W DOC AIRBUS | AMM A320F

Adjustment of the Forward Passenger/Crew Door

TASK 52-11-00-820-001-A
Adjustment of the Forward Passenger/Crew Door

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 831
ZONE: 841
1. Reason for the Job
To adjust the door immediately after you replace it or the door components, or if there is a report related to a door defect.
NOTE: The values given in this procedure are not applicable to general inspections and checks.
NOTE: You can do this task with the aircraft on jacks or on wheels.
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
SAFETY CLIP - CIRCUIT BREAKER
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 ) T
No specific
Torque wrench: range to between 0.748 and 0.612 m.daN (66.19 and 54.16 lbf.in ) T
No specific
Torque wrench: range to between 1.35 and 1.2 m.daN (119.47 and 106.19 lbf.in ) T
No specific
Torque wrench: range to between 1.5 and 1.25 m.daN (132.74 and 110.62 lbf.in ) T
No specific
Torque wrench: range to between 2.2 and 2 m.daN (16.22 and 14.75 lbf.ft ) T
98D52103501000
1
BALLAST WEIGHT - PASSENGER CREW DOOR
98DNSA20206060
1
RIGGING PIN
OR
OR
98DNSA20206120
1
RIGGING PIN
 B. Consumable Materials
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 -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
831
FORWARD PASSENGER/CREW DOOR
841
FORWARD PASSENGER/CREW DOOR
221AW, 221BW, 221CW, 221EW, 221FW, 221RW, 221SW, 221VW, 222RW, 222SW, 222TW, 222UW, 222VW, 231AW, 231CW, 232AW, 232CW, 831, 831AZ, 831BZ, 831CZ, 831DZ, 831EZ, 831FZ, 831GZ, 841, 841AZ, 841BZ, 841CZ, 841DZ, 841EZ, 841FZ, 841GZ
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
13
COTTER PIN
AIPC 52-11-01-04-150
208
COTTER PIN
AIPC 52-11-01-05-040
53
LOCK PLATE
AIPC 52-11-11-21-040
13
COTTER PIN
AIPC 52-11-81-02-150
208
COTTER PIN
AIPC 52-11-81-03-700
53
LOCK PLATE
AIPC 52-11-81-17-040
47
COTTER PIN
AIPC 53-16-01-23-020
47
COTTER PIN
AIPC 53-16-81-23-100
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
TASK 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
TASK 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 25-23-46-000-001-A
Removal of the Door Linings from the Forward Passenger/Crew Doors
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 52-10-00-010-001-A
Opening of the Passenger/Crew Door
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 52-10-00-860-002-A
Special Precautions after Work on the 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 52-11-14-820-002-A
Adjustment of the Percussion Bellcrank Finger of the Door Damper and Emergency Operation Cylinder of the FWD Passenger/Crew Door
TASK 52-11-31-000-001-A
Removal of the Lining Flap
TASK 52-11-31-000-002-A
Removal of the Stop Fittings, Buffer, Guide Fittings, Rollers, Door Stop Fittings, Roller Fittings and Guide Arm Fittings
TASK 52-11-31-400-001-A
Installation of the Lining Flap
TASK 52-11-31-400-002-A
Installation of the Stop Fittings, the Buffer, the Guide Fittings, the Rollers, the Door Stop Fittings, the Roller Fittings and the Guide Arm Fittings
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)
F Adjustment of the Door Stop Fittings of the Forward Passenger/Crew Door
F Adjustment of the Upper and Lower Guide Fittings of the Forward Passenger/Crew Door
F Adjustment of the Girt Bar and Load on the Inner Control Handle of the Forward Passenger/Crew Door
F Adjustment of the Girt Bar Fittings of the Forward Passenger/Crew Door
F Adjustment on the X Axis of the Forward Passenger/Crew Door
F Adjustment of the Y Axis and Stops of the Forward Passenger/Crew Door
F Clearances - Adjustment on the Z Axis of the Forward Passenger/Crew Door
F Adjustment of the Upper Hook of the Forward Passenger/Crew Door
F Adjustment of the Safety Pin of the Forward Passenger/Crew Door
F Adjustment of the Upper and Lower Guide Arms of the Forward Passenger/Crew Door
F Upper and Lower Guide Arms - Adjustment on the X Axis
F Adjustment of the Buffer of the Forward Passenger/Crew Door
F Adjustment of the Outer Control Handle of the Forward Passenger/Crew Door ** ON A/C NOT FOR ALL
F Adjustment of the Outer Control Handle of the Forward Passenger/Crew Door ** ON A/C NOT FOR ALL
F Adjustment of the Outer Control-Handle of the Handle Stop ** ON A/C NOT FOR ALL
F Adjustment of the Inner Contol Handle of the Forward Passenger/Crew Door
3. Job Set-up
Subtask 52-11-00-861-050-A
A. Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).
Subtask 52-11-00-010-061-A
B. Get Access
WARNING: DO NOT OPEN THE PASSENGER/CREW DOOR IF THE WIND SPEED IS MORE THAN 65 KNOTS.
WARNING: BEFORE YOU START WORK ON THE DOOR, MAKE SURE THAT:
  • THE EMERGENCY CONTROL HANDLE IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
  • THE PERCUSSION LEVER OF THE DOOR-DAMPER AND EMERGENCY-OPERATION CYLINDER IS IN THE DISARMED POSITION WITH THE SAFETY PIN INSTALLED.
IF YOU DO NOT OBEY THESE INSTRUCTIONS, THE DOOR CAN OPEN WITH FORCE OR THE ESCAPE SLIDE CAN DEPLOY SUDDENLY. THIS CAN CAUSE INJURY AND/OR DAMAGE.
WARNING: STOP THE OPENING PROCEDURE IF THE RED WARNING LIGHT FLASHES. IF THE RED WARNING LIGHT FLASHES, REMAINING PRESSURE CAN CAUSE THE DOOR TO OPEN SUDDENLY AND CAN:
  • KILL OR CAUSE SERIOUS INJURY TO PERSONS
  • CAUSE DAMAGE TO THE AIRCRAFT.
   (1) Put the ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE in position in front of passenger/crew door 831 or 841.
   (2) Open the applicable passenger/crew door (Ref. AMM TASK 52-10-00-010-001).
   (3) Obey the special precautions before you start the work on the door (Ref. AMM TASK 52-10-00-860-001).
Subtask 52-11-00-865-052-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUEIS/SLIDES/ARM AND WARN/FLT15WNP11
121VUEIS/SLIDES/ARM AND WARN/GND13WNP10
121VUEIS/SDAC1 AND 2/DOOR/DET/PAX48WVP05
Subtask 52-11-00-010-052-A ** ON A/C NOT FOR ALL
D. Removal of the Components
   (1) Remove the lining flap (Ref. AMM TASK 52-11-31-000-001).
   (2) Remove the escape-slide pack-assembly:
     (a) For the left door:
If installed, remove the left escape-slide pack-assembly (Ref. AMM TASK 25-62-44-000-002).
     (b) For the right door:
If installed, remove the right escape-slide pack-assembly (Ref. AMM TASK 25-62-44-000-802).
   (3) Remove the door lining panels (Ref. AMM TASK 25-23-46-000-001):
     (a) For the left door: 831FZ, 831CZ, 831DZ, 831AZ, 831BZ, 831EZ and 831GZ
     (b) For the right door: 841FZ, 841CZ, 841DZ, 841AZ, 841BZ, 841EZ and 841GZ.
Subtask 52-11-00-010-052-B ** ON A/C NOT FOR ALL
D. Removal of Components
   (1) Remove the lining flap (Ref. AMM TASK 52-11-31-000-001).
   (2) Remove the escape slide:
     (a) For the left door:
If installed, remove the left-hand escape slide raft pack assembly (Ref. AMM TASK 25-62-44-000-012).
     (b) For the right door:
If installed, remove the right-hand escape slide raft pack assembly (Ref. AMM TASK 25-62-44-000-804).
   (3) Remove the door lining panels (Ref. AMM TASK 25-23-46-000-001):
     (a) For the left door: 831FZ 831CZ 831DZ 831AZ 831BZ 831EZ 831GZ.
     (b) For the right door: 841FZ 841CZ 841DZ 841AZ 841BZ 841EZ 841GZ.
Subtask 52-11-00-010-066-B
E. Removal of the Door-Frame Lining Panels
   (1) Remove the door-frame lining panels:
     (a) For the left door: 221AW, 221BW, 221CW, 221EW, 221FW, 221VW, 221SW and 221RW (Ref. AMM TASK 25-23-45-000-005)
     (b) For the right door: 222RW, 222SW, 222TW, 222UW and 222VW (Ref. AMM TASK 25-23-45-000-002).
   (2) Remove the door insulation blankets.
   (3) Remove lower sidewall panels 231AW and 232AW (Ref. AMM TASK 25-23-44-000-001).
   (4) Remove cove light panels 231CW and 232CW (Ref. AMM TASK 25-23-48-000-001).
Subtask 52-11-00-420-053-A ** ON A/C NOT FOR ALL
F. Installation of the Ballast Weight
   (1) Install the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR on the 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 as an alternative during the adjustment.
   (2) If you use the escape-slide pack-assembly alternative, make sure that it lets you have access to the door for the adjustment procedure.
Subtask 52-11-00-420-053-B ** ON A/C NOT FOR ALL
F. Installation of the Ballast Weight
   (1) Install the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR on the door (Ref. AMM TASK 52-10-00-480-001).
NOTE: If no ballast weight is available, it is permitted to use the escape slide or raft on the door as an alternative during the adjustment.
   (2) If you use the escape slide or raft alternative, make sure that it lets you have access to the door for the adjustment procedure.
4. Procedure
Subtask 52-11-00-820-050-C
A. Adjustment of the Door during its Opening and Closure
F Adjustment of the Door Stop Fittings of the Forward Passenger/Crew Door
F Adjustment of the Upper and Lower Guide Fittings of the Forward Passenger/Crew Door
F Adjustment of the Girt Bar and Load on the Inner Control Handle of the Forward Passenger/Crew Door
   (1) Make sure that there is no damage and cracks on the door stops (21):
     (a) If you find damage on one or more door stop(s) (21), replace (it)them in six flight cycles or less (Ref. AMM TASK 52-11-31-000-002) and (Ref. AMM TASK 52-11-31-400-002).
     (b) If you find damage on more than two door stop(s) (21), replace (it)them (Ref. AMM TASK 52-11-31-000-002) and (Ref. AMM TASK 52-11-31-400-002).
     (c) If you find cracks on one or more door stop(s) (21), replace (it)them (Ref. AMM TASK 52-11-31-000-002) and (Ref. AMM TASK 52-11-31-400-002).
   (2) Make sure that when you open the door, clearance H1 between the door stops (21) and the door frame stops (22) is 5 mm (0.1969 in.) minimum.
   (3) Slowly close the door and make sure that there is no hard point between the door stops (21) and the door frame stops (22).
   (4) Make sure that clearance H2 is 0.2 mm (0.0079 in.) minimum with overlap H3 between 3 mm (0.1181 in.) and 4 mm (0.1575 in.).
   (5) Make sure that the guide rollers (31) touch the guide fittings (32) and (36).
   (6) If clearance H2 is not in the tolerance, adjust the upper and lower guide fittings (32) and (36) as follows:
     (a) Open the door.
     (b) Find the position of the serration plates (37) and (38) and the upper and lower guide fittings (32) and (36).
     (c) Loosen the screws (40).
     (d) Move the guide fittings (32) and (36) to get clearance H2.
     (e) Make sure that the eccentric washers (39):
  • Fully seal the holes of the guide fittings (32) and (36)
  • Are not above the rounded areas or the spot-facing edges
  • Are not out of the outer contour of the fitting.
     (f) Temporarily tighten the screws (40).
     (g) Close the door.
   (7) Open the door.
   (8) Make sure that when you open the door (during the door lifting travel), clearance F3 is 5 mm (0.1969 in.) minimum between the ends of the telescopic fork(s) (2) and the girt bar fittings (1).
   (9) If clearance F3 is not in the tolerance, adjust the girt bar fittings (92) and (95) as follows:
F Adjustment of the Girt Bar Fittings of the Forward Passenger/Crew Door
     (a) Loosen the screws (91) and (96) of the girt bar fittings (92) and (95).
     (b) Remove the sealant from the girt bar fittings (92) and (95) and the heads of the screws (91)and (96). For this, use Non Aqueous Cleaner-General - - (Material No.08BAA9) with the Textile-Lint free Cotton - (Material No.14SBA1) .
     (c) Find the position of the serrations of the girt bar fittings (92) and (95) and the plates (93) and (94).
     (d) Move the girt bar fittings (92) and (95) from the serrations on the X and Y axes to get the correct clearance.
Subtask 52-11-00-820-052-A
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.
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.
B. Adjustment of the Door in the Down Position
F Adjustment on the X Axis of the Forward Passenger/Crew Door
F Adjustment of the Y Axis and Stops of the Forward Passenger/Crew Door
F Clearances - Adjustment on the Z Axis of the Forward Passenger/Crew Door
   (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, adjust the door on the X axis as follows:
     (a) Close and lock the door.
     (b) Disconnect the upper and lower connection links (11) from each side of the yoke.
     (c) Remove and discard the cotter pin (13).
     (d) Remove the nuts (14), the washers (15) and the bolts (16) to disconnect the upper and lower connection links (11).
     (e) Adjust the door on the X axis with the thickness of the washers (12).
     (f) Make sure that clearance B is less than or equal to 0.1 mm (0.0039 in.).
NOTE: The thickness of the two washers (12) at the lower and upper connection links (11) is equal to the nominal thickness.
     (g) Make sure that clearance B is in the tolerance.
     (h) Connect the upper and lower connection links (11) to each side of the yoke.
     (i) Install the washers (15) and the bolts (16).
     (j) Install the nuts (14).
     (k) TORQUE the nuts (14) to between 1.35 and 1.2 m.daN (119.47 and 106.19 lbf.in ) T.
   (3) Make sure that clearance E8 is 70 +0.7 mm or -0.7 mm (2.7559 +0.0276 in. or -0.0276 in.).
   (4) Do a check of the peripheral clearance between the door and the door frame:
     (a) At FR16, make sure that peripheral clearance E1 is 4 +1 mm or -1 mm (0.1575 +0.0394 in. or -0.0394 in.).
     (b) At FR20, make sure that peripheral clearance E2 is 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 for a maximum length of 400 mm (15.7480 in.).
This maximum total length can be the sum of smaller lengths in a maximum of three locations.
     (c) Make sure that peripheral clearance E3 is 4 +1.5 mm or -2.5 mm (0.1575 +0.0591 in. or -0.0984 in.).
   (5) Do a check of the flushness between the door and the door frame at door stop levels L1 thru L7:
     (a) Make sure that 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 for a maximum length of 400 mm (15.7480 in.).
This maximum total length can be the sum of smaller lengths in a maximum of three locations.
   (6) Make sure that overlap E6 of the stop axis is:
     (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.).
   (7) Make sure that clearance E7 is 0 +1 mm or -1 mm (0.0000 +0.0394 in. or -0.0394 in.).
   (8) Make sure that clearance E9 is 4.5 +2 mm or -2 mm (0.1772 +0.0787 in. or -0.0787 in.) compresses the seal.
   (9) When you open the door, make sure that clearance E10 between the stop and the door frame is 5 mm (0.1969 in.).
   (10) If clearances E1, E2, E6 and E10 on the X axis are not in the tolerances, change the door position as follows:
     (a) Disconnect the upper and lower connection links (11) from each side of the yoke.
     (b) Remove the nuts (14), the washers (13) and the bolts (16) to disconnect the upper and lower connection links.
     (c) Adjust the door on the X axis with the thickness of the washers (12).
     (d) Make sure that clearance B is less than or equal to 0.1 mm (0.0039 in.).
NOTE: The thickness of the two washers (12) at the lower and upper connection links (11) is equal to the nominal thickness.
     (e) Make sure that clearance B is in the tolerance.
     (f) Connect the upper and lower connection links (11) to each side of the yoke.
     (g) Install the washers (15) and the bolts (16).
     (h) Install the nuts (14).
     (i) TORQUE the nuts (14) to between 1.35 and 1.2 m.daN (119.47 and 106.19 lbf.in ) T.
     (j) Install the new AIPC 52-11-01-04-150 COTTER PIN (13) or the new AIPC 52-11-81-02-150 COTTER PIN (13).
   (11) If clearances E5 and E9 on the Y axis are not in the tolerances, change the door position as follows:
F Adjustment of the Y Axis and Stops of the Forward Passenger/Crew Door
     (a) Remove the nuts (52) and the lock plate (53).
     (b) Adjust the stop screws (51) to make sure that:
       1 Clearance J1 between the stop and the door frame is 0 +0 mm or +0.5 mm (0.0000 +0.0000 in. or +0.0197 in.).
       2 Dimension J2 is 6 mm (0.2362 in.) maximum.
       3 Three stop screws (51) touch the door frame with:
  • Stop screws (51) on one side of the frame, and
  • Stop screw (51) on the opposite side of the frame.
     (c) Make sure that clearances E5 and E9 are correct.
     (d) Install the nuts (52) with the new AIPC 52-11-11-21-040 LOCK PLATE (53) or the new AIPC 52-11-81-17-040 LOCK PLATE (53).
     (e) TORQUE the nuts (52) to between 2.2 and 2 m.daN (16.22 and 14.75 lbf.ft ) T.
     (f) Fold the lugs of the lock plate (53).
     (g) Make sure that the lugs of the lock plate (53) are fully folded against the stop fittings.
   (12) If clearances E3 and E7 on the Z axis are not in the tolerances, change the door position as follows:
F Clearances - Adjustment on the Z Axis of the Forward Passenger/Crew Door
     (a) Cut the lockwire from the nuts (61) and (63) and discard it.
     (b) Loosen the nuts (61) and (63).
     (c) Adjust the length of the rod (62) until you get the correct configuration.
     (d) Tighten the nuts (61) and (63).
     (e) Safety the rod (62) with the 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
     (f) Make sure that clearances E3 and E7 are correct.
   (13) Remove the TEMPLATE 70 MM (2,75 IN) from the frame.
Subtask 52-11-00-820-053-B
C. Check and Adjustment of Clearances between the Rollers and the Guide Fittings
F Adjustment of the Upper and Lower Guide Fittings of the Forward Passenger/Crew Door
   (1) Operate the door for some time.
   (2) With the door in the up position, make sure that:
     (a) The guide rollers (31) move off the guide fittings (32) and (36) 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 clearances C1 and C2 are not in the tolerances, adjust the guide fittings (32) and (36) as follows:
     (a) Open the door.
     (b) Find the position of the serrations of the plates (37) and (38) on the upper and lower guide fittings (32) and (36).
     (c) Loosen the screws (40) and move the guide fittings (32) and (36) to get correct clearances C1 and C2.
     (d) Make sure that the eccentric washers (39):
  • Fully seal the holes of the guide fittings (32) and (36)
  • Are not above the rounded areas or the spot-facing edges
  • Are not out of the outer contour of the fitting.
     (e) Temporarily tighten the screws (40).
   (4) With the door in the down position, make sure that:
     (a) The guide rollers (31) of the guide fittings (36) turn freely.
     (b) The guide rollers (31) of the guide fittings (32) turn freely or touch the bolts (35).
     (c) Clearance C4 is between 0.2 mm (0.0079 in.) and 1.5 mm (0.0591 in.).
     (d) Clearance C3 is 0.2 mm (0.0079 in.) minimum.
     (e) 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.
     (f) If clearances C3 and C4 are not in the tolerances, adjust the upper and lower guide fittings (32) and (36).
   (5) If the bolts (35) and/or the upper guide fitting (32) were(was) replaced, do the adjustment that follows:
     (a) Open the door.
     (b) Remove the nuts (34), the adjustable washers (33) and the bolts (35).
     (c) Install the bolts (35) and the nuts (34).
     (d) Close the door and measure the dimension between the guide rollers (31) and the bolts (35).
     (e) Open the door.
     (f) Remove the nuts (34) and the bolts (35).
     (g) Adjust the thickness of the adjustable washers (33).
     (h) Install the adjustable washers (33), the bolts (35) and the nuts (34) and tighten them.
Subtask 52-11-00-820-054-B
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.
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.
D. Check and Adjustment on the Z Axis of the Door and Locking Hook Adjustment
F Adjustment of the Upper and Lower Guide Fittings of the Forward Passenger/Crew Door
F Adjustment of the Upper Hook of the Forward Passenger/Crew Door
   (1) Close the door.
   (2) When the SHIM THICKNESS 0.2 MM (0.008 IN) is between the bolts (35) and the guide rollers (31) make sure that:
  • The locking hook (41) touches the roller (40), and
  • Clearance M1 is 0.5 +0.3 mm or -0.3 mm (0.0197 +0.0118 in. or -0.0118 in.).
   (3) If no component touches the locking hook (41), do the adjustment that follows:
     (a) Put the two shims in position in the upper guide fittings (32).
     (b) Close the door.
     (c) Cut and discard the lockwire from the nuts (42).
     (d) Loosen the nuts (42) and release the lock washers (43).
     (e) Loosen the clamp (45).
     (f) Turn the barrel of the rod (44) until the locking hook (41) and the roller (40) touch.
     (g) Tighten the nuts (42) and the clamp (45).
     (h) Make sure that the lock washers (43) are in the correct position.
     (i) Safety the nuts (42) and the lock washers (43) with the 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
     (j) Open the door and remove the two shims.
   (4) If clearance M1 is not in the tolerance, do the adjustment that follows:
     (a) Put the two shims in position in the upper guide fittings (32).
     (b) Close the door.
     (c) Cut and discard the lockwire from the nuts (42).
     (d) Loosen the nuts (42) and release the lock washers (43).
     (e) Loosen the clamp (45).
     (f) Turn the rod (44) one turn to make it shorter.
     (g) Remove and discard the cotter pin (47).
     (h) Remove the nut (46).
     (i) Pull the bush (48) out by 4 mm (0.1575 in.) to disengage it from the stop flat (50).
     (j) Turn the bush (48) to the necessary correction value:
  • 0.9, -0.6, +0.6, +1.5 or +1.2.
     (k) Make sure that the bush (48) stays engaged with its slots in the eccentric yoke (49).
NOTE: The slotted drive between the bush (48) and the eccentric yoke (49) has a foolproofing device (one position only).
     (l) Push the bush (48) until the correction value aligns with the mark on the stop flat (50).
     (m) Install the nut (46).
     (n) TORQUE the nut (46) to between 1.5 and 1.25 m.daN (132.74 and 110.62 lbf.in ) T.
     (o) Turn the barrel of the rod (44) until the locking hook (41) and the roller (40) touch.
     (p) Install the new AIPC 53-16-01-23-020 COTTER PIN (47) or the new AIPC 53-16-81-23-100 COTTER PIN (47).
     (q) Tighten the nuts (42) and the clamp (45).
     (r) Make sure that the lock washers (43) are in the correct position.
     (s) Safety the nuts (42) and the lock washers (43) with the 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
     (t) Open the door and remove the two shims.
   (5) Make sure that the roller (40) turns freely when the door is closed.
Subtask 52-11-00-820-055-A
E. Adjustment of the Safety Pin
F Adjustment of the Safety Pin of the Forward Passenger/Crew Door
   (1) Close the door.
   (2) Make sure that clearance G1 between the fitting (71) and the safety pin (72) 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 as follows:
     (a) Open the door.
     (b) Remove the stop screw (74) and the adjustment washers (73).
     (c) Install the new adjustable washers (73) to get clearance G1.
     (d) Apply Threadlocking Adhesive-- Medium strength - (Material No.05BAE1) on the thread of the stop screw (74).
     (e) Install the stop screw (74).
     (f) Torque the stop screw (74) to between 0.7 and 0.6 m.daN (61.95 and 53.10 lbf.in ) T.
Subtask 52-11-00-820-056-C
F. Check of the Adjustment of the Upper and Lower Guide Arms
F Adjustment of the Upper and Lower Guide Arms of the Forward Passenger/Crew Door
   (1) Adjustment on the X axis:
F Upper and Lower Guide Arms - Adjustment on the X Axis
     (a) For the door that has the door damper and emergency operation cylinder (series Part Numbers (P/N) FE174 and FE196).
       1 Put the door in the up-closed position to make it touch the seal.
     (b) For the door that has the door damper and emergency operation cylinder (series P/N FE240).
       1 Put the door in the up-closed position to make it touch the seal at FR20.
         a Do a check of clearance L1 at FR16.
         b Measure the clearance at door stop level L5.
         c Make sure that clearance L1 is equal to the difference between flushness D1 (measured between the door and the frame of the forward door) and flushness D2 (measured between the door and the frame of the aft door).
         d Clearance L1 is 5 mm (0.1969 in.).
     (c) Make sure that the bolts (88) at the guide arm and the door attachment do not have too much tension.
     (d) If they have too much tension, do an adjustment of the upper guide arm (87) and lower guide arm (84) as follows:
       1 Find the position of the serrations of the plates (82) and (85).
       2 Loosen the nuts (81) and (89).
       3 Move the fittings (83) and (86) on the X axis to get the correct position.
       4 Make sure that the eccentric washers (80) and (90):
  • Fully seal the holes of the fittings (83) and (86)
  • Are not above the rounded areas or the spot-facing edges
  • Are not out of the outer contour of the fitting.
       5 Temporarily tighten the nuts (81) and (89).
   (2) Adjustment on the Y axis:
     (a) Open the door until the nominal axis of the guide arms and the support arms align.
     (b) Make sure that the bolts (88) at the guide arm and the door attachment do not have too much tension.
     (c) If they have too much tension, do an adjustment of the upper guide arm (87) and lower guide arm (84) as follows:
       1 Find the position of the serrations of the plates (82) and (85).
       2 Loosen the nuts (81) and (89).
       3 Move the fittings (83) and (86) on the Y axis to get the correct position.
       4 Make sure that the eccentric washers (80) and (90):
  • Fully seal the holes of the fittings (83) and (86)
  • Are not above the rounded areas or the spot-facing edges
  • Are not out of the outer contour of the fitting.
       5 Tighten the nuts (81) and (89).
Subtask 52-11-00-820-057-A
G. Adjustment of the Escape Slide and the Girt Bar Fittings
F Adjustment of the Girt Bar and Load on the Inner Control Handle of the Forward Passenger/Crew Door
F Adjustment of the Girt Bar Fittings of the Forward Passenger/Crew Door
   (1) Put the door in the closed position.
   (2) Put the emergency control handle in the ARMED position.
   (3) Install the 98DNSA20206060 RIGGING PIN98DNSA20206120 RIGGING PIN on the emergency control handle.
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) Make sure that F1 is between 0.2 mm (0.0079 in.) and 0.8 mm (0.0315 in.).
     (b) Measure clearance F1 between the girt bar and the escape slide shoes with a light manual pressure to the aircraft centerline. This will make sure that the girt bart touches the actuating fingers.
     (c) Make sure that F2 is between 0.5 mm (0.0197 in.) and 1.0 mm (0.0394 in.).
     (d) Measure clearance F2 between the girt bar and the escape slide shoes with a light manual pressure (on the girt bar to the opposite escape slide shoe). This will make sure that the girt bart touches the actuating fingers.
   (5) If clearances F1 and F2 are not in the tolerances, adjust the girt bar fittings as follows:
     (a) Remove the 98DNSA20206060 RIGGING PIN98DNSA20206120 RIGGING PIN from the emergency control handle (rigging point).
     (b) Put the emergency control handle in the DISARMED position.
     (c) Open the door.
     (d) Find the position of the serrations between the girt bar fitting plates (93) and (94).
     (e) Adjust the position of the girt bar fittings on the X axis and the Y axis to get correct clearances F1 and F2.
     (f) Tighten the nuts (91) and (96) on the girt bar fittings (92) and (95).
     (g) 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 for some time, and
  • Make sure that the load necessary to operate the emergency control handle is not more than 10 daN (22.48 lbf).
Subtask 52-11-00-820-058-B
H. Adjustment of the Door Damper and Emergency Operation Cylinder
   (1) Do a check of the adjustment of the bellcrank finger of the door damper and emergency operation cylinder (Ref. AMM TASK 52-11-14-820-002).
Subtask 52-11-00-820-059-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.
I. Adjustment of the Door Buffer
F Adjustment of the Buffer of the Forward Passenger/Crew Door
   (1) Fully open the door.
   (2) Make sure that the support arm locks correctly on the fuselage frame when the door is open.
   (3) Make sure that the forward face of the hook fully touches the roller.
   (4) Make sure that the buffer is parallel to the fuselage structure.
   (5) Make sure that clearance G2 between the buffer (201) and the fuselage is between 0.5 mm (0.0197 in.) and 1.5 mm (0.0591 in.).
   (6) If clearance G2 is not in the tolerance, adjust the buffer as follows:
     (a) Put the door in the center position.
     (b) Remove the cotter pin (208) and discard it.
     (c) Remove the nut (207) and the cap (206).
     (d) Release the bushing (205), the washer (204) and the adjusting washer (203).
     (e) Release the bolt (209) and the buffer (201).
     (f) Keep the adjusting washer (202).
     (g) Move the adjusting washers (202) and (203) to get clearance G2.
     (h) Install the bolt (209), the buffer (201) and the adjusting washer (202) on the support (210).
     (i) Install the adjusting washer (203), the washer (204) and the bushing (205).
     (j) Install the cup (206) and the nut (207).
     (k) Tighten the nut (207).
     (l) Install the new AIPC 52-11-01-05-040 COTTER PIN (208) or the new AIPC 52-11-81-03-700 COTTER PIN (208).
     (m) Fully open the door.
Subtask 52-11-00-820-060-A
J. Check and Adjustment of the Compensation Mechanism
   (1) Do a check and adjustment of the compensation mechanism (Ref. AMM TASK 52-11-00-820-002).
Subtask 52-11-00-820-061-A ** ON A/C NOT FOR ALL
K. Check of the Outer Control-Handle Locking
F Adjustment of the Outer Control Handle of the Forward Passenger/Crew Door ** ON A/C NOT FOR ALL
   (1) Open the door from the outside and close it from the inside.
   (2) Make sure that the handle flap (304) goes back to its initial position when you close the door from the outside.
   (3) Apply a manual pressure on the handle flap (304) until it touches the stop (303).
   (4) Release the handle flap (304) and make sure that it goes back to its initial position.
   (5) Do this procedure five times.
   (6) If necessary, adjust the handle flap (304) as follows:
     (a) Loosen the nut (301) and remove the stop (303) and the adjustable shim (302).
     (b) Adjust the adjustable shim (302) to get the correct position of the handle flap (304) when the handle is in the closed position.
     (c) Install the stop (303) with the adjustable shim (302) and the nut (301).
     (d) TORQUE the nut (301) to between 0.748 and 0.612 m.daN (66.19 and 54.16 lbf.in ) T.
     (e) Do step (3) again.
Subtask 52-11-00-820-061-B ** ON A/C NOT FOR ALL
K. Check of the Outer Control-Handle Locking
F Adjustment of the Outer Control Handle of the Forward Passenger/Crew Door ** ON A/C NOT FOR ALL
   (1) Open the door from the outside and close it from the inside.
   (2) Make sure that the handle flap (304) goes back to its initial position when you close the door from the outside.
   (3) Apply a manual pressure on the handle flap (304) until it touches the stop (303).
   (4) Release the handle flap and make sure that the handle flap (304) goes back to its initial position.
   (5) Do this procedure five times.
Subtask 52-11-00-820-061-C ** ON A/C NOT FOR ALL
K. Check of the Outer Control-Handle Locking
F Adjustment of the Outer Control Handle of the Forward Passenger/Crew Door ** ON A/C NOT FOR ALL
F Adjustment of the Outer Control-Handle of the Handle Stop ** ON A/C NOT FOR ALL
   (1) With the outer control handle (192) in the up position, make sure that:
  • The outer control handle (192) locks in the up position.
  • Clearance J9 is 3 +0 mm or +1 mm (0.12 +0.00 in. or +0.04 in.) minimum at the level of the outer control handle before the pin stop (242) touches the stop screw (241).
   (2) If clearance J9 is not in the tolerance, do the adjustment that follows:
     (a) Adjust the length of the stop screw (241) until:
  • Clearance J9 between the outer control handle (192) and the door outer skin is 3 +0 mm or +1 mm (0.12 +0.00 in. or +0.04 in.) minimum.
  • The pin stop (242) touches the stop screw (241).
   (3) Close the door.
   (4) Open the door from the outside and close it from the inside.
   (5) Make sure that the handle flap (304) goes back to its initial position when you close the door from the outside.
   (6) Apply a manual pressure on the handle flap (304) until it touches the stop (303).
   (7) Release the handle flap (304) and make sure that it goes back to its initial position.
   (8) Do this procedure five times.
   (9) If necessary, adjust the handle flap (304) as follows:
     (a) Loosen the nut (301) and remove the stop (303) and the adjustable shim (302).
     (b) Adjust the adjustable shim (302) to get the correct position of the handle flap (304) when the handle is in the closed position.
     (c) Install the stop (303) with the adjustable shim (302) and the nut (301).
     (d) TORQUE the nut (301) to between 0.748 and 0.612 m.daN (66.19 and 54.16 lbf.in ) T.
     (e) Do step (3) again.
Subtask 52-11-00-820-062-A
L. Check of the Emergency Control-Handle Disarming
   (1) Close the door.
   (2) Put the emergency control handle in the ARMED position.
   (3) Open the door with the outer control handle.
   (4) Make sure that the emergency control handle moves to the DISARMED position.
Subtask 52-11-00-820-063-A
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.
M. Check of the Door Locking in the Up Position
F Adjustment of the Inner Contol Handle of the Forward Passenger/Crew Door
   (1) Make sure that during the opening of the door, the inner control handle (405) is in the locked position before the rollers release the guide fittings.
   (2) Make sure that when you close the door with the inner control handle (405), you feel no hard points because of the non-retraction of the hook (404).
   (3) If necessary, do the adjustment that follows:
     (a) Cut and discard the lockwire from the nuts (401) and (403).
     (b) Decrease the length of the rod (403) until there is no hard point because of the non-retraction of the hook (404) (when you close the door in the up position).
     (c) Tighten the nuts (401) and (403).
     (d) Safety them with the 14QFB1Wire-Locking Dia: 0.8 mm CRES Nickel Alloy -.
     (e) Put the door in the up position and make sure that you can install the 98DNSA20206060 RIGGING PIN98DNSA20206120 RIGGING PIN correctly.
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 in all the locations.
   (4) If you feel the hard points again, apply Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) on the mating surfaces of the hook (404) and the inner control handle (405).
Subtask 52-11-00-820-065-A
N. Check of 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).
NOTE: After the adjustment of the door, you can possibly see a permitted bend line on the cover plate.
Subtask 52-11-00-820-066-A
O. Adjustment of the Proximity Switch
   (1) Do an adjustment of proximity switch 11WV1 or 11WV2 (Ref. AMM TASK 52-71-00-820-001).
5. Close-up
Subtask 52-11-00-020-053-A ** ON A/C NOT FOR ALL
A. Removal of the Ballast Weight
   (1) Remove the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR or the escape-slide pack-assembly (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).
Subtask 52-11-00-020-053-B ** ON A/C NOT FOR ALL
A. Removal of the Ballast Weight
   (1) Remove the 98D52103501000 BALLAST WEIGHT - PASSENGER CREW DOOR or the escape slide if previously kept 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).
Subtask 52-11-00-865-053-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
121VUEIS/SLIDES/ARM AND WARN/FLT15WNP11
121VUEIS/SLIDES/ARM AND WARN/GND13WNP10
121VUEIS/SDAC1 AND 2/DOOR/DET/PAX48WVP05
Subtask 52-11-00-410-065-B
C. Installation of the Door-Frame Lining Panels
   (1) Install cove light panels 231CW and 232CW (Ref. AMM TASK 25-23-48-400-001).
   (2) Install lower sidewall panels 231AW and 232AW (Ref. AMM TASK 25-23-44-400-001).
   (3) Install the door insulation blankets.
   (4) Install the door-frame lining panels:
     (a) For the left door: 221AW, 221BW, 221CW, 221EW, 221FW, 221VW, 221SW and 221RW (Ref. AMM TASK 25-23-45-400-006)
     (b) For the right door: 222RW, 222TW, 222UW and 222VW (Ref. AMM TASK 25-23-45-400-007).
Subtask 52-11-00-410-051-A ** ON A/C NOT FOR ALL
D. Installation of the Components
   (1) Install the door linings (Ref. AMM TASK 25-23-46-400-001).
     (a) For the left door: 831FZ, 831CZ, 831DZ, 831AZ, 831BZ, 831EZ and 831GZ
     (b) For the right door: 841FZ, 841CZ, 841DZ, 841AZ, 841BZ, 841EZ and 841GZ.
   (2) Install the escape-slide pack-assembly:
     (a) For the left door:
Install the left escape-slide pack-assembly (Ref. AMM TASK 25-62-44-400-006).
     (b) For the right door:
Install the right escape-slide pack-assembly (Ref. AMM TASK 25-62-44-400-802).
   (3) Install the lining flap (Ref. AMM TASK 52-11-31-400-001).
Subtask 52-11-00-410-051-B ** ON A/C NOT FOR ALL
D. Installation of Components
   (1) Install the door lining panels (Ref. AMM TASK 25-23-46-400-001).
     (a) For the left door: 831FZ 831CZ 831DZ 831AZ 831BZ 831EZ 831GZ.
     (b) For the right door: 841FZ 841CZ 841DZ 841AZ 841BZ 841EZ 841GZ.
   (2) Install the escape slide:
     (a) For the left door:
Install the left-hand escape slide raft pack assembly (Ref. AMM TASK 25-62-44-400-007).
     (b) For the right door:
Install the right-hand escape slide raft pack assembly (Ref. AMM TASK 25-62-44-400-803).
   (3) Install the lining flap (Ref. AMM TASK 52-11-31-400-001).
Subtask 52-11-00-410-060-A
E. Close Access
   (1) Obey the special precautions after the work on the passenger/crew door (Ref. AMM TASK 52-10-00-860-002).
   (2) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
   (3) Close passenger/crew door 831 or 841 (Ref. AMM TASK 52-10-00-410-001).
   (4) Remove the access platform(s).
   (5) Make sure that the work area is clean and clear of tools and other items.
Subtask 52-11-00-862-050-A
F. De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001).
[Rev.10 from 2021] 2026.04.01 04:11:02 UTC
"Aviabrain" 2025