__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 08-007  USA MIL-R-46082 TYPE II
 SEALANT, HIGH TEMP. (Ref. 20-31-00)

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from
 the External Power
 25-45-19-991-001 Fig. 401
 25-45-19-991-002 Fig. 402

 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
 25-45-19-991-005 Fig. 403 R **ON A/C 106-149, 218-299, 301-399, 401-499,
 25-45-19-991-005-A Fig. 403A
 **ON A/C ALL

 25-45-19-991-003  Fig. 404
 EFF : ALL
25-45-19Page 405

 3. Job Set-up
__________ Subtask 25-45-19-860-050
 A. Aircraft Maintenance Configuration
 (1) Make sure that the ground service network is energized
 (Ref. TASK 24-42-00-861-001).

 4. Procedure
_________ Subtask 25-45-19-210-050
 A. Preparation for Installation
 (1)
 Clean the component interface and/or the adjacent area.

 (2)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (3) Do an inspection of the component interface and/or the adjacent area. Subtask 25-45-19-420-050
 B. Installation of the Lavatory Bi-folding Door
 (Ref. Fig. 401/TASK 25-45-19-991-001)

 (1)
 Put the lavatory bi-folding door (1) in position and make sure the lower door fitting (8) inserts into the door rail (9).

 (2)
 Slide the screw (4) upwards to lock the door (1) and tighten the screw (4).

 (3)
 Connect the damper (2) to the lavatory wall bracket (3).

 (4)
 Close the lavatory bi-folding door (1).

 (5)
 Lock the upper and the lower door latches (5).

 (6)
 Measure the dimension E clearance between the lavatory door (1) and the door frame. This must be 3.0 mm (0.12 in.) minimum. If necessary, adjust the door as follows:

 (a)
 Loosen the grubscrew (6).

 (b)
 Adjust the nut (7) to set the dimension E clearance between the lavatory door (1) and the door frame.

 EFF : ALL
25-45-19Page 406
Feb 01/04
R
 CES

 (c)
 Tighten the grubscrew (6).

 (d)
 Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-007) to the grubscrew (6).

 Subtask 25-45-19-420-051
 C. Installation of the Lavatory Single Blade Door
 (Ref. Fig. 402/TASK 25-45-19-991-002)

 (1)
 Put the lavatory single blade door (1) in position and install the screws (4).

 (2)
 Put the door stop (3) in position and install the washer (6) and the screw (2).

 (3)
 Measure the dimension C clearance between the lavatory door (1) and the door frame. This must be 3.0 mm (0.12 in.) minimum. If necessary, adjust the door (1) as follows:

 (a)
 Open the lavatory door (1).

 (b)
 Loosen the screws (4).

 (c)
 Adjust the hinge (5) to get dimension C upper and lower clearance between the lavatory door (1) and the door frame.

 (d)
 Tighten the screws (4).

 (e) Close the Lavatory door (1). R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-217,
 Subtask 25-45-19-710-050
 D. Do the Operational Test of the Emergency Opening (from outside of the lavatory) of the Lavatory Doors.
 NOTE : For this test, the lavatory door must be locked from the inside.
____
 (1) Single Bladed Door
 (Ref. Fig. 403/TASK 25-45-19-991-005)

 (a) Lift up the spring loaded LAVATORY over (1).
 EFF : ALL
25-45-19Page 407

 Lavatory Single-Blade Door - Emergency Opening from the Outside Figure 403/TASK 25-45-19-991-005
R  EFF : 001-049, 051-099, 101-105, 151-199, 25-45-19Page 408 201-217, May 01/05
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM EQUIPMENT/FURNISHINGS 設備3(122)