DOC AIRBUS | AMM A320FInstallation of the Forward Passenger/Crew Door
TASK 52-11-11-400-001-A
Installation of the Forward Passenger/Crew Door
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Expendable Parts
E. Referenced Information
3. Job Set-up
Subtask 52-11-11-869-052-A
Subtask 52-11-11-420-055-A
(1) Put the upper connection link (61) in position.
(2) Install the washer sets (64) on each side of the yoke (65).
(3) Install the bolt (63), the washer (62) and the spacer (73).
(4) Install the nut (70) and the washer (71).
(5) Tighten the nut (70).
(6) Safety the nut (70) with the new AIPC 52-11-01-04-150 COTTER PIN (69).
(7) Put the lower connection link (61) in position.
(8) Install the washer sets (64) on each side of the yoke (65).
(9) Install the bolt (63), the washer (62) and the spacer (73).
(10) Install the nut (70) and the washer (71).
(11) Tighten the nut (70).
(12) Safety the nut (70) with the new AIPC 52-11-01-04-150 COTTER PIN (69).
Subtask 52-11-11-420-050-A
(1) Slowly put the door in position in the door frame (the upper and lower guide arms are not installed).
(2) Make sure that the guide rollers (101) of the door engage in the guide fittings (102) and (106).
(3) Make sure that the seal is correctly installed on the door, at the front and rear vertical-frame sections.
(4) If the seal is not correctly applied on the door, do as follows:
(a) On the Z axis:
1 Removal of the lockwire:
a Remove and discard the lockwire from the nuts (201) and (203).
2 Loosen the nuts (201) and (203).
3 Adjust the length of the rod (202) until you get the correct configuration.
4 Tighten the nuts (201) and (203).
5 Safety the rod (202) with the14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
(b) On the X axis:
1 Disconnect the upper and lower connection links (61) from each side of the yoke (65).
2 Remove and discard the cotter pins (69).
3 Remove the nuts (70), the washers (71) and (62), the spacers (73) and the bolts (63) to disconnect the upper and lower connection links (61).
4 Adjust the door on the X axis with the washer sets (64) of a different thickness.
5 Make sure that clearance B is less than or equal to 0.1 mm (0.0039 in.).
7 Install the washers (62), the spacers (73) and the bolts (63).
8 Install the washers (71) and the nuts (70).
9 Tighten the nuts (70).
10 Safety the nuts (70) with the new AIPC 52-11-01-04-150 COTTER PIN (69).
(5) Make sure that when you open the door, clearance H1 between the door stops (301) and the door frame stops (302) is 5 mm (0.1969 in.) minimum.
Subtask 52-11-11-820-067-B
(1) Install the two TEMPLATE 70 MM (2,75 IN) on the X axis, on the door frame:
(a) Install one template between longerons L5 and L6.
(b) Install the other template between longerons L2 and L3.
(2) If the templates do not touch the door frame or the door contour on the X axis:
(a) Disconnect the upper and lower connection links (61) from each side of the yoke (65).
(b) Remove and discard the cotter pins (69).
(c) Remove the nuts (70), the washers (71) and (62), the spacers (73) and the bolts (63) to disconnect the upper and lower connection links (61).
(d) Adjust the door on the X axis with the washer sets (64) of a different thickness.
(e) Make sure that clearance B is less than or equal to 0.1 mm (0.0039 in.).
(g) Install the washers (62), the spacers (73) and the bolts (63).
(h) Install the washers (71) and the nuts (70).
(i) Tighten the nuts (70).
(j) Safety the nuts (70) with the new AIPC 52-11-01-04-150 COTTER PIN (69).
(3) Do a check of the peripheral clearance between the door and the door frame:
(a) At FR16, peripheral clearance E1 must be 4 +1 mm or -1 mm (0.1575 +0.0394 in. or -0.0394 in.).
(b) At FR20, peripheral clearance E2 must be 4 +1.8 mm or -1.8 mm (0.1575 +0.0709 in. or -0.0709 in.).
(4) Do a check of the flushness between the door and the door frame at door stop levels L1 thru L7:
(a) Flushness E5 is 1.5 +1 mm or -1 mm (0.0591 +0.0394 in. or -0.0394 in.).
(a) For the forward stops at FR16: 13.5 +1 mm or -1 mm (0.5315 +0.0394 in. or -0.0394 in.)
(b) For the aft stops at FR20: 13.5 +2 mm or -2 mm (0.5315 +0.0787 in. or -0.0787 in.).
(6) Make sure that clearance E7 is 0 +1 mm or -1 mm (0.0000 +0.0394 in. or -0.0394 in.).
(7) Make sure that clearance E9 of 4.5 +2 mm or -2 mm (0.1772 +0.0787 in. or -0.0787 in.) compresses the seal.
(8) When you open the door, make sure that clearance E10 between the stop and the door frame is 5 mm (0.1969 in.).
(9) If clearances E1, E2, E6 and E10 are not in the tolerances on the X axis, change the door position as follows:
(a) Disconnect the upper and lower connection links (61) from each side of the yoke (65).
(b) Remove and discard the cotter pins (69).
(c) Remove the nuts (70), the washers (71) and (62), the spacers (73) and the bolts (63) to disconnect the upper and lower connection links (61).
(d) Adjust the door on the X axis with the washer sets (64) of a different thickness.
(e) Make sure that clearance B is less than or equal to 0.1 mm (0.0039 in.).
(g) Install the washers (62), the spacers (73) and the bolts (63).
(h) Install the washers (71) and the nuts (70).
(i) Tighten the nuts (70).
(j) Safety the nuts (70) with the new AIPC 52-11-01-04-150 COTTER PIN (69).
(10) If clearances E3 and E7 are not in the tolerances on the Z axis, change the door position as follows:
(a) Removal of the lockwire:
1 Remove and discard the lockwire from the nuts (201) and (203).
(b) Loosen the nuts (201) and (203).
(c) Adjust the length of the rod (202) until you get the correct configuration.
(d) Tighten the nuts (201) and (203).
(e) Safety the rod (202) with the14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
(11) Do a check and adjust clearances E5 and E9 on the Y axis.
(12) Change the door position as follows:
(a) Remove the nuts (501) and the lock plate (502).
(b) Adjust the stop screws (503) to get the conditions that follow:
1 Clearance J1 between the stop and the door frame must be 0 +0 mm or +0.5 mm (0.0000 +0.0000 in. or +0.0197 in.).
2 Dimension J2 must be 6 mm (0.2362 in.) maximum.
3 Make sure that a minimum of:
(d) Install the nuts (501) with the new AIPC 52-11-11-21-040 LOCK PLATE (502) or the new AIPC 52-11-81-17-040 LOCK PLATE (502).
(e) TORQUE the nuts (501) to between 2.2 and 2 m.daN (16.22 and 14.75 lbf.ft )
.
(f) Fold the lugs of the lock plate (502).
(13) Remove the TEMPLATE 70 MM (2,75 IN) from the door frame.
Subtask 52-11-11-820-066-B
(1) Open and close the door some times.
(2) With the door in the up position, make sure that:
(a) The guide rollers (101) move off the guide fittings (102) and (106) with the clearances that follow:
1 Clearance C1: between 0.2 mm (0.0079 in.) and 0.8 mm (0.0315 in.)
2 Clearance C2: between 0.2 mm (0.0079 in.) and 2.2 mm (0.0866 in.).
(3) If the clearances are not in the tolerances, adjust the guide fittings (102) and (106) as follows:
(a) Open the door and identify the position of the serration plates (107) and (108) and of the upper and lower guide fittings (102) and (106).
(b) Loosen the screws (110) and move the guide fittings (102) and (106) to get correct clearances C1 and C2.
(c) Make sure that the eccentric washers (109):
(4) With the door in the down position, make sure that:
(a) The guide rollers (101) of the guide fittings (102) and (106) turn freely.
(b) Clearance C3 is 0.2 mm (0.0079 in.) minimum.
(c) Clearance C4 is between 0.2 mm (0.0079 in.) and 1.5 mm (0.0591 in.).
(d) Clearance C5 is between 3 mm (0.1181 in.) and 6 mm (0.2362 in.).
(5) Tighten the screws (110).
(6) Open the door.
(7) On the upper guide fittings (102), put the SHIM THICKNESS 0.2 MM (0.008 IN) in position between the bolt heads (105) and the guide rollers (101).
(8) Close the door.
(9) Measure the dimension between the shim and the guide rollers (101).
(10) Open the door.
(11) Remove the nuts (104), the bolts (105) and the shims.
(12) Adjust the thickness of the washers (103) until the guide rollers (101) touch the shim when the door is closed.
(13) Install the washers (103), the bolts (105) and the nuts (104).
(14) Tighten the nuts (104).
(15) Install the two shims in the upper guide fittings (102) on the heads of the bolts (105).
(16) Close the door.
(17) Make sure that there is no tension on the bolts (63) of the upper and lower connection links (61) when you install it in its hole.
(18) If there is tension on the bolts (63), change radius R of the upper and lower connection links (61) as follows:
(a) Disconnect the upper and lower connection links (61) from each side of the yoke (65).
(b) Remove and discard the cotter pins (69).
(c) Remove the nuts (70), the washers (71) and (62), the spacers (73), the bolts (63) and the washer sets (64).
(d) Disengage the support arm (72) from the upper connection link.
(e) Loosen the end of the upper connection link (61).
(f) Adjust the thickness of the set of the washers (64) on the upper connection link (61) to change radius R of the upper connection link (61).
(g) Tighten the end of the upper connection link (61).
(h) Install the washer sets (64).
(i) Install the support arm (72) on the upper and lower connection links (61).
(j) Install the washers (62), the spacers (73) and the bolts (63).
(k) Install the washers (71) and the nuts (70).
(l) TORQUE the nuts (70) to between 1.35 and 1.2 m.daN (119.47 and 106.19 lbf.in ).
(m) Safety the nuts (70) with the new AIPC 52-11-01-04-150 COTTER PIN (69).
Subtask 52-11-11-820-053-B
(1) Open the door.
(2) Put the SHIM THICKNESS 0.2 MM (0.008 IN) in position in the upper guide fittings (102).
(3) Close the door.
(4) Make sure clearance M1 between the locking hook (111) and the guide rollers (110) is 0.5 +0.3 mm or -0.3 mm (0.0197 +0.0118 in. or -0.0118 in.).
(a) Turn the rod (112) two turns to make it shorter.
(b) Remove and discard the cotter pin (117).
(c) Remove the nut (116).
(d) Pull the bush (118) 4 mm (0.1575 in.) out to disengage it from the stop flat (120).
(e) Turn the bush (118) the necessary correction value:
-0.9, -0.6, +0.6, +1.5 or +1.2.
(f) Make sure that the bush (118) stays engaged with its slots in the eccentric yoke (119).
(h) Install the nut (116).
(i) TORQUE the nut (116) to between 1.5 and 1.25 m.daN (132.74 and 110.62 lbf.in ).
(j) Turn the barrel of the rod (112) until the locking hook (111) touches the guide rollers (110).
(k) Install the new AIPC 53-16-01-23-020 COTTER PIN (117) or the new AIPC 53-16-81-23-100 COTTER PIN (117).
(l) Tighten the nuts (115) and the clamp (113).
(m) Make sure that the lock washers (114) are in the correct position.
14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
(6) Remove the two shims from the upper guide fittings (102) and the TEMPLATE 70 MM (2,75 IN) from the frame.
(7) Make sure that, when the door is closed, the guide rollers (110) turns freely.
Subtask 52-11-11-820-054-A
(1) Make sure that, during the opening of the door, the handle locks before the release of the guide rollers from the guide fittings.
(2) Make sure that, when you close the door with the inner control handle (805), you feel no hard points because of the non-retraction of the hook (804).
(3) If necessary, do the adjustment that follows:
(a) Removal of the lockwire:
1 Remove and discard the lockwire from the nuts (801) and (803).
(b) Decrease the rod length (802) until there is no hard point because of the non-retraction of the hook (804) (when you close the door in the up position).
(c) Tighten the nuts (801) and (803).
(d) Safety the nuts (801) and (803) with the14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -
(e) Put the door in the up position and make sure that you can correctly install the 98DNSA20206060 RIGGING PIN or the 98DNSA20206120 RIGGING PIN.
Subtask 52-11-11-820-062-A
Subtask 52-11-11-865-051-A
[Rev.10 from 2021]
2026.04.01 04:11:26 UTC
Installation of the Forward Passenger/Crew Door
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION:
THIS PART IS A REMOVABLE STRUCTURAL COMPONENT (RSC), WHICH CAN BE MOVED BETWEEN AIRCRAFT. THUS IT CAN HAVE DIFFERENT OPERATION CONDITIONS AND A DIFFERENT LIFE RECORD (FLIGHT HOURS/FLIGHT CYCLES/CALENDAR) FROM THE AIRCRAFT IT IS INSTALLED ON OR REMOVED FROM. THE OPERATOR IS RESPONSIBLE FOR THE SPECIFIC TRACKING AND CONTINUED AIRWORTHINESS OF REMOVABLE STRUCTURAL COMPONENTS. INCORRECT MAINTENANCE OF THESE COMPONENTS CAN CAUSE A RISK FOR THE FLIGHT SAFETY.
1. Reason for the JobSelf explanatory
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 | DYNAMOMETER 20 DAN (45 LBF) - PULL |
| No specific | AR | SHIM THICKNESS 0.2 MM (0.008 IN) |
| No specific | AR | TEMPLATE 70 MM (2,75 IN) |
| No specific | Torque wrench: range to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in ) | |
| No specific | Torque wrench: range to between 1.35 and 1.2 m.daN (119.47 and 106.19 lbf.in ) | |
| No specific | Torque wrench: range to between 1.5 and 1.25 m.daN (132.74 and 110.62 lbf.in ) | |
| No specific | Torque wrench: range to between 2.2 and 2 m.daN (16.22 and 14.75 lbf.ft ) | |
| 98A52008509000 | 1 | SLING-UNIVERSAL,DOORS |
| 98D52003003002 | 1 | SAFETY BARRIER KIT 4 |
| 98D52103006000 | 1 | PIN - RIGGING, DOOR ADJUST |
| 98D52103501000 | 1 | BALLAST WEIGHT - PASSENGER CREW DOOR |
| 98DNSA20206060 | 1 | RIGGING PIN |
| 98DNSA20206120 | 1 | RIGGING PIN |
| 98V52008861000 | 1 | SLING- UNIVERSAL, DOORS |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.03HBD9) | Synthetic Ester base Grease-General Purpose Low Temp - |
| (Material No.05BAE1) | Threadlocking Adhesive-- Medium strength - |
| (Material No.06AAC1) | Polysulfide Sealant-General Purpose Interfay - |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14QFB1) | Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 221 | FWD CAB UTILITY AREA |
| 222 | FWD CAB UTILITY AREA |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 3 | SELF-ADHESIVE PATCHES | AIPC 11-21-52-08-010 |
| 49 | COTTER PIN | AIPC 52-11-01-02-010 |
| 69 | COTTER PIN | AIPC 52-11-01-04-150 |
| 502 | LOCK PLATE | AIPC 52-11-11-21-040 |
| 69 | COTTER PIN | AIPC 52-11-81-02-150 |
| 49 | COTTER PIN | AIPC 52-11-81-05-010 |
| 502 | LOCK PLATE | AIPC 52-11-81-17-040 |
| 117 | COTTER PIN | AIPC 53-16-01-23-020 |
| 117 | COTTER PIN | AIPC 53-16-81-23-100 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 05-51-29-200-001-A | Inspection after Abnormal Movement of the Pax/Crew Door |
| TASK 05-51-29-200-001-B | Inspection after Abnormal Movement of the Pax/Crew Door or Emergency Exit |
| TASK 20-28-00-912-802-A | Electrical Bonding - General Maintenance Procedure |
| 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 25-23-43-000-001-A | Removal of the Upper Sidewall Panel |
| TASK 25-23-43-400-001-A | Installation of the Upper Sidewall Panel |
| TASK 25-23-44-000-001-A | Removal of the Lower Sidewall Panels (Dado Panels) |
| TASK 25-23-44-400-001-A | Installation of the Lower Sidewall Panels (Dado Panels) |
| TASK 25-23-45-000-002-A | Removal of the Door Frame Linings from the Right Forward Passenger/Crew Door |
| TASK 25-23-45-000-005-A | Removal of the Door Frame Linings from the Left Forward Passenger/Crew Door |
| TASK 25-23-45-400-006-A | Installation of the Door Frame Linings on the Left Forward Passenger/Crew Door |
| TASK 25-23-45-400-007-A | Installation of the Door Frame Linings on the Right Forward Passenger/Crew Door |
| TASK 25-23-46-400-001-A | Installation of the Door Linings on the Forward Passenger/Crew Doors |
| TASK 25-23-48-000-001-A | Removal of the Cove Light Panel |
| TASK 25-23-48-400-001-A | Installation of the Cove Light Panel |
| TASK 25-62-44-000-002-A | Removal of the Left Escape-Slide Pack-Assembly |
| TASK 25-62-44-000-012-A | Removal of the Left-Hand Escape-Slide-Raft Pack-Assembly |
| TASK 25-62-44-000-802-A | Removal of the Right Escape-Slide Pack-Assembly |
| TASK 25-62-44-000-804-A | Removal of the Right-Hand Escape-Slide-Raft Pack-Assembly |
| TASK 25-62-44-400-006-A | Installation of the Left Escape-Slide Pack-Assembly |
| TASK 25-62-44-400-007-A | Installation of the Left-Hand Escape-Slide-Raft Pack-Assembly |
| TASK 25-62-44-400-802-A | Installation of the Right Escape-Slide Pack-Assembly |
| TASK 25-62-44-400-803-A | Installation of the Right-Hand Escape-Slide-Raft Pack-Assembly |
| TASK 25-80-00-400-001-A | Installation of the Insulation Blankets |
| TASK 51-75-12-300-003-A | Repair of Minor Paint Damage (Topcoat Only) |
| TASK 52-00-00-081-001-A | Removal of the Safety Barrier |
| TASK 52-10-00-220-007-A | Check of the Preload of the Cover Plate |
| TASK 52-10-00-410-001-A | Closing of the Passenger/Crew Door |
| TASK 52-10-00-480-001-A | Installation of the Passenger/Crew Door Ballast Weight (98D52103501000) for Escape Slide |
| TASK 52-10-00-480-001-B | Installation of the Passenger/Crew Door Ballast Weight (98D52103501000) for Escape Slide/Raft |
| TASK 52-10-00-860-001-A | Special Precautions before Work on the Passenger/Crew Door |
| TASK 52-11-00-820-001-A | Adjustment of the Forward Passenger/Crew Door |
| TASK 52-11-00-820-002-A | Load Adjustment of the Control Handle of the FWD Passenger/Crew Door |
| TASK 52-11-00-820-002-A-01 | Load Adjustment of the Control Handle of the FWD Passenger/Crew Door |
| TASK 52-11-12-400-003-A | Installation of the Guide Arms |
| TASK 52-11-22-820-001-A | Adjustment/Test of the Release Mechanism of the Emergency Escape Slide |
| TASK 52-11-31-000-001-A | Removal of the Lining Flap |
| TASK 52-11-31-400-001-A | Installation of the Lining Flap |
| TASK 52-71-00-710-001-A | Operational Test of the Door Warning System |
| TASK 52-71-00-820-001-A | Adjustment of the Proximity Switches of the Locking Hook of the Passenger/Crew Doors with the Doors Checking Tool |
| TASK 52-71-00-820-001-A-01 | Adjustment of the Proximity Switches of the Locking Hook of the Passenger/Crew Doors with the ECAM Display Unit (DU) |
| TASK 06-41-52-00 | DOORS - DESCRIPTION AND OPERATION |
| TASK 06-41-53-00 | FUSELAGE-DESCRIPTION AND OPERATION |
Door RiggingSubtask 52-11-11-869-052-A
A. Aircraft Maintenance Configuration
(1) Make sure that the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE is in position.
(2) Make sure that you obeyed the special precautions (Ref. AMM TASK 52-10-00-860-001).
(3) Make sure that there is no blockage in the door drain holes.
(4) Make sure that the parts retained from the removed component are clean and in the correct condition.
(5) Make sure that the ground service network is energized
(Ref. AMM TASK 24-42-00-861-001).
(6) If the door you removed has damage because of an unusual movement, you must do the subsequent inspection (Ref. AMM TASK 05-51-29-200-001).
Subtask 52-11-11-865-055-A (1) Make sure that the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE is in position.
(2) Make sure that you obeyed the special precautions (Ref. AMM TASK 52-10-00-860-001).
(3) Make sure that there is no blockage in the door drain holes.
(4) Make sure that the parts retained from the removed component are clean and in the correct condition.
(5) Make sure that the ground service network is energized
(Ref. AMM TASK 24-42-00-861-001).
(6) If the door you removed has damage because of an unusual movement, you must do the subsequent inspection (Ref. AMM TASK 05-51-29-200-001).
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
Subtask 52-11-11-210-055-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C 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. Check before the Installation
(1) Before you install the door:
(a) When the door is in the up position, do a check of:
1 The rigging of the lowering shaft (F) with the 98DNSA20206060 RIGGING PIN or the 98DNSA20206120 RIGGING PIN
3 The rigging of the reducer shaft bellcrank (H) with the 98D52103006000 PIN - RIGGING, DOOR ADJUST.
(b) When the door is in the down position (door closed and locked):
1 On the door, put the emergency control handle in the ARMED position.
2 Do a check of:
Subtask 52-11-11-081-050-A (1) Before you install the door:
(a) When the door is in the up position, do a check of:
1 The rigging of the lowering shaft (F) with the 98DNSA20206060 RIGGING PIN or the 98DNSA20206120 RIGGING PIN
NOTE: The 98DNSA20206120 RIGGING PIN is an alternative to the 98DNSA20206060 RIGGING PIN. But, because of its length, you cannot use the 98DNSA20206120 RIGGING PIN at all the locations.
2 The rigging of the compensation mechanism (K) with the 98DNSA20206060 RIGGING PIN3 The rigging of the reducer shaft bellcrank (H) with the 98D52103006000 PIN - RIGGING, DOOR ADJUST.
(b) When the door is in the down position (door closed and locked):
1 On the door, put the emergency control handle in the ARMED position.
2 Do a check of:
- The rigging of the triple lever of the percussion mechanism (V) with the 98DNSA20206060 RIGGING PIN or the 98DNSA20206120 RIGGING PIN
- The rigging of the emergency control handle (Pt) with the 98DNSA20206060 RIGGING PIN or the 98DNSA20206120 RIGGING PIN
NOTE: The 98DNSA20206120 RIGGING PIN is an alternative to the 98DNSA20206060 RIGGING PIN. But, because of its length, you cannot use the 98DNSA20206120 RIGGING PIN at all the locations.
- The rigging of the reducer shaft mechanism (H) with the 98D52103006000 PIN - RIGGING, DOOR ADJUST
- The rigging of the triple bellcrank on the locking shaft mechanism (E) with the 98D52103006000 PIN - RIGGING, DOOR ADJUST.
D. Removal of the Safety Barrier
(1) Remove the 98D52003003002 SAFETY BARRIER KIT 4 from the opening of the removed door (Ref. AMM TASK 52-00-00-081-001).
Subtask 52-11-11-420-053-A (1) Remove the 98D52003003002 SAFETY BARRIER KIT 4 from the opening of the removed door (Ref. AMM TASK 52-00-00-081-001).
E. Installation of the Eye bolt on the Door
(1) Put the eye bolt (37) on the door fitting with the washer (36) and the bush (35).
(2) Install the clamp (38).
(3) Install the screws (34) and the nuts (39).
(4) Tighten the nuts (39).
(5) Install the washer (33) and the nut (32).
(6) TORQUE the nut (32) to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in ).
Subtask 52-11-11-010-055-A (1) Put the eye bolt (37) on the door fitting with the washer (36) and the bush (35).
(2) Install the clamp (38).
(3) Install the screws (34) and the nuts (39).
(4) Tighten the nuts (39).
(5) Install the washer (33) and the nut (32).
(6) TORQUE the nut (32) to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in )
. F. Removal of the Lining
(1) Remove the lining flap (Ref. AMM TASK 52-11-31-000-001).
(2) Remove the applicable door-frame lining panels (Ref. AMM TASK 25-23-45-000-002) or (Ref. AMM TASK 25-23-45-000-005).
(a) Refer to AMM chapter 06 for the door-frame lining panels details (Ref. AMM D/O 06-41-53-00).
(3) Remove the applicable upper sidewall-panels (Ref. AMM TASK 25-23-43-000-001).
(a) Refer to AMM CHAPTER 06 for the upper sidewall-panels details (Ref. AMM D/O 06-41-53-00).
(4) Remove the applicable lower sidewall-panels (Ref. AMM TASK 25-23-44-000-001).
(a) Refer to AMM chapter 06 for the lower sidewall-panels details (Ref. AMM D/O 06-41-53-00).
(5) Remove the applicable cover light-panels (Ref. AMM TASK 25-23-48-000-001).
(a) Refer to AMM chapter 06 for the cover light-panels details (Ref. AMM D/O 06-41-53-00).
Subtask 52-11-11-420-054-B (1) Remove the lining flap (Ref. AMM TASK 52-11-31-000-001).
(2) Remove the applicable door-frame lining panels (Ref. AMM TASK 25-23-45-000-002) or (Ref. AMM TASK 25-23-45-000-005).
(a) Refer to AMM chapter 06 for the door-frame lining panels details (Ref. AMM D/O 06-41-53-00).
(3) Remove the applicable upper sidewall-panels (Ref. AMM TASK 25-23-43-000-001).
(a) Refer to AMM CHAPTER 06 for the upper sidewall-panels details (Ref. AMM D/O 06-41-53-00).
(4) Remove the applicable lower sidewall-panels (Ref. AMM TASK 25-23-44-000-001).
(a) Refer to AMM chapter 06 for the lower sidewall-panels details (Ref. AMM D/O 06-41-53-00).
(5) Remove the applicable cover light-panels (Ref. AMM TASK 25-23-48-000-001).
(a) Refer to AMM chapter 06 for the cover light-panels details (Ref. AMM D/O 06-41-53-00).
G. Installation of the Sling
(1) Remove and discard the self-adhesive patches (3) from the door hoisting points.
(2) Remove the two blanking plugs (1) from the door hoisting points.
(3) Remove the door hoist fittings (2) from the 98A52008509000 SLING-UNIVERSAL,DOORS or the 98V52008861000 SLING- UNIVERSAL, DOORS.
(4) Install the door hoist fittings (2) on the door hoisting points.
(5) Put the door in the up position.
(6) Install the 98A52008509000 SLING-UNIVERSAL,DOORS or the 98V52008861000 SLING- UNIVERSAL, DOORS (10) on the door hoist fittings (2).
(7) If necessary, adjust the cable tension regulator to balance the door.
(8) Lift the 98A52008509000 SLING-UNIVERSAL,DOORS or the 98V52008861000 SLING- UNIVERSAL, DOORS(10) to remove the weight of the door from the door suspension.
Subtask 52-11-11-420-058-A (1) Remove and discard the self-adhesive patches (3) from the door hoisting points.
(2) Remove the two blanking plugs (1) from the door hoisting points.
(3) Remove the door hoist fittings (2) from the 98A52008509000 SLING-UNIVERSAL,DOORS or the 98V52008861000 SLING- UNIVERSAL, DOORS.
(4) Install the door hoist fittings (2) on the door hoisting points.
(5) Put the door in the up position.
(6) Install the 98A52008509000 SLING-UNIVERSAL,DOORS or the 98V52008861000 SLING- UNIVERSAL, DOORS (10) on the door hoist fittings (2).
(7) If necessary, adjust the cable tension regulator to balance the door.
(8) Lift the 98A52008509000 SLING-UNIVERSAL,DOORS or the 98V52008861000 SLING- UNIVERSAL, DOORS(10) to remove the weight of the door from the door suspension.
H. Loosening of the Girt Bar Fittings
(1) Loosen the screws (91) and (96) from the girt bar fittings (92) and (95).
(2) Remove the sealant with the Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) from:
Subtask 52-11-11-020-052-A (1) Loosen the screws (91) and (96) from the girt bar fittings (92) and (95).
(2) Remove the sealant with the Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) from:
- The edge of the girt bar fittings (92) and (95)
- The heads of the screws (91) and (96).
I. Removal of the Washers of the Upper Guide Fittings
(1) Remove the nuts (104), the bolts (105) and the washers (103) from the upper guide fittings (102).
(2) Install the bolts (105) and the nuts (104).
(3) Retain the washers (103).
Subtask 52-11-11-420-057-A ** ON A/C NOT FOR ALL (1) Remove the nuts (104), the bolts (105) and the washers (103) from the upper guide fittings (102).
(2) Install the bolts (105) and the nuts (104).
(3) Retain the washers (103).
J. Installation of the Ballast Weight
(1) Install the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR (Ref. AMM TASK 52-10-00-480-001).
Subtask 52-11-11-420-057-B ** ON A/C NOT FOR ALL (1) Install the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR (Ref. AMM TASK 52-10-00-480-001).
NOTE: If no ballast weight is available, it is permitted to use the escape-slide pack-assembly on the door during the adjustment (as an alternative to the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR).
(2) For the adjustment procedure, make sure that the escape-slide pack-assembly lets you have access to the ballast weight. J. Installation of the Ballast Weight
(1) Install the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR (Ref. AMM TASK 52-10-00-480-001).
4. Procedure(1) Install the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR (Ref. AMM TASK 52-10-00-480-001).
NOTE: If no ballast weight is available, it is permitted to use the escape-slide raft pack-assembly on the door during the adjustment (as an alternative to the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR).
(2) For the adjustment procedure, make sure that the escape-slide raft pack-assembly lets you have access to the ballast weight. Subtask 52-11-11-420-055-A
WARNING:
USE PROTECTIVE GOGGLES WHEN YOU REMOVE OR INSTALL A COTTER PIN. EACH TIME YOU REMOVE A COTTER PIN DURING THE TASK, DISCARD IT IMMEDIATELY. A LOOSE COTTER PIN CAN CUT YOU OR MAKE YOU BLIND.
A. Temporary Installation of the Door on the Door Support Arm (1) Put the upper connection link (61) in position.
(2) Install the washer sets (64) on each side of the yoke (65).
(3) Install the bolt (63), the washer (62) and the spacer (73).
(4) Install the nut (70) and the washer (71).
(5) Tighten the nut (70).
(6) Safety the nut (70) with the new AIPC 52-11-01-04-150 COTTER PIN (69).
(7) Put the lower connection link (61) in position.
(8) Install the washer sets (64) on each side of the yoke (65).
(9) Install the bolt (63), the washer (62) and the spacer (73).
(10) Install the nut (70) and the washer (71).
(11) Tighten the nut (70).
(12) Safety the nut (70) with the new AIPC 52-11-01-04-150 COTTER PIN (69).
WARNING:
USE PROTECTIVE GOGGLES WHEN YOU REMOVE OR INSTALL A COTTER PIN. EACH TIME YOU REMOVE A COTTER PIN DURING THE TASK, DISCARD IT IMMEDIATELY. A LOOSE COTTER PIN CAN CUT YOU OR MAKE YOU BLIND.
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.
B. Installation of the Door (1) Slowly put the door in position in the door frame (the upper and lower guide arms are not installed).
(2) Make sure that the guide rollers (101) of the door engage in the guide fittings (102) and (106).
(3) Make sure that the seal is correctly installed on the door, at the front and rear vertical-frame sections.
(4) If the seal is not correctly applied on the door, do as follows:
(a) On the Z axis:
1 Removal of the lockwire:
a Remove and discard the lockwire from the nuts (201) and (203).
2 Loosen the nuts (201) and (203).
3 Adjust the length of the rod (202) until you get the correct configuration.
4 Tighten the nuts (201) and (203).
5 Safety the rod (202) with the
(b) On the X axis:
1 Disconnect the upper and lower connection links (61) from each side of the yoke (65).
2 Remove and discard the cotter pins (69).
3 Remove the nuts (70), the washers (71) and (62), the spacers (73) and the bolts (63) to disconnect the upper and lower connection links (61).
4 Adjust the door on the X axis with the washer sets (64) of a different thickness.
5 Make sure that clearance B is less than or equal to 0.1 mm (0.0039 in.).
NOTE: The thickness of the two washer sets (64) at the lower and upper connection links (61) is equal to the nominal thickness.
Clearance B must be in the tolerance.
6 Connect the upper and lower connections links (61). Clearance B must be in the tolerance.
7 Install the washers (62), the spacers (73) and the bolts (63).
8 Install the washers (71) and the nuts (70).
9 Tighten the nuts (70).
10 Safety the nuts (70) with the new AIPC 52-11-01-04-150 COTTER PIN (69).
(5) Make sure that when you open the door, clearance H1 between the door stops (301) and the door frame stops (302) is 5 mm (0.1969 in.) minimum.
C. Adjustment of the Door in its Frame during the Door Closure
(1) Slowly close the door and make sure that:
(a) Open the door and find the position of the serration plates (107) and (108), and the upper and the lower guide fittings (102) and (106).
(b) Loosen the screws (110).
(c) Move the guide fittings (102) and (106) to get clearance H2.
(d) Make sure that the eccentric washers (109):
(4) Release the upper hook as follows:
(a) Open the door.
(b) Removal of the lockwire:
(c) Loosen the nuts (115).
(d) Release the lock washers (114).
(e) Loosen the clamp (113).
(f) Turn the barrel of the rod (112) to retract it.
(5) Slowly close the door and make sure that there are no hard points between the telescopic fork ends (402) and the girt bar fittings (401).
Subtask 52-11-11-820-050-A (1) Slowly close the door and make sure that:
- There are no hard points between the door stops (301) and the door frame stops (302).
- The upper hook (111) and the frame roller (110) do not touch.
NOTE: The guide rollers (101) touch the guide fittings (102) and (106).
(3) If clearance H2 is not in the tolerance, adjust the upper and lower guide fittings (102) and (106) as follows: (a) Open the door and find the position of the serration plates (107) and (108), and the upper and the lower guide fittings (102) and (106).
(b) Loosen the screws (110).
(c) Move the guide fittings (102) and (106) to get clearance H2.
(d) Make sure that the eccentric washers (109):
- Fully seal the holes of the guide fittings (102) and (106)
- Are not above the rounded areas or the spot-facing edges
- Are not out of the outer contour of the fitting.
(4) Release the upper hook as follows:
(a) Open the door.
(b) Removal of the lockwire:
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.
1 Remove and discard the lockwire from the nuts (115). (c) Loosen the nuts (115).
(d) Release the lock washers (114).
(e) Loosen the clamp (113).
(f) Turn the barrel of the rod (112) to retract it.
(5) Slowly close the door and make sure that there are no hard points between the telescopic fork ends (402) and the girt bar fittings (401).
WARNING:
USE PROTECTIVE GOGGLES WHEN YOU REMOVE OR INSTALL A COTTER PIN. EACH TIME YOU REMOVE A COTTER PIN DURING THE TASK, DISCARD IT IMMEDIATELY. A LOOSE COTTER PIN CAN CUT YOU OR MAKE YOU BLIND.
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.
D. Adjustment of the Door in the Down Position (1) Install the two TEMPLATE 70 MM (2,75 IN) on the X axis, on the door frame:
(a) Install one template between longerons L5 and L6.
(b) Install the other template between longerons L2 and L3.
(2) If the templates do not touch the door frame or the door contour on the X axis:
(a) Disconnect the upper and lower connection links (61) from each side of the yoke (65).
(b) Remove and discard the cotter pins (69).
(c) Remove the nuts (70), the washers (71) and (62), the spacers (73) and the bolts (63) to disconnect the upper and lower connection links (61).
(d) Adjust the door on the X axis with the washer sets (64) of a different thickness.
(e) Make sure that clearance B is less than or equal to 0.1 mm (0.0039 in.).
NOTE: The thickness of the two washer sets (64) at the level of the lower and upper connection links (61) is equal to the nominal thickness.
Clearance B must be in the tolerance.
(f) Connect the upper and lower connection links (61). Clearance B must be in the tolerance.
(g) Install the washers (62), the spacers (73) and the bolts (63).
(h) Install the washers (71) and the nuts (70).
(i) Tighten the nuts (70).
(j) Safety the nuts (70) with the new AIPC 52-11-01-04-150 COTTER PIN (69).
(3) Do a check of the peripheral clearance between the door and the door frame:
(a) At FR16, peripheral clearance E1 must be 4 +1 mm or -1 mm (0.1575 +0.0394 in. or -0.0394 in.).
(b) At FR20, peripheral clearance E2 must be 4 +1.8 mm or -1.8 mm (0.1575 +0.0709 in. or -0.0709 in.).
NOTE: A clearance of 4 +2.2 mm or -2.2 mm (0.1575 +0.0866 in. or -0.0866 in.) is permitted on the rear part with a maximum length of 400 mm (15.7480 in.).
This maximum total length can be the sum of smaller lengths at a maximum of three locations.
(c) Peripheral clearance E3 must be 4 +1.5 mm or -2.5 mm (0.1575 +0.0591 in. or -0.0984 in.). This maximum total length can be the sum of smaller lengths at a maximum of three locations.
(4) Do a check of the flushness between the door and the door frame at door stop levels L1 thru L7:
(a) Flushness E5 is 1.5 +1 mm or -1 mm (0.0591 +0.0394 in. or -0.0394 in.).
NOTE: A clearance of 1.5 +1.3 mm or -1.3 mm (0.0591 +0.0512 in. or -0.0512 in.) is permitted on the rear part with a maximum length of 400 mm (15.7480 in.).
This maximum total length can be the sum of smaller lengths at a maximum of three locations.
(5) Make sure that overlap E6 of the stop axis is: This maximum total length can be the sum of smaller lengths at a maximum of three locations.
(a) For the forward stops at FR16: 13.5 +1 mm or -1 mm (0.5315 +0.0394 in. or -0.0394 in.)
(b) For the aft stops at FR20: 13.5 +2 mm or -2 mm (0.5315 +0.0787 in. or -0.0787 in.).
(6) Make sure that clearance E7 is 0 +1 mm or -1 mm (0.0000 +0.0394 in. or -0.0394 in.).
(7) Make sure that clearance E9 of 4.5 +2 mm or -2 mm (0.1772 +0.0787 in. or -0.0787 in.) compresses the seal.
(8) When you open the door, make sure that clearance E10 between the stop and the door frame is 5 mm (0.1969 in.).
(9) If clearances E1, E2, E6 and E10 are not in the tolerances on the X axis, change the door position as follows:
(a) Disconnect the upper and lower connection links (61) from each side of the yoke (65).
(b) Remove and discard the cotter pins (69).
(c) Remove the nuts (70), the washers (71) and (62), the spacers (73) and the bolts (63) to disconnect the upper and lower connection links (61).
(d) Adjust the door on the X axis with the washer sets (64) of a different thickness.
(e) Make sure that clearance B is less than or equal to 0.1 mm (0.0039 in.).
NOTE: The thickness of the two washer sets (64) at the lower and upper connection links (61) is equal to the nominal thickness.
Clearance B must be in the tolerance.
(f) Connect the upper and lower connection links (61). Clearance B must be in the tolerance.
(g) Install the washers (62), the spacers (73) and the bolts (63).
(h) Install the washers (71) and the nuts (70).
(i) Tighten the nuts (70).
(j) Safety the nuts (70) with the new AIPC 52-11-01-04-150 COTTER PIN (69).
(10) If clearances E3 and E7 are not in the tolerances on the Z axis, change the door position as follows:
(a) Removal of the lockwire:
1 Remove and discard the lockwire from the nuts (201) and (203).
(b) Loosen the nuts (201) and (203).
(c) Adjust the length of the rod (202) until you get the correct configuration.
(d) Tighten the nuts (201) and (203).
(e) Safety the rod (202) with the
(11) Do a check and adjust clearances E5 and E9 on the Y axis.
(12) Change the door position as follows:
(a) Remove the nuts (501) and the lock plate (502).
(b) Adjust the stop screws (503) to get the conditions that follow:
1 Clearance J1 between the stop and the door frame must be 0 +0 mm or +0.5 mm (0.0000 +0.0000 in. or +0.0197 in.).
2 Dimension J2 must be 6 mm (0.2362 in.) maximum.
3 Make sure that a minimum of:
- Two stop screws touch one side of the door frame, and
- One stop screw touches the opposite side of the door frame.
(d) Install the nuts (501) with the new AIPC 52-11-11-21-040 LOCK PLATE (502) or the new AIPC 52-11-81-17-040 LOCK PLATE (502).
(e) TORQUE the nuts (501) to between 2.2 and 2 m.daN (16.22 and 14.75 lbf.ft )
. (f) Fold the lugs of the lock plate (502).
(13) Remove the TEMPLATE 70 MM (2,75 IN) from the door frame.
WARNING:
USE PROTECTIVE GOGGLES WHEN YOU REMOVE OR INSTALL A COTTER PIN. EACH TIME YOU REMOVE A COTTER PIN DURING THE TASK, DISCARD IT IMMEDIATELY. A LOOSE COTTER PIN CAN CUT YOU OR MAKE YOU BLIND.
E. Check and Adjustment of the Clearances between the Guide Rollers and the Guide Fittings (1) Open and close the door some times.
(2) With the door in the up position, make sure that:
(a) The guide rollers (101) move off the guide fittings (102) and (106) with the clearances that follow:
1 Clearance C1: between 0.2 mm (0.0079 in.) and 0.8 mm (0.0315 in.)
2 Clearance C2: between 0.2 mm (0.0079 in.) and 2.2 mm (0.0866 in.).
(3) If the clearances are not in the tolerances, adjust the guide fittings (102) and (106) as follows:
(a) Open the door and identify the position of the serration plates (107) and (108) and of the upper and lower guide fittings (102) and (106).
(b) Loosen the screws (110) and move the guide fittings (102) and (106) to get correct clearances C1 and C2.
(c) Make sure that the eccentric washers (109):
- Fully seal the holes of the guide fittings (102) and (106)
- Are not above the rounded areas or the spot-facing edges
- Are not out of the outer contour of the fitting.
(4) With the door in the down position, make sure that:
(a) The guide rollers (101) of the guide fittings (102) and (106) turn freely.
(b) Clearance C3 is 0.2 mm (0.0079 in.) minimum.
(c) Clearance C4 is between 0.2 mm (0.0079 in.) and 1.5 mm (0.0591 in.).
(d) Clearance C5 is between 3 mm (0.1181 in.) and 6 mm (0.2362 in.).
NOTE: Clearance C5 between 3 mm (0.1181 in.) and 8 mm (0.3150 in.) is permitted.
(e) If clearances C3 and C4 are not in the tolerances, adjust the upper and lower guide fittings (102) and (106). (5) Tighten the screws (110).
(6) Open the door.
(7) On the upper guide fittings (102), put the SHIM THICKNESS 0.2 MM (0.008 IN) in position between the bolt heads (105) and the guide rollers (101).
(8) Close the door.
(9) Measure the dimension between the shim and the guide rollers (101).
(10) Open the door.
(11) Remove the nuts (104), the bolts (105) and the shims.
(12) Adjust the thickness of the washers (103) until the guide rollers (101) touch the shim when the door is closed.
(13) Install the washers (103), the bolts (105) and the nuts (104).
(14) Tighten the nuts (104).
(15) Install the two shims in the upper guide fittings (102) on the heads of the bolts (105).
(16) Close the door.
(17) Make sure that there is no tension on the bolts (63) of the upper and lower connection links (61) when you install it in its hole.
(18) If there is tension on the bolts (63), change radius R of the upper and lower connection links (61) as follows:
(a) Disconnect the upper and lower connection links (61) from each side of the yoke (65).
(b) Remove and discard the cotter pins (69).
(c) Remove the nuts (70), the washers (71) and (62), the spacers (73), the bolts (63) and the washer sets (64).
(d) Disengage the support arm (72) from the upper connection link.
(e) Loosen the end of the upper connection link (61).
(f) Adjust the thickness of the set of the washers (64) on the upper connection link (61) to change radius R of the upper connection link (61).
(g) Tighten the end of the upper connection link (61).
(h) Install the washer sets (64).
(i) Install the support arm (72) on the upper and lower connection links (61).
(j) Install the washers (62), the spacers (73) and the bolts (63).
(k) Install the washers (71) and the nuts (70).
(l) TORQUE the nuts (70) to between 1.35 and 1.2 m.daN (119.47 and 106.19 lbf.in )
. (m) Safety the nuts (70) with the new AIPC 52-11-01-04-150 COTTER PIN (69).
WARNING:
USE PROTECTIVE GOGGLES WHEN YOU REMOVE OR INSTALL A COTTER PIN. EACH TIME YOU REMOVE A COTTER PIN DURING THE TASK, DISCARD IT IMMEDIATELY. A LOOSE COTTER PIN CAN CUT YOU OR MAKE YOU BLIND.
F. Adjustment of the Upper Hook (1) Open the door.
(2) Put the SHIM THICKNESS 0.2 MM (0.008 IN) in position in the upper guide fittings (102).
(3) Close the door.
(4) Make sure clearance M1 between the locking hook (111) and the guide rollers (110) is 0.5 +0.3 mm or -0.3 mm (0.0197 +0.0118 in. or -0.0118 in.).
NOTE: Clearance M1 automatically adjusts when you turn the eccentric yoke (119).
(5) If clearance M1 is not in the tolerance, do as follows: (a) Turn the rod (112) two turns to make it shorter.
(b) Remove and discard the cotter pin (117).
(c) Remove the nut (116).
(d) Pull the bush (118) 4 mm (0.1575 in.) out to disengage it from the stop flat (120).
(e) Turn the bush (118) the necessary correction value:
-0.9, -0.6, +0.6, +1.5 or +1.2.
(f) Make sure that the bush (118) stays engaged with its slots in the eccentric yoke (119).
NOTE: The slotted drive between the bush (118) and the eccentric yoke (119) has a foolproofing device (one position only).
(g) Push back the bush (118) until the correction value aligns with the mark on the stop flat (120). (h) Install the nut (116).
(i) TORQUE the nut (116) to between 1.5 and 1.25 m.daN (132.74 and 110.62 lbf.in )
. (j) Turn the barrel of the rod (112) until the locking hook (111) touches the guide rollers (110).
(k) Install the new AIPC 53-16-01-23-020 COTTER PIN (117) or the new AIPC 53-16-81-23-100 COTTER PIN (117).
(l) Tighten the nuts (115) and the clamp (113).
(m) Make sure that the lock washers (114) are in the correct position.
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.
(n) Safety the nuts (115) and the lock washers (114) with the (6) Remove the two shims from the upper guide fittings (102) and the TEMPLATE 70 MM (2,75 IN) from the frame.
(7) Make sure that, when the door is closed, the guide rollers (110) turns freely.
G. Check of the Door Adjustment
(1) Open and close the door some times and make sure that the clearances between the guide rollers (101) and the guide fittings (102) are correct (with the door in the up and down positions).
(2) Make sure that clearance E8 is 70 +0.7 mm or -0.7 mm (2.7559 +0.0276 in. or -0.0276 in.).
Subtask 52-11-11-820-063-A (1) Open and close the door some times and make sure that the clearances between the guide rollers (101) and the guide fittings (102) are correct (with the door in the up and down positions).
(2) Make sure that clearance E8 is 70 +0.7 mm or -0.7 mm (2.7559 +0.0276 in. or -0.0276 in.).
H. Adjustment of the Safety Pin
(1) Close the door.
(2) Make sure that clearance G1 between the fittings (601) and the safety pin (602) is 4 +1 mm or -1 mm (0.1575 +0.0394 in. or -0.0394 in.).
(3) If clearance G1 is not in the tolerance, adjust the safety pin (602) as follows:
(a) Open the door.
(b) Remove the stop screw (604) and the adjustment washers (603).
(c) Install the new adjustable washers (603) to get clearance G1.
(d) Apply Threadlocking Adhesive-- Medium strength - (Material No.05BAE1) on the threads of the stop screw (604).
(e) Install the stop screw (604).
(f) TORQUE the stop screw (604) to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in ).
Subtask 52-11-11-420-059-A (1) Close the door.
(2) Make sure that clearance G1 between the fittings (601) and the safety pin (602) is 4 +1 mm or -1 mm (0.1575 +0.0394 in. or -0.0394 in.).
(3) If clearance G1 is not in the tolerance, adjust the safety pin (602) as follows:
(a) Open the door.
(b) Remove the stop screw (604) and the adjustment washers (603).
(c) Install the new adjustable washers (603) to get clearance G1.
(d) Apply Threadlocking Adhesive-- Medium strength - (Material No.05BAE1) on the threads of the stop screw (604).
(e) Install the stop screw (604).
(f) TORQUE the stop screw (604) to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in )
. I. Installation of the Door Support Arm
(2) Install the bonding leads (68), the washers (67) and the bolts (66).
(3) Tighten the bolts (66).
(4) Do an electrical bonding when you install the bolts (66) (Ref. AMM TASK 20-28-00-912-802).
Subtask 52-11-11-420-060-A WARNING:
USE PROTECTIVE GOGGLES WHEN YOU REMOVE OR INSTALL A COTTER PIN. EACH TIME YOU REMOVE A COTTER PIN DURING THE TASK, DISCARD IT IMMEDIATELY. A LOOSE COTTER PIN CAN CUT YOU OR MAKE YOU BLIND.
(1) Install the new AIPC 52-11-01-04-150 COTTER PIN (69) or the new AIPC 52-11-81-02-150 COTTER PIN (69). (2) Install the bonding leads (68), the washers (67) and the bolts (66).
(3) Tighten the bolts (66).
(4) Do an electrical bonding when you install the bolts (66) (Ref. AMM TASK 20-28-00-912-802).
J. Connection of the Electrical Harness
(1) Install the attachment clamps on the cable sheaths.
(2) Remove the CAP-BLANKING from each electrical connector and receptacle.
(3) Make sure that all the electrical connections are clean and in the correct condition.
(4) Connect the electrical connectors:
(a) For the left side:
Subtask 52-11-11-420-061-B (1) Install the attachment clamps on the cable sheaths.
(2) Remove the CAP-BLANKING from each electrical connector and receptacle.
(3) Make sure that all the electrical connections are clean and in the correct condition.
(4) Connect the electrical connectors:
(a) For the left side:
- 2819VC
- 2818VC.
K. Installation of the Upper and Lower Guide Arms
(1) For the door that has the door damper and the emergency operation cylinder, (serie P/Ns FE174 and FE196), connect the upper and lower guide arms (132) and (133) on the door side (Ref. AMM TASK 52-11-12-400-003).
(2) For the door that has the door damper and the emergency operation cylinder, (serie P/N FE240), connect the upper and lower guide arms as follows:
(a) Put the door in the up closed position, against the seal (134) at FR20.
1 Do a check of clearance L1 at FR16.
2 Measure the clearance at door stop level L5.
3 Make sure that clearance L1 is equal to the difference between flushness D1 (measured between the door and the door frame forward of the door) and flushness D2 (measured between the door and the door frame aft of the door).
4 Clearance L1 is maximum 5 mm (0.1969 in.).
5 If necessary, adjust the fittings (130) and (131) on the X axis.
(b) Connect the guide arms (133) and (132) (Ref. AMM TASK 52-11-12-400-003).
Subtask 52-11-11-420-063-B (1) For the door that has the door damper and the emergency operation cylinder, (serie P/Ns FE174 and FE196), connect the upper and lower guide arms (132) and (133) on the door side (Ref. AMM TASK 52-11-12-400-003).
(2) For the door that has the door damper and the emergency operation cylinder, (serie P/N FE240), connect the upper and lower guide arms as follows:
(a) Put the door in the up closed position, against the seal (134) at FR20.
1 Do a check of clearance L1 at FR16.
2 Measure the clearance at door stop level L5.
3 Make sure that clearance L1 is equal to the difference between flushness D1 (measured between the door and the door frame forward of the door) and flushness D2 (measured between the door and the door frame aft of the door).
4 Clearance L1 is maximum 5 mm (0.1969 in.).
5 If necessary, adjust the fittings (130) and (131) on the X axis.
(b) Connect the guide arms (133) and (132) (Ref. AMM TASK 52-11-12-400-003).
L. Connection of the Door Damper and Emergency Operation Cylinder
(1) Put the telescopic rod (52) in position on the eye bolt (37).
(2) Install the spacer (51), the screw (42) and the lock washer (53).
(3) Install the washer (50) and the nut (48).
(4) Tighten the nut (48).
Subtask 52-11-11-020-060-B (1) Put the telescopic rod (52) in position on the eye bolt (37).
(2) Install the spacer (51), the screw (42) and the lock washer (53).
(3) Install the washer (50) and the nut (48).
(4) Tighten the nut (48).
WARNING:
USE PROTECTIVE GOGGLES WHEN YOU REMOVE OR INSTALL A COTTER PIN. EACH TIME YOU REMOVE A COTTER PIN DURING THE TASK, DISCARD IT IMMEDIATELY. A LOOSE COTTER PIN CAN CUT YOU OR MAKE YOU BLIND.
(5) Install the new AIPC 52-11-01-02-010 COTTER PIN (49) or the new AIPC 52-11-81-05-010 COTTER PIN (49). M. Removal of the Sling
(1) Remove the sling (10) from the door hoist fittings (2).
(2) Remove the door hoist fittings (2) from the door.
(3) Attach the door hoist fittings (2) to the sling (10).
(4) Install the blanking plugs (1) in the door hoisting point holes.
(5) Install the new AIPC 11-21-52-08-010 SELF-ADHESIVE PATCHES (3) on the doors at the door hoisting points.
(6) If necessary, paint the two self-adhesive patches (3) the same color as the adjacent area (Ref. AMM TASK 51-75-12-300-003).
Subtask 52-11-11-820-069-A (1) Remove the sling (10) from the door hoist fittings (2).
(2) Remove the door hoist fittings (2) from the door.
(3) Attach the door hoist fittings (2) to the sling (10).
(4) Install the blanking plugs (1) in the door hoisting point holes.
(5) Install the new AIPC 11-21-52-08-010 SELF-ADHESIVE PATCHES (3) on the doors at the door hoisting points.
(6) If necessary, paint the two self-adhesive patches (3) the same color as the adjacent area (Ref. AMM TASK 51-75-12-300-003).
N. Check and Adjustment of the Escape Slide
(1) Close the door.
(2) Put the emergency control handle in the ARMED position.
(3) Install the 98DNSA20206060 RIGGING PIN or the 98DNSA20206120 RIGGING PIN on the emergency control handle (rigging point).
(a) Clearance F1 must be between 0.2 mm (0.0079 in.) and 0.8 mm (0.0315 in.).
(b) Clearance F2 must be between 0.5 mm (0.0197 in.) and 1.0 mm (0.0394 in.).
(5) If clearances F1 and F2 are not in the tolerances, adjust the girt bar fittings (92) and (95) as follows:
(a) Remove the 98DNSA20206060 RIGGING PIN or the 98DNSA20206120 RIGGING PIN from the emergency control handle (rigging point).
(b) Put the emergency control handle in the DISARMED position.
(c) Open the door and find the position of the serration plates (93) and (94) and the girt bar fittings (92) and (95).
(d) Adjust the position of the girt bar fittings (92) and (95) on the X axis and the Y axis to get correct clearances F1 and F2.
(e) Tighten the screws (91) and (96) on the girt bar fittings (92) and (95).
(f) Apply Polysulfide Sealant-General Purpose Interfay - (Material No.06AAC1) on the heads of the screws (91) and (96) and on the periphery of the girt bar fittings (92) and (95).
(6) Use the DYNAMOMETER 20 DAN (45 LBF) - PULL to:
Subtask 52-11-11-820-059-B (1) Close the door.
(2) Put the emergency control handle in the ARMED position.
(3) Install the 98DNSA20206060 RIGGING PIN or the 98DNSA20206120 RIGGING PIN on the emergency control handle (rigging point).
NOTE: The 98DNSA20206120 RIGGING PIN is an alternative to the 98DNSA20206060 RIGGING PIN. But, because of its length, you cannot use the 98DNSA20206120 RIGGING PIN at all the locations.
(4) Make sure that clearances F1 and F2 are correct: (a) Clearance F1 must be between 0.2 mm (0.0079 in.) and 0.8 mm (0.0315 in.).
(b) Clearance F2 must be between 0.5 mm (0.0197 in.) and 1.0 mm (0.0394 in.).
(5) If clearances F1 and F2 are not in the tolerances, adjust the girt bar fittings (92) and (95) as follows:
(a) Remove the 98DNSA20206060 RIGGING PIN or the 98DNSA20206120 RIGGING PIN from the emergency control handle (rigging point).
(b) Put the emergency control handle in the DISARMED position.
(c) Open the door and find the position of the serration plates (93) and (94) and the girt bar fittings (92) and (95).
(d) Adjust the position of the girt bar fittings (92) and (95) on the X axis and the Y axis to get correct clearances F1 and F2.
(e) Tighten the screws (91) and (96) on the girt bar fittings (92) and (95).
(f) Apply Polysulfide Sealant-General Purpose Interfay - (Material No.06AAC1) on the heads of the screws (91) and (96) and on the periphery of the girt bar fittings (92) and (95).
(6) Use the DYNAMOMETER 20 DAN (45 LBF) - PULL to:
- Measure the load
- Operate the emergency control handle some times, and
- Make sure that the load necessary to operate the handle is not more than 10 daN (22.48 lbf).
O. Check and Adjustment of the Door Damper and Emergency Operation Cylinder
(1) Put the door in the up closed position against the door frame with the seal compressed.
(2) Make sure that clearance K2 between the telescopic rod (41) and the fitting (42) is 1.5 mm (0.0591 in.) minimum.
Subtask 52-11-11-820-060-A (1) Put the door in the up closed position against the door frame with the seal compressed.
(2) Make sure that clearance K2 between the telescopic rod (41) and the fitting (42) is 1.5 mm (0.0591 in.) minimum.
P. Check and Adjustment of the Compensation Mechanism
(1) Do the load adjustment of the control handle (Ref. AMM TASK 52-11-00-820-002).
Subtask 52-11-11-220-050-A (1) Do the load adjustment of the control handle (Ref. AMM TASK 52-11-00-820-002).
Q. Check of the Outer Control-Handle Locking
(1) Open the door from the outer side of the aircraft and close the door from the inner side of the aircraft.
(2) Make sure that the handle flap (704) comes back to its initial position when you close the door from the outer side of the aircraft.
(3) Apply a manual pressure on the handle flap (704) until it touches the stop (703).
(4) Release the handle flap and make sure that the handle flap (704) goes back to its initial position.
(5) Do this procedure five times.
(6) If necessary, adjust the handle flap (704) as follows:
(a) Loosen the screw (701).
(b) Remove the stop (703) and the adjustable shim (702).
(c) Adjust the adjustable shim (702) to get the correct position of the handle flap (704) when the handle is in the closed position.
(d) Install the stop (703) with the adjustable shim (702) and the screw (701).
(e) Tighten the screw (701).
(f) Do step (3) again.
Subtask 52-11-11-820-065-A (1) Open the door from the outer side of the aircraft and close the door from the inner side of the aircraft.
(2) Make sure that the handle flap (704) comes back to its initial position when you close the door from the outer side of the aircraft.
(3) Apply a manual pressure on the handle flap (704) until it touches the stop (703).
(4) Release the handle flap and make sure that the handle flap (704) goes back to its initial position.
(5) Do this procedure five times.
(6) If necessary, adjust the handle flap (704) as follows:
(a) Loosen the screw (701).
(b) Remove the stop (703) and the adjustable shim (702).
(c) Adjust the adjustable shim (702) to get the correct position of the handle flap (704) when the handle is in the closed position.
(d) Install the stop (703) with the adjustable shim (702) and the screw (701).
(e) Tighten the screw (701).
(f) Do step (3) again.
R. Check of the Emergency Escape-Slide Control-Handle Disarming
(1) Close the door.
(2) Put the emergency control handle in the ARMED position.
(3) Open the door from the outer side of the aircraft.
(4) Make sure that the emergency escape slide moves to the DISARMED position.
Subtask 52-11-11-820-061-A (1) Close the door.
(2) Put the emergency control handle in the ARMED position.
(3) Open the door from the outer side of the aircraft.
(4) Make sure that the emergency escape slide moves to the DISARMED position.
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.
S. Check of the Door Handle Lock in the Up Position (1) Make sure that, during the opening of the door, the handle locks before the release of the guide rollers from the guide fittings.
(2) Make sure that, when you close the door with the inner control handle (805), you feel no hard points because of the non-retraction of the hook (804).
(3) If necessary, do the adjustment that follows:
(a) Removal of the lockwire:
1 Remove and discard the lockwire from the nuts (801) and (803).
(b) Decrease the rod length (802) until there is no hard point because of the non-retraction of the hook (804) (when you close the door in the up position).
(c) Tighten the nuts (801) and (803).
(d) Safety the nuts (801) and (803) with the
(e) Put the door in the up position and make sure that you can correctly install the 98DNSA20206060 RIGGING PIN or the 98DNSA20206120 RIGGING PIN.
NOTE: The 98DNSA20206120 RIGGING PIN is an alternative to the 98DNSA20206060 RIGGING PIN. But, because of its length, you cannot use the 98DNSA20206120 RIGGING PIN at all the locations.
(4) If you feel the hard point again, apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the mating surface of the hook (804) with the handle (805). T. Check of the Pre-load of the Cover Plate
(1) After you replace the door with a new door, do a check of the pre-load of the cover plate (Ref. AMM TASK 52-10-00-220-007).
Subtask 52-11-11-820-068-A (1) After you replace the door with a new door, do a check of the pre-load of the cover plate (Ref. AMM TASK 52-10-00-220-007).
NOTE: After the adjustment of the door, you can possibly see a permitted bend line on the cover plate.
U. Check and Adjustment of the Proximity Switch
(1) Do the adjustment of proximity switch 11WV1 or 11WV2 of the door locking mechanism (Ref. AMM TASK 52-71-00-820-001).
Subtask 52-11-11-730-050-A ** ON A/C NOT FOR ALL (1) Do the adjustment of proximity switch 11WV1 or 11WV2 of the door locking mechanism (Ref. AMM TASK 52-71-00-820-001).
V. Adjustment/Test of the Components
(1) Adjust the forward passenger/crew door (Ref. AMM TASK 52-11-00-820-001).
(2) Adjust the emergency escape-slide release-mechanism (Ref. AMM TASK 52-11-22-820-001).
(3) Do an operational test of the door warning system (Ref. AMM TASK 52-71-00-710-001).
Subtask 52-11-11-730-050-B ** ON A/C NOT FOR ALL (1) Adjust the forward passenger/crew door (Ref. AMM TASK 52-11-00-820-001).
(2) Adjust the emergency escape-slide release-mechanism (Ref. AMM TASK 52-11-22-820-001).
(3) Do an operational test of the door warning system (Ref. AMM TASK 52-71-00-710-001).
V. Adjustment/Test of the Components
(1) Adjust the forward passenger/crew door (Ref. AMM TASK 52-11-00-820-001).
(2) Adjust the emergency escape-slide raft release-mechanism (Ref. AMM TASK 52-11-22-820-001).
(3) Do an operational test of the door warning system (Ref. AMM TASK 52-71-00-710-001).
5. Close-up(1) Adjust the forward passenger/crew door (Ref. AMM TASK 52-11-00-820-001).
(2) Adjust the emergency escape-slide raft release-mechanism (Ref. AMM TASK 52-11-22-820-001).
(3) Do an operational test of the door warning system (Ref. AMM TASK 52-71-00-710-001).
Subtask 52-11-11-865-051-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 52-11-11-410-051-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C 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 |
B. Installation of the Components
(1) Install the removed cover light panels (Ref. AMM TASK 25-23-48-400-001).
(a) Refer to AMM chapter 06 for the cover light-panels details (Ref. AMM D/O 06-41-53-00).
(2) Install the applicable upper sidewall-panels (Ref. AMM TASK 25-23-43-400-001).
(a) Refer to AMM chapter 06 for the upper sidewall-panels details (Ref. AMM D/O 06-41-53-00).
(3) Install the applicable lower sidewall-panels (Ref. AMM TASK 25-23-44-400-001).
(a) Refer to AMM chapter 06 for the lower sidewall-panels details (Ref. AMM D/O 06-41-53-00).
(4) Remove the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR or the escape slide if you kept it in position (as an alternative to the ballast weight):
(a) For the left door (Ref. AMM TASK 52-10-00-480-001) or (Ref. AMM TASK 25-62-44-000-002)
(b) For the right door (Ref. AMM TASK 52-10-00-480-001) or (Ref. AMM TASK 25-62-44-000-802).
(5) Install the door insulation blankets (Ref. AMM TASK 25-80-00-400-001).
(6) Install the removed door lining-panels (Ref. AMM TASK 25-23-46-400-001).
(a) Refer to AMM chapter 06 for the door lining-panels details (Ref. AMM D/O 06-41-52-00).
(7) Install the removed door-frame lining panels (Ref. AMM TASK 25-23-45-400-006) or (Ref. AMM TASK 25-23-45-400-007).
(a) Refer to AMM chapter 06 for the door-frame lining panels details (Ref. AMM D/O 06-41-53-00).
(8) Install the lining flap (Ref. AMM TASK 52-11-31-400-001).
(9) Install the escape-slide pack-assembly:
(a) For the left door (Ref. AMM TASK 25-62-44-400-006)
(b) For the right door (Ref. AMM TASK 25-62-44-400-802).
Subtask 52-11-11-410-051-C ** ON A/C NOT FOR ALL (1) Install the removed cover light panels (Ref. AMM TASK 25-23-48-400-001).
(a) Refer to AMM chapter 06 for the cover light-panels details (Ref. AMM D/O 06-41-53-00).
(2) Install the applicable upper sidewall-panels (Ref. AMM TASK 25-23-43-400-001).
(a) Refer to AMM chapter 06 for the upper sidewall-panels details (Ref. AMM D/O 06-41-53-00).
(3) Install the applicable lower sidewall-panels (Ref. AMM TASK 25-23-44-400-001).
(a) Refer to AMM chapter 06 for the lower sidewall-panels details (Ref. AMM D/O 06-41-53-00).
(4) Remove the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR or the escape slide if you kept it in position (as an alternative to the ballast weight):
(a) For the left door (Ref. AMM TASK 52-10-00-480-001) or (Ref. AMM TASK 25-62-44-000-002)
(b) For the right door (Ref. AMM TASK 52-10-00-480-001) or (Ref. AMM TASK 25-62-44-000-802).
(5) Install the door insulation blankets (Ref. AMM TASK 25-80-00-400-001).
(6) Install the removed door lining-panels (Ref. AMM TASK 25-23-46-400-001).
(a) Refer to AMM chapter 06 for the door lining-panels details (Ref. AMM D/O 06-41-52-00).
(7) Install the removed door-frame lining panels (Ref. AMM TASK 25-23-45-400-006) or (Ref. AMM TASK 25-23-45-400-007).
(a) Refer to AMM chapter 06 for the door-frame lining panels details (Ref. AMM D/O 06-41-53-00).
(8) Install the lining flap (Ref. AMM TASK 52-11-31-400-001).
(9) Install the escape-slide pack-assembly:
(a) For the left door (Ref. AMM TASK 25-62-44-400-006)
(b) For the right door (Ref. AMM TASK 25-62-44-400-802).
B. Installation of the Components
(1) Install the removed cover light-panels (Ref. AMM TASK 25-23-48-400-001).
(a) Refer to AMM chapter 06 for the cover light-panels details (Ref. AMM D/O 06-41-53-00).
(2) Install the removed upper sidewall-panels (Ref. AMM TASK 25-23-43-400-001).
(a) Refer to AMM chapter 06 for the upper sidewall-panels details (Ref. AMM D/O 06-41-53-00).
(3) Install the removed lower sidewall-panels (Ref. AMM TASK 25-23-44-400-001).
(a) Refer to AMM chapter 06 for the lower sidewall-panels details (Ref. AMM D/O 06-41-53-00).
(4) Remove the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR or the escape slide if you kept it in position (as an alternative to the ballast weight):
(a) For the left door (Ref. AMM TASK 52-10-00-480-001) or (Ref. AMM TASK 25-62-44-000-012)
(b) For the right door (Ref. AMM TASK 52-10-00-480-001) or (Ref. AMM TASK 25-62-44-000-804).
(5) Install the door insulation blankets (Ref. AMM TASK 25-80-00-400-001).
(6) Install the removed door lining-panels (Ref. AMM TASK 25-23-46-400-001).
(a) Refer to AMM chapter 06 for the door lining-panels details (Ref. AMM D/O 06-41-52-00).
(7) Install the removed door-frame lining panels (Ref. AMM TASK 25-23-45-400-006) or (Ref. AMM TASK 25-23-45-400-007).
(a) Refer to AMM chapter 06 for the door-frame lining panels details (Ref. AMM D/O 06-41-53-00).
(8) Install the lining flap (Ref. AMM TASK 52-11-31-400-001).
(9) Install the escape slide-raft pack-assembly:
(a) For the left door (Ref. AMM TASK 25-62-44-400-007)
(b) For the right door (Ref. AMM TASK 25-62-44-400-803).
Subtask 52-11-11-410-054-A (1) Install the removed cover light-panels (Ref. AMM TASK 25-23-48-400-001).
(a) Refer to AMM chapter 06 for the cover light-panels details (Ref. AMM D/O 06-41-53-00).
(2) Install the removed upper sidewall-panels (Ref. AMM TASK 25-23-43-400-001).
(a) Refer to AMM chapter 06 for the upper sidewall-panels details (Ref. AMM D/O 06-41-53-00).
(3) Install the removed lower sidewall-panels (Ref. AMM TASK 25-23-44-400-001).
(a) Refer to AMM chapter 06 for the lower sidewall-panels details (Ref. AMM D/O 06-41-53-00).
(4) Remove the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR or the escape slide if you kept it in position (as an alternative to the ballast weight):
(a) For the left door (Ref. AMM TASK 52-10-00-480-001) or (Ref. AMM TASK 25-62-44-000-012)
(b) For the right door (Ref. AMM TASK 52-10-00-480-001) or (Ref. AMM TASK 25-62-44-000-804).
(5) Install the door insulation blankets (Ref. AMM TASK 25-80-00-400-001).
(6) Install the removed door lining-panels (Ref. AMM TASK 25-23-46-400-001).
(a) Refer to AMM chapter 06 for the door lining-panels details (Ref. AMM D/O 06-41-52-00).
(7) Install the removed door-frame lining panels (Ref. AMM TASK 25-23-45-400-006) or (Ref. AMM TASK 25-23-45-400-007).
(a) Refer to AMM chapter 06 for the door-frame lining panels details (Ref. AMM D/O 06-41-53-00).
(8) Install the lining flap (Ref. AMM TASK 52-11-31-400-001).
(9) Install the escape slide-raft pack-assembly:
(a) For the left door (Ref. AMM TASK 25-62-44-400-007)
(b) For the right door (Ref. AMM TASK 25-62-44-400-803).
C. Close Access
(1) Obey the special precautions after the work on the door (Ref. AMM TASK 52-10-00-860-001).
(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 forward passenger/crew door 841 or 842 (Ref. AMM TASK 52-10-00-410-001).
(5) Remove the access platform(s).
Subtask 52-11-11-862-051-A (1) Obey the special precautions after the work on the door (Ref. AMM TASK 52-10-00-860-001).
(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 forward passenger/crew door 841 or 842 (Ref. AMM TASK 52-10-00-410-001).
(5) Remove the access platform(s).