Work on the Passenger/Crew Door
TASK 52-10-00-915-001-A
Replacement of the Bonded Bushes (with Seal Bead)
TASK 52-11-21-000-001-A
Removal of the Door Locking Mechanism
TASK 52-11-21-400-001-A
Installation of the Door Locking Mechanism
3. Job Set-up
Subtask 52-11-21-861-050-A
A. Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001)
Subtask 52-11-21-010-062-A
B. Get Access
WARNING: BEFORE YOU START WORK ON THE DOOR, MAKE SURE THAT:
  • THE EMERGENCY CONTROL HANDLE IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
  • THE PERCUSSION LEVER OF THE DOOR-DAMPER AND EMERGENCY-OPERATION CYLINDER IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
IF YOU DO NOT OBEY THESE INSTRUCTIONS, THE DOOR CAN OPEN WITH FORCE OR THE ESCAPE SLIDE CAN DEPLOY SUDDENLY. THIS CAN CAUSE INJURY AND/OR DAMAGE.
WARNING: DO NOT OPEN THE PASSENGER/CREW DOOR IF THE WIND SPEED IS MORE THAN 65 KNOTS.
WARNING: STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT FLASHES. IF THE RED WARNING LIGHT FLASHES, REMAINING PRESSURE CAN CAUSE THE DOOR TO OPEN SUDDENLY AND CAN:
  • KILL OR CAUSE SERIOUS INJURY TO PERSONS
  • CAUSE DAMAGE TO THE AIRCRAFT.
   (1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position at the applicable FWD passenger/crew door 831 or 841.
   (2) Open the applicable FWD passenger/crew door 831 or 841 (Ref. AMM TASK 52-10-00-010-001).
   (3) Obey the special precautions before you start work on the door (Ref. AMM TASK 52-10-00-860-001)
Subtask 52-11-21-865-060-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUEIS/SLIDES/ARM AND WARN/FLT15WNP11
121VUEIS/SLIDES/ARM AND WARN/GND13WNP10
121VUEIS/SDAC1 AND 2/DOOR/DET/PAX48WVP05
Subtask 52-11-21-020-061-A
D. Removal of the Door Locking Mechanism
(Ref. AMM TASK 52-11-21-000-001)
   (1) Remove the lowering shaft, if not removed.
   (2) Remove the inner control handle, the outer control handle and the gearbox, if not removed.
   (3) Remove the reducer shaft mechanism, if not removed.
   (4) Remove the upper and lower connection links, if not removed.
   (5) Remove the compensation mechanism, if not removed.
   (6) Remove the locking shaft mechanism, if not removed.
   (7) Remove the safety pin and the locking hook, if not removed.
4. Procedure
Subtask 52-11-21-220-052-A
A. Inspection of the Lowering Shaft
   (1) Do a detailed visual inspection of the bushes, the bearing and the parts of the lowering shaft.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
DD
10.966
10.980


10.949


OD 1
(0.4317)
(0.4323)


(0.4311)





0.0200
0.1420


0.1030



(0.0008)
(0.0056)


(0.0041)
DD
11.000
11.108



11.052

ID 2
(0.4331)
(0.4373)



(0.4351)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the bearing (3) is worn or unserviceable:
     (a) Replace the flange bearing assy.
Subtask 52-11-21-220-060-A
B. Inspection of the Lowering Shaft
   (1) Do a detailed visual inspection of the bushes, the bearing and the parts of the lowering shaft.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
EE
6.344
6.353


6.332


OD 4
(0.2498)
(0.2501)


(0.2493)





0.0050
0.0360


0.0720



(0.0002)
(0.0014)


(0.0028)
EE
6.358
6.380



6.404

ID 5
(0.2503)
(0.2512)



(0.2521)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the bearing (3) is worn or unserviceable:
     (a) Replace the flange bearing assy.
Subtask 52-11-21-220-053-A
C. Inspection of the Inner and Outer Contol Handles and Gearbox
   (1) Do a detailed visual inspection of the bushes, the link assemblies (at rod level) and the parts of the inner and outer control handles and the geabox.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
DD
6.344
6.353


6.332


OD 11
(0.2498)
(0.2501)


(0.2493)





0.0050
0.0360


0.0720



(0.0002)
(0.0014)


(0.0028)
DD
6.358
6.380



6.404

ID 12
(0.2503)
(0.2512)



(0.2521)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the link assembly (13) is worn or unserviceable:
     (a) Replace the rod end of the link assembly (13).
Subtask 52-11-21-220-054-A
D. Inspection of the Reducer Shaft Mechanism
   (1) Do a detailed visual inspection of the link assemblies (at rod level) and the parts of the reducer shaft mechanism.
   (2) If the link assemblies (22) and (23) are worn or unserviceable:
     (a) Replace the rod end of the link assemblies (22) and (23).
   (3) If the bearing (21) is worn or unserviceable:
     (a) Replace the flange bearing assy.
Subtask 52-11-21-220-055-A
E. Inspection of the Upper and Lower Connection Links
   (1) Do a detailed visual inspection of the bushes, the connection links (at rod level) and the parts of the upper and lower connection links.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
BB
15.882
15.893


15.870


OD 31
(0.6253)
(0.6257)


(0.6248)





0.0000
0.0360


0.0720



(0.0000)
(0.0014)


(0.0028)
BB
15.893
15.918



15.942

ID 30
(0.6257)
(0.6267)



(0.6276)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the connection links (34) and (35) are worn or unserviceable:
     (a) Replace the rod end of the connection links (34) and (35).
Subtask 52-11-21-220-061-A
F. Inspection of the Upper and Lower Connection Links
   (1) Do a detailed visual inspection of the bushes, the connection links (at rod level) and the parts of the upper and lower connection links.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
CC
15.882
15.893


15.870


OD 33
(0.6253)
(0.6257)


(0.6248)





0.0000
0.0360


0.0720



(0.0000)
(0.0014)


(0.0028)
CC
15.893
15.918



15.942

ID 32
(0.6257)
(0.6267)



(0.6276)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the connection links (34) and (35) are worn or unserviceable:
     (a) Replace the rod end of the connection links (34) and (35).
Subtask 52-11-21-220-062-A
G. Inspection of the Upper and Lower Connection Links
   (1) Do a detailed visual inspection of the bushes, the connection links (at rod level) and the parts of the upper and lower connection links.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
BB
12.704
12.715


12.691


OD 37
(0.5002)
(0.5006)


(0.4996)





0.0000
0.0370


0.0740



(0.0000)
(0.0015)


(0.0029)
BB
12.715
12.741



12.765

ID 36
(0.5006)
(0.5016)



(0.5026)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the connection links (34) and (35) are worn or unserviceable:
     (a) Replace the rod end of the connection links (34) and (35).
Subtask 52-11-21-220-063-A
H. Inspection of the Upper and Lower Connection Links
   (1) Do a detailed visual inspection of the bushes, the connection links (at rod level) and the parts of the upper and lower connection links.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
CC
12.704
12.715


12.691


OD 39
(0.5002)
(0.5006)


(0.4996)





0.0000
0.0370


0.0740



(0.0000)
(0.0015)


(0.0029)
CC
12.715
12.741



12.765

ID 38
(0.5006)
(0.5016)



(0.5026)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the connection links (34) and (35) are worn or unserviceable:
     (a) Replace the rod end of the connection links (34) and (35).
Subtask 52-11-21-220-056-A
I. Inspection of the Compensation Mechanism
   (1) Do a detailed visual inspection of the bushes, the link assemblies (at rod level) and the parts of the compensation mechanism.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
B
22.235
22.248


22.220


OD 41
(0.8754)
(0.8759)


(0.8748)





0.0000
0.0430


0.0860



(0.0000)
(0.0017)


(0.0034)
B
22.248
22.278



22.306

ID 40
(0.8759)
(0.8771)



(0.8782)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the link assembly (46) is worn or unserviceable:
     (a) Replace the rod end of the link assembly (46).
Subtask 52-11-21-220-064-A
J. Inspection of the Compensation Mechanism
   (1) Do a detailed visual inspection of the bushes, the link assemblies (at rod level) and the parts of the compensation mechanism.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
B
34.842
34.958


34.923


OD 42
(1.3717)
(1.3763)


(1.3749)





0.0000
0.1570


0.1140



(0.0000)
(0.0062)


(0.0045)
B
34.958
34.999



35.037

ID 40
(1.3763)
(1.3779)



(1.3794)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the link assembly (46) is worn or unserviceable:
     (a) Replace the rod end of the link assembly (46).
Subtask 52-11-21-220-065-A
K. Inspection of the Compensation Mechanism
   (1) Do a detailed visual inspection of the bushes, the link assemblies (at rod level) and the parts of the compensation mechanism.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
B
22.235
22.248


22.220


OD 44
(0.8754)
(0.8759)


(0.8748)





0.0000
0.0430


0.0860



(0.0000)
(0.0017)


(0.0034)
B
22.248
22.278



22.306

ID 43
(0.8759)
(0.8771)



(0.8782)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the link assembly (46) is worn or unserviceable:
     (a) Replace the rod end of the link assembly (46).
Subtask 52-11-21-220-066-A
L. Inspection of the Compensation Mechanism
   (1) Do a detailed visual inspection of the bushes, the link assemblies (at rod level) and the parts of the compensation mechanism.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
B
28.959
28.980


28.938


OD 44
(1.1401)
(1.1409)


(1.1393)





0.0200
0.0620


0.1240



(0.0008)
(0.0024)


(0.0049)
B
29.000
29.021



29.062

ID 45
(1.1417)
(1.1426)



(1.1442)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the link assembly (46) is worn or unserviceable:
     (a) Replace the rod end of the link assembly (46).
Subtask 52-11-21-220-057-A
M. Inspection of the Locking Shaft Mechanism
   (1) Do a detailed visual inspection of the bushes, the bearing, the link assemblies (at rod level) and the parts of the locking shaft mechanism.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
CC
28.595
28.608


28.577


OD 52
(1.1258)
(1.1263)


(1.1251)





0.0000
0.0540


0.2910



(0.0000)
(0.0021)


(0.0115)
CC
28.608
28.649



28.868

ID 51
(1.1263)
(1.1279)



(1.1365)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the link assemblies (53), (54), (55) and (59) are worn or unserviceable:
     (a) Replace the rod end of the link assemblies (53), (54), (55) and (59).
   (5) If the bearing (58) is worn or unserviceable:
     (a) Replace the flange bearing assy.
Subtask 52-11-21-220-067-A
N. Inspection of the Locking Shaft Mechanism
   (1) Do a detailed visual inspection of the bushes, the bearing, the link assemblies (at rod level) and the parts of the locking shaft mechanism.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
CC
25.411
25.420


25.396


OD 57
(1.0004)
(1.0008)


(0.9998)





0.0050
0.0450


0.0900



(0.0002)
(0.0018)


(0.0035)
CC
25.425
25.456



25.486

ID 56
(1.0010)
(1.0022)



(1.0034)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the link assemblies (53), (54), (55) and (59) are worn or unserviceable:
     (a) Replace the rod end of the link assemblies (53), (54), (55) and (59).
   (5) If the bearing (58) is worn or unserviceable:
     (a) Replace the flange bearing assy.
Subtask 52-11-21-220-068-A
O. Inspection of the Locking Shaft Mechanism
   (1) Do a detailed visual inspection of the bushes, the bearing, the link assemblies (at rod level) and the parts of the locking shaft mechanism.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
CC
7.941
7.950


7.930


OD 61
(0.3126)
(0.3130)


(0.3122)





0.0000
0.0320


0.0640



(0.0000)
(0.0013)


(0.0025)
CC
7.950
7.973



7.994

ID 60
(0.3130)
(0.3139)



(0.3147)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the link assemblies (53), (54), (55) and (59) are worn or unserviceable:
     (a) Replace the rod end of the link assemblies (53), (54), (55) and (59).
   (5) If the bearing (58) is worn or unserviceable:
     (a) Replace the flange bearing assy.
Subtask 52-11-21-220-069-A
P. Inspection of the Locking Shaft Mechanism
   (1) Do a detailed visual inspection of the bushes, the bearing, the link assemblies (at rod level) and the parts of the locking shaft mechanism.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
CC
7.941
7.950


7.930


OD 63
(0.3126)
(0.3130)


(0.3122)





0.0000
0.0320


0.0640



(0.0000)
(0.0013)


(0.0025)
CC
7.950
7.973



7.994

ID 62
(0.3130)
(0.3139)



(0.3147)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the link assemblies (53), (54), (55) and (59) are worn or unserviceable:
     (a) Replace the rod end of the link assemblies (53), (54), (55) and (59).
   (5) If the bearing (58) is worn or unserviceable:
     (a) Replace the flange bearing assy.
Subtask 52-11-21-220-070-A
Q. Inspection of the Locking Shaft Mechanism
   (1) Do a detailed visual inspection of the bushes, the bearing, the link assemblies (at rod level) and the parts of the locking shaft mechanism.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
CC
28.595
28.608


28.577


OD 64
(1.1258)
(1.1263)


(1.1251)





0.0000
0.0540


0.2910



(0.0000)
(0.0021)


(0.0115)
CC
28.608
28.649



28.868

ID 65
(1.1263)
(1.1279)



(1.1365)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the link assemblies (53), (54), (55) and (59) are worn or unserviceable:
     (a) Replace the rod end of the link assemblies (53), (54), (55) and (59).
   (5) If the bearing (58) is worn or unserviceable:
     (a) Replace the flange bearing assy.
Subtask 52-11-21-220-058-A
R. Inspection of the Locking Hook and Safety Pin
   (1) Do a detailed visual inspection of the bushes, the link assemblies (at rod level) and the parts of the locking hook and safety pin.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
CC
14.183
14.194


14.182


OD 71
(0.5584)
(0.5588)


(0.5583)





0.0060
0.0350


0.0600



(0.0002)
(0.0014)


(0.0024)
CC
14.200
14.218



14.242

ID 70
(0.5591)
(0.5598)



(0.5607)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the link assemblies (72) and (76) are worn or unserviceable:
     (a) Replace the rod end of the link assemblies (72) and (76).
Subtask 52-11-21-220-071-A
S. Inspection of the Locking Hook and Safety Pin
   (1) Do a detailed visual inspection of the bushes, the link assemblies (at rod level) and the parts of the locking hook and safety pin.
   (2) Make sure that the dimensions are correct.
FIG. DETAIL AND ITEM N°
ORIGINAL MANUFACTURING LIMITS
IN-SERVICE WEAR LIMITS
GG
19.053
19.064


19.041


OD 73
(0.7501)
(0.7506)


(0.7496)





0.0060
0.0480


0.0840



(0.0002)
(0.0019)


(0.0033)
GG
19.070
19.101



19.125

ID 75
(0.7508)
(0.7520)



(0.7530)

   (3) If the wear of the bushes is not in the tolerances:
     (a) Replace the bushes (Ref. AMM TASK 52-10-00-915-001).
     (b) Or replace the parts on which they are installed.
   (4) If the link assemblies (72) and (76) are worn or unserviceable:
     (a) Replace the rod end of the link assemblies (72) and (76).
5. Close-up
Subtask 52-11-21-420-061-A
A. Installation of the Door Locking Mechanism
(Ref. AMM TASK 52-11-21-400-001)
   (1) Install the lowering shaft.
   (2) Install the inner control handle, the outer control handle and the gearbox.
   (3) Install the reducer shaft mechanism.
   (4) Install the upper and lower connection links.
   (5) Install the compensation mechanism.
   (6) Install the locking shaft mechanism.
   (7) Install the safety pin and locking hook.
Subtask 52-11-21-865-061-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUEIS/SLIDES/ARM AND WARN/FLT15WNP11
121VUEIS/SLIDES/ARM AND WARN/GND13WNP10
121VUEIS/SDAC1 AND 2/DOOR/DET/PAX48WVP05
Subtask 52-11-21-410-062-A
C. Close Access
   (1) Obey the special precautions after the work on the door (Ref. AMM TASK 52-10-00-860-002).
   (2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
   (3) Make sure that the work area is clean and clear of tools and other items.
   (4) Close the FWD passenger/crew door 831 or 841 (Ref. AMM TASK 52-10-00-410-001).
   (5) Remove the access platform(s).
Subtask 52-11-21-862-050-A
D. De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001)
[Rev.10 from 2021] 2026.04.02 06:27:24 UTC