DOC AIRBUS | AMM A320FAdjustment of the Emergency Exit Door
TASK 52-22-00-820-002-A
Adjustment of the Emergency Exit Door
1. Reason for the Job
To adjust the emergency exit doors immediately after replacement of the door/door components, or if a door malfunction is reported.
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Expendable Parts
D. Referenced Information
3. Job Set-up
Subtask 52-22-00-010-062-A ** ON A/C NOT FOR ALL
Subtask 52-22-00-820-050-A ** ON A/C NOT FOR ALL
Subtask 52-22-00-410-057-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.02 06:43:18 UTC
Adjustment of the Emergency Exit Door
1. Reason for the Job
To adjust the emergency exit doors immediately after replacement of the door/door components, or if a door malfunction is reported.
NOTE: The values given in this procedure are not applicable for the general inspection/checks
2. Job Set-up InformationA. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | TAPE - SELF-AMALGAMATING |
| No specific | Torque wrench: range to between 2.2 and 2.0 m.daN (16.22 and 14.75 lbf.ft )  | |
| 98D52207557000 | 1 | BALLAST WEIGHT - EMERGENCY EXIT |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 833 | EMERGENCY EXITS |
| 834 | EMERGENCY EXITS |
| 835 | MID PASSENGER/CREW DOOR |
| 843 | EMERGENCY EXITS |
| 844 | EMERGENCY EXITS |
| 845 | MID PASSENGER/CREW DOOR |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 12 | COTTER PIN | AIPC 52-22-02-04-330 |
| 50 | COTTER PIN | AIPC 52-22-04-06-070 |
| 60 | COTTER PIN | AIPC 52-22-04-06-070 |
| 32 | LOCK PLATES | AIPC 52-22-31-02-040 |
| 12 | COTTER PIN | AIPC 52-22-84-20-180 |
| 50 | COTTER PIN | AIPC 52-22-84-30-060 |
| 60 | COTTER PIN | AIPC 52-22-84-30-060 |
| 32 | LOCK PLATES | AIPC 52-22-84-80-040 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 25-23-47-000-004-A | Removal of the Door Frame Linings of the LH FWD Emergency Exit Door, zone 231 |
| TASK 25-23-47-000-010-A | Removal of the Door Frame Linings of the Left/Right Aft Emergency Exit Doors from Zones 251/252 |
| TASK 25-23-47-000-012-A | Removal of the Door Linings of the LH FWD Emergency Exit Door, zone 231 |
| TASK 25-23-47-000-013-A | Removal of the Door Linings of the RH FWD Emergency Exit Door at zone 251 or RH AFT at zone 252 or LH AFT at zone 232. |
| TASK 25-23-47-400-004-A | Installation of the Door Frame Linings of the LH FWD Emergency Exit Door, zone 231 |
| TASK 25-23-47-400-009-A | Installation of the Door Frame Linings of the Right Forward Emergency Exit Door in Zone 232 |
| TASK 25-23-47-400-010-A | Installation of the Door Frame Linings of the Left/Right Aft Emergency Exit Doors in Zones 251/252 |
| TASK 25-23-47-400-012-A | Installation of the Door Linings of the LH FWD Emergency Exit Door, zone 231 |
| TASK 25-23-47-400-013-A | Installation of the Door Linings of the RH FWD Emergency Exit Door at zone 251, or RH AFT at zone 252, or LH AFT at zone 232. |
| TASK 52-22-00-010-001-A | Opening of the Emergency Exit Doors from the Passenger Compartment |
| TASK 52-22-00-410-001-A | Closing of the Emergency Exit Doors from the Passenger Compartment |
| TASK 52-22-00-820-005-A | Adjustment of the Balance Mechanism |
| TASK 52-22-00-860-003-A | Special Precaution before Maintenance on the Door Damper and Emergency Operation Cylinder |
| TASK 52-22-00-860-004-A | Special Precaution after Maintenance on the Door Damper and Emergency Operation Cylinder |
| TASK 52-22-31-820-001-A | Adjustment of the Stop and Guide Fittings |
Subtask 52-22-00-010-062-A ** ON A/C NOT FOR ALL
A. Get Access
(1) Partly open the applicable emergency exit door (referred to as door) (Ref. AMM TASK 52-22-00-010-001).
(2) Make sure that the special precaution on the door damper and emergency operation cylinder is done (Ref. AMM TASK 52-22-00-860-003).
Subtask 52-22-00-865-054-A ** ON A/C NOT FOR ALL (1) Partly open the applicable emergency exit door (referred to as door) (Ref. AMM TASK 52-22-00-010-001).
(2) Make sure that the special precaution on the door damper and emergency operation cylinder is done (Ref. AMM TASK 52-22-00-860-003).
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
Subtask 52-22-00-860-068-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 121VU | EIS/SLIDES/ARM AND WARN/FLT | 15WN | P11 |
| 121VU | EIS/SLIDES/ARM AND WARN/GND | 13WN | P10 |
| 121VU | EIS/SDAC1 AND 2/DOOR/DET/PAX | 48WV | P05 |
C. Aircraft Maintenance Configuration
(1) Make sure that the door linings and the door frame linings are removed (Ref. AMM TASK 25-23-47-000-012) (Ref. AMM TASK 25-23-47-000-013) (Ref. AMM TASK 25-23-47-000-010) and (Ref. AMM TASK 25-23-47-000-004).
(2) Install the 98D52207557000 BALLAST WEIGHT - EMERGENCY EXIT on the door to replace the weight of the door linings during the adjustment procedure.
(3) Make sure that the door stays in the lifted position. If not, increase the tension of the torsion spring (Ref. AMM TASK 52-22-00-820-005).
(4) Make sure that the stops at the door frame and the fuselage are in the center position (Ref. AMM TASK 52-22-31-820-001).
Subtask 52-22-00-860-068-B ** ON A/C NOT FOR ALL (1) Make sure that the door linings and the door frame linings are removed (Ref. AMM TASK 25-23-47-000-012) (Ref. AMM TASK 25-23-47-000-013) (Ref. AMM TASK 25-23-47-000-010) and (Ref. AMM TASK 25-23-47-000-004).
(2) Install the 98D52207557000 BALLAST WEIGHT - EMERGENCY EXIT on the door to replace the weight of the door linings during the adjustment procedure.
(3) Make sure that the door stays in the lifted position. If not, increase the tension of the torsion spring (Ref. AMM TASK 52-22-00-820-005).
(4) Make sure that the stops at the door frame and the fuselage are in the center position (Ref. AMM TASK 52-22-31-820-001).
C. Aircraft Maintenance Configuration
(1) Make sure that the door linings and the door frame linings are removed (Ref. AMM TASK 25-23-47-000-010).
(2) Install the 98D52207557000 BALLAST WEIGHT - EMERGENCY EXIT on the door to replace the weight of the door linings during the adjustment procedure.
(3) Make sure that the door stays in the lifted position. If not, increase the tension of the torsion spring (Ref. AMM TASK 52-22-00-820-005).
(4) Make sure that the stops at the door frame and the fuselage are in the center position (Ref. AMM TASK 52-22-31-820-001).
4. Procedure(1) Make sure that the door linings and the door frame linings are removed (Ref. AMM TASK 25-23-47-000-010).
(2) Install the 98D52207557000 BALLAST WEIGHT - EMERGENCY EXIT on the door to replace the weight of the door linings during the adjustment procedure.
(3) Make sure that the door stays in the lifted position. If not, increase the tension of the torsion spring (Ref. AMM TASK 52-22-00-820-005).
(4) Make sure that the stops at the door frame and the fuselage are in the center position (Ref. AMM TASK 52-22-31-820-001).
Subtask 52-22-00-820-050-A ** ON A/C NOT FOR ALL
A. Adjustment for the Parallel Motion
Parallel Motion for Emergency Exit Door ** ON A/C NOT FOR ALL
Parallel Motion for Emergency Exit Door ** ON A/C NOT FOR ALL
(1) Measure the distance "A" between the front and rear edges of the door and the fuselage:
(a) Move the door in the open direction until the upper guide arm (5) is in the rectangular position.
(b) The distance "A" must be the same at all positions. The tolerance is 2.0 mm (0.079 in.) maximum.
(2) If the distance "A" is out of tolerance, disconnect the lower guide arm (6) from the guide fitting (7) of the door as follows:
(a) Remove and discard the cotter pin (12) from the nut (11).
(b) Remove the nut (11), the washers (9), the bush (10) and the bolt (8) from the guide fitting (7).
(c) Disconnect the eye-end of the guide arm (6) from the fork-end of the guide fitting (7).
(d) Attach the guide arm (6) with TAPE - SELF-AMALGAMATING to the door frame of the fuselage.
(3) Adjust the position of the upper attachment fitting (4) as follows:
(a) Loosen the nuts (1) to disconnect the attachment fitting (4) and the serrated plate (2) from the door frame.
(b) Change the position of the attachment fitting (4) and/or the serrated plate (2) until the dimension "A" is as specified.
(c) Tighten the nuts (1) again.
(4) Attach the lower guide arm (6) on the guide fitting (7) as follows:
(a) Release the lower guide arm (6) from the door frame.
(b) Connect the eye-end of the lower guide arm (6) in the related fork-end of the guide fitting (7)
(c) Install the bush (10), the bolt (8), the washers (9) and the nut (11).
(5) Make sure that the motion of the door is parallel to the fuselage.
Subtask 52-22-00-820-051-A ** ON A/C NOT FOR ALL Parallel Motion for Emergency Exit Door ** ON A/C NOT FOR ALL Parallel Motion for Emergency Exit Door ** ON A/C NOT FOR ALL (a) Move the door in the open direction until the upper guide arm (5) is in the rectangular position.
(b) The distance "A" must be the same at all positions. The tolerance is 2.0 mm (0.079 in.) maximum.
(2) If the distance "A" is out of tolerance, disconnect the lower guide arm (6) from the guide fitting (7) of the door as follows:
(a) Remove and discard the cotter pin (12) from the nut (11).
(b) Remove the nut (11), the washers (9), the bush (10) and the bolt (8) from the guide fitting (7).
(c) Disconnect the eye-end of the guide arm (6) from the fork-end of the guide fitting (7).
(d) Attach the guide arm (6) with TAPE - SELF-AMALGAMATING to the door frame of the fuselage.
(3) Adjust the position of the upper attachment fitting (4) as follows:
(a) Loosen the nuts (1) to disconnect the attachment fitting (4) and the serrated plate (2) from the door frame.
(b) Change the position of the attachment fitting (4) and/or the serrated plate (2) until the dimension "A" is as specified.
(c) Tighten the nuts (1) again.
(4) Attach the lower guide arm (6) on the guide fitting (7) as follows:
(a) Release the lower guide arm (6) from the door frame.
(b) Connect the eye-end of the lower guide arm (6) in the related fork-end of the guide fitting (7)
(c) Install the bush (10), the bolt (8), the washers (9) and the nut (11).
NOTE: The bolt (8) must go in smoothly.
(d) If you cannot install the bolt (8) smoothly, adjust the position of the lower attachment fitting (3). NOTE: This adjustment is the same as for the upper attachment fitting (4).
(e) Tighten the nut (11) and safety it with the new AIPC 52-22-02-04-330 COTTER PIN (12) or the new AIPC 52-22-84-20-180 COTTER PIN (12). (5) Make sure that the motion of the door is parallel to the fuselage.
B. Adjustment of the Skin Offset (Y-Axis of the Door)
(1) Move the door rearward and pull it inboard until the guide rollers (21) and (23) engage in the guide fittings (22) and (24).
(2) Measure the clearance "B" between the guide rollers (21) and (23) and the guide fittings (22) and (24).
(4) Make sure that the distance "D" between the heads of the stop bolts (35) and the surface of the stop bracket (34) is pre-adjusted with 4.0 mm (0.157 in.).
(5) Operate the outboard locking handle to close the door from the outer side.
(6) Make sure that a minimum of three stop bolts (35) touch the related fuselage fitting (31).
(a) Make sure that the skin offset "C" at the forward doors is between 0.4 mm (0.016 in.) and 3.6 mm (0.142 in.).
(b) Make sure that the skin offset "C" at the rear doors is between 0.1 mm (0.004 in.) and 3.1 mm (0.122 in.).
(8) If the skin offset "C" is out of tolerance, adjust the stop bolts (35) as follows:
(a) If necessary, bend the lock plates (32) to release the nuts (33).
1 If it was necessary to bend the lock plates (32), replace the AIPC 52-22-31-02-040 LOCK PLATES (32) or the AIPC 52-22-84-80-040 LOCK PLATES (32).
(b) Loosen the nuts (33) and turn the stop bolts (35) as necessary until the skin offset is correct.
(c) Make sure that the dimension "D" is not more than 6.0 mm (0.236 in.).
(d) TORQUE the nuts (33) to between 2.2 and 2.0 m.daN (16.22 and 14.75 lbf.ft ).
(e) Safety the nuts (33) with the lock plates (32).
Subtask 52-22-00-820-051-CS ** ON A/C NOT FOR ALL (1) Move the door rearward and pull it inboard until the guide rollers (21) and (23) engage in the guide fittings (22) and (24).
(2) Measure the clearance "B" between the guide rollers (21) and (23) and the guide fittings (22) and (24).
NOTE: The clearance must be between 0.1 mm (0.004 in.) and 0.5 mm (0.020 in.).
(3) If the clearance "B" is out of tolerance, change the position of the guide fittings (22) and (24) in parallel to the loftline. (4) Make sure that the distance "D" between the heads of the stop bolts (35) and the surface of the stop bracket (34) is pre-adjusted with 4.0 mm (0.157 in.).
(5) Operate the outboard locking handle to close the door from the outer side.
(6) Make sure that a minimum of three stop bolts (35) touch the related fuselage fitting (31).
NOTE: A minimum of one stop bolt (35) on each side must touch.
(7) Measure the skin offset "C" which must be always out of wind between the door contour and the fuselage contour: (a) Make sure that the skin offset "C" at the forward doors is between 0.4 mm (0.016 in.) and 3.6 mm (0.142 in.).
(b) Make sure that the skin offset "C" at the rear doors is between 0.1 mm (0.004 in.) and 3.1 mm (0.122 in.).
(8) If the skin offset "C" is out of tolerance, adjust the stop bolts (35) as follows:
(a) If necessary, bend the lock plates (32) to release the nuts (33).
1 If it was necessary to bend the lock plates (32), replace the AIPC 52-22-31-02-040 LOCK PLATES (32) or the AIPC 52-22-84-80-040 LOCK PLATES (32).
(b) Loosen the nuts (33) and turn the stop bolts (35) as necessary until the skin offset is correct.
(c) Make sure that the dimension "D" is not more than 6.0 mm (0.236 in.).
(d) TORQUE the nuts (33) to between 2.2 and 2.0 m.daN (16.22 and 14.75 lbf.ft )
. (e) Safety the nuts (33) with the lock plates (32).
B. Adjustment of the Skin Offset (Y-Axis of the Door)
(1) Move the door rearward and pull it inboard until the guide rollers (21) and (23) engage in the guide fittings (22) and (24).
(2) Measure clearance B between the guide rollers (21) and (23) and the guide fittings (22) and (24).
(3) Make sure that clearance B is between 0.1 mm (0.004 in.) and 0.5 mm (0.020 in.)
(4) If clearance B is out of tolerance, change the position of the guide fittings (22) and (24) in parallel to the loftline.
(5) Make sure that distance D between the heads of the stop bolts (35) and the surface of the stop bracket (34) is pre-adjusted with 4.0 mm (0.157 in.).
(6) Operate the outboard locking handle to close the door from the outer side.
(7) Make sure that a minimum of three stop bolts (35) touch the related fuselage fitting (31).
(a) Make sure that skin offset C at the forward doors is between 0.4 mm (0.016 in.) and 3.6 mm (0.142 in.).
(b) Make sure that skin offset C at the rear doors is between 0.1 mm (0.004 in.) and 3.1 mm (0.122 in.).
(9) If skin offset C is out of tolerance, adjust the stop bolts (35) as follows:
(a) If necessary, bend the lock plates (32) to release the nuts (33):
1 If it was necessary to bend the lock plates (32), replace the AIPC 52-22-31-02-040 LOCK PLATES (32) or the AIPC 52-22-84-80-040 LOCK PLATES (32).
(b) Loosen the nuts (33) and turn the stop bolts (35) as necessary until the skin offset is correct.
(c) Make sure that dimension D is not more than 6.0 mm (0.236 in.).
(d) TORQUE the nuts (33) to between 2.2 and 2.0 m.daN (16.22 and 14.75 lbf.ft ).
(e) Safety the nuts (33) with the lock plates (32).
Subtask 52-22-00-820-052-B ** ON A/C NOT FOR ALL (1) Move the door rearward and pull it inboard until the guide rollers (21) and (23) engage in the guide fittings (22) and (24).
(2) Measure clearance B between the guide rollers (21) and (23) and the guide fittings (22) and (24).
(3) Make sure that clearance B is between 0.1 mm (0.004 in.) and 0.5 mm (0.020 in.)
(4) If clearance B is out of tolerance, change the position of the guide fittings (22) and (24) in parallel to the loftline.
(5) Make sure that distance D between the heads of the stop bolts (35) and the surface of the stop bracket (34) is pre-adjusted with 4.0 mm (0.157 in.).
(6) Operate the outboard locking handle to close the door from the outer side.
(7) Make sure that a minimum of three stop bolts (35) touch the related fuselage fitting (31).
NOTE: A minimum of one stop bolt (35) on each side must touch.
(8) Measure skin offset C which must be always out of wind between the door contour and the fuselage contour: (a) Make sure that skin offset C at the forward doors is between 0.4 mm (0.016 in.) and 3.6 mm (0.142 in.).
(b) Make sure that skin offset C at the rear doors is between 0.1 mm (0.004 in.) and 3.1 mm (0.122 in.).
(9) If skin offset C is out of tolerance, adjust the stop bolts (35) as follows:
(a) If necessary, bend the lock plates (32) to release the nuts (33):
1 If it was necessary to bend the lock plates (32), replace the AIPC 52-22-31-02-040 LOCK PLATES (32) or the AIPC 52-22-84-80-040 LOCK PLATES (32).
(b) Loosen the nuts (33) and turn the stop bolts (35) as necessary until the skin offset is correct.
(c) Make sure that dimension D is not more than 6.0 mm (0.236 in.).
(d) TORQUE the nuts (33) to between 2.2 and 2.0 m.daN (16.22 and 14.75 lbf.ft )
. (e) Safety the nuts (33) with the lock plates (32).
C. Adjustment of the Clearances around the Door (X-Axis of the Door)
Lateral and Lower Clearances - Fuselage/Emergency Exit Door ** ON A/C NOT FOR ALL
Lateral and Lower Clearances - Fuselage/Emergency Exit Door ** ON A/C NOT FOR ALL
(1) Make sure that the door is closed (Ref. AMM TASK 52-22-00-410-001).
(2) Measure the distance "G" between the door edge member and the door frame.
(a) The distance "G" must be between 71.5 mm (2.815 in.) and 68.5 mm (2.697 in.).
(3) Measure the lateral clearances "E" and the lower clearance "F" between the door and the fuselage from the outboard side.
(a) The clearances must be between 2.5 mm (0.098 in.) and 5.5 mm (0.217 in.).
(4) If the lateral clearances "E" or the distance "G" are out of tolerance, change the quantity of the adjustment washers (42) as follows:
(b) Remove the nut (49), the washers (46), the upper hinge bolt (45) and the bracket (67) from the control lever (48).
(c) Remove the bracket (67), the washer (41), the adjustment washers (42) and the bushes (47) from the spacer tube (44).
(d) Change the quantity of the adjustment washers (42) as necessary until the lateral clearances "E" are correct.
(e) Put the bracket (67), the adjustment washers (42) and the washer (41) in position and install the bushes (47) into the spacer tube (44).
(f) Install the upper hinge bolt (45), the washers (46) and the nut (49) on the control lever (48).
(g) Measure the clearance "H" between the adjustment washers (42) and the spacer tube (44). A clearance of 0.05 mm (0.002 in.) is permitted.
(5) If the lower clearance "F" is out of tolerance, change the quantity of the adjustment washers (63) as follows:
(a) Remove the nut (49), the washers (46) and the upper hinge pin (45) from the control lever (48).
(b) Remove the journal pin (61) from the upper fork-end of the support arm (43).
(c) Change the quantity of the adjustment washers (63) as necessary until the lower clearances "F" are correct.
(d) Install the journal pin (61) in the upper fork-end (43).
(e) Measure the clearance "J" between the adjustment washers (63) and the spacer tube (44). A clearance of 0.05 mm (0.002 in.) is permitted.
(f) Install the upper hinge pin (45), the washers (46) and the nut (49) on the control lever (48).
(g) Tighten the nut (49) and safety it with the new AIPC 52-22-04-06-070 COTTER PIN (50) or the new AIPC 52-22-84-30-060 COTTER PIN (50).
(6) To set the door in the vertical position, change the quantity of the adjustment washers (52) as follows:
(a) Remove and discard the cotter pin (60) from the nut (59).
(b) Remove the nut (59), the washers (56) and the lower hinge bolt (55) from the lifting lever (58).
(c) Remove the bracket (68), the washer (51), the adjustment washers (52) and the bushes (57) from the spacer tube (54).
(d) Change the quantity of the adjustment washers (52) as necessary until the lateral clearances "E" are correct.
(e) Put the adjustment washers (52), the washer (51) and the bracket (68) in position and install the bushes (57) in the spacer tube (54).
(f) Install the lower hinge bolt (55), the washers (56) and the nut (59) on the lifting lever (58).
(g) Measure the clearance "H" between the adjustment washers (52) and the spacer tube (54). A clearance of 0.05 mm (0.002 in.) is permitted.
(7) Change the quantity of the adjustment washers (66) as follows:
(a) Remove the nut (59), the washers (56) and the lower hinge pin (55) from the lifting lever (58).
(b) Remove the journal pin (64) from the lower fork-end of the support arm (53).
(c) Change the quantity of the adjustment washers (66) as necessary until the lower clearances "F" are correct.
(d) Install the journal pin (64) in the lower fork-end (53).
(e) Measure the clearance "J" between the adjustment washers (66) and the spacer tube (54). A clearance of 0.05 mm (0.002 in.) is permitted.
(f) Install the lower hinge pin (55), the washers (56) and the nut (59) on the lifting lever (57).
(g) Tighten the nut (59) and safety it with the new AIPC 52-22-04-06-070 COTTER PIN (60) or the new AIPC 52-22-84-30-060 COTTER PIN (60).
5. Close-up Lateral and Lower Clearances - Fuselage/Emergency Exit Door ** ON A/C NOT FOR ALL Lateral and Lower Clearances - Fuselage/Emergency Exit Door ** ON A/C NOT FOR ALL (2) Measure the distance "G" between the door edge member and the door frame.
(a) The distance "G" must be between 71.5 mm (2.815 in.) and 68.5 mm (2.697 in.).
(3) Measure the lateral clearances "E" and the lower clearance "F" between the door and the fuselage from the outboard side.
(a) The clearances must be between 2.5 mm (0.098 in.) and 5.5 mm (0.217 in.).
(4) If the lateral clearances "E" or the distance "G" are out of tolerance, change the quantity of the adjustment washers (42) as follows:
NOTE: The adjustment washers (42) are installed between the fork-end of the support arm (43) and the control lever (48).
(a) Remove and discard the cotter pin (50) from the nut (49). (b) Remove the nut (49), the washers (46), the upper hinge bolt (45) and the bracket (67) from the control lever (48).
(c) Remove the bracket (67), the washer (41), the adjustment washers (42) and the bushes (47) from the spacer tube (44).
(d) Change the quantity of the adjustment washers (42) as necessary until the lateral clearances "E" are correct.
(e) Put the bracket (67), the adjustment washers (42) and the washer (41) in position and install the bushes (47) into the spacer tube (44).
(f) Install the upper hinge bolt (45), the washers (46) and the nut (49) on the control lever (48).
(g) Measure the clearance "H" between the adjustment washers (42) and the spacer tube (44). A clearance of 0.05 mm (0.002 in.) is permitted.
(5) If the lower clearance "F" is out of tolerance, change the quantity of the adjustment washers (63) as follows:
(a) Remove the nut (49), the washers (46) and the upper hinge pin (45) from the control lever (48).
(b) Remove the journal pin (61) from the upper fork-end of the support arm (43).
(c) Change the quantity of the adjustment washers (63) as necessary until the lower clearances "F" are correct.
(d) Install the journal pin (61) in the upper fork-end (43).
(e) Measure the clearance "J" between the adjustment washers (63) and the spacer tube (44). A clearance of 0.05 mm (0.002 in.) is permitted.
(f) Install the upper hinge pin (45), the washers (46) and the nut (49) on the control lever (48).
(g) Tighten the nut (49) and safety it with the new AIPC 52-22-04-06-070 COTTER PIN (50) or the new AIPC 52-22-84-30-060 COTTER PIN (50).
(6) To set the door in the vertical position, change the quantity of the adjustment washers (52) as follows:
(a) Remove and discard the cotter pin (60) from the nut (59).
(b) Remove the nut (59), the washers (56) and the lower hinge bolt (55) from the lifting lever (58).
(c) Remove the bracket (68), the washer (51), the adjustment washers (52) and the bushes (57) from the spacer tube (54).
(d) Change the quantity of the adjustment washers (52) as necessary until the lateral clearances "E" are correct.
(e) Put the adjustment washers (52), the washer (51) and the bracket (68) in position and install the bushes (57) in the spacer tube (54).
(f) Install the lower hinge bolt (55), the washers (56) and the nut (59) on the lifting lever (58).
(g) Measure the clearance "H" between the adjustment washers (52) and the spacer tube (54). A clearance of 0.05 mm (0.002 in.) is permitted.
(7) Change the quantity of the adjustment washers (66) as follows:
(a) Remove the nut (59), the washers (56) and the lower hinge pin (55) from the lifting lever (58).
(b) Remove the journal pin (64) from the lower fork-end of the support arm (53).
(c) Change the quantity of the adjustment washers (66) as necessary until the lower clearances "F" are correct.
(d) Install the journal pin (64) in the lower fork-end (53).
(e) Measure the clearance "J" between the adjustment washers (66) and the spacer tube (54). A clearance of 0.05 mm (0.002 in.) is permitted.
(f) Install the lower hinge pin (55), the washers (56) and the nut (59) on the lifting lever (57).
(g) Tighten the nut (59) and safety it with the new AIPC 52-22-04-06-070 COTTER PIN (60) or the new AIPC 52-22-84-30-060 COTTER PIN (60).
Subtask 52-22-00-410-057-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Remove the 98D52207557000 BALLAST WEIGHT - EMERGENCY EXIT from the door.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Install the door linings (Ref. AMM TASK 25-23-47-400-012) and (Ref. AMM TASK 25-23-47-400-013) and the door frame linings (Ref. AMM TASK 25-23-47-400-004) and (Ref. AMM TASK 25-23-47-400-009).
(4) Do the special precaution on the door damper and emergency operation cylinder (Ref. AMM TASK 52-22-00-860-004).
(5) Close the door correctly (Ref. AMM TASK 52-22-00-410-001).
Subtask 52-22-00-410-057-B ** ON A/C NOT FOR ALL (1) Remove the 98D52207557000 BALLAST WEIGHT - EMERGENCY EXIT from the door.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Install the door linings (Ref. AMM TASK 25-23-47-400-012) and (Ref. AMM TASK 25-23-47-400-013) and the door frame linings (Ref. AMM TASK 25-23-47-400-004) and (Ref. AMM TASK 25-23-47-400-009).
(4) Do the special precaution on the door damper and emergency operation cylinder (Ref. AMM TASK 52-22-00-860-004).
(5) Close the door correctly (Ref. AMM TASK 52-22-00-410-001).
A. Close Access
(1) Remove the 98D52207557000 BALLAST WEIGHT - EMERGENCY EXIT from the door.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Install the door frame linings (Ref. AMM TASK 25-23-47-400-010).
(4) Do the special precaution on the door damper and emergency operation cylinder (Ref. AMM TASK 52-22-00-860-004).
(5) Close the door correctly (Ref. AMM TASK 52-22-00-410-001).
Subtask 52-22-00-865-055-A ** ON A/C NOT FOR ALL (1) Remove the 98D52207557000 BALLAST WEIGHT - EMERGENCY EXIT from the door.
(2) Make sure that the work area is clean and clear of tools and other items.
(3) Install the door frame linings (Ref. AMM TASK 25-23-47-400-010).
(4) Do the special precaution on the door damper and emergency operation cylinder (Ref. AMM TASK 52-22-00-860-004).
(5) Close the door correctly (Ref. AMM TASK 52-22-00-410-001).