NOTE : Make sure that the handle seal (38) touches the frame
____
 panel (37).

 (e) Measure the distance between the push plate (39) and the opening of the outer hatch skin on all the sides.
 NOTE : The distance must be between 0.5 mm (0.0196 in.) and 2.5
____
 mm (0.0984 in.) and symmetrical.

 (f)
 If the distance is not symmetrical, change the position of the push plate (39) as follows:

 -Loosen the screws (40) and move the push plate (39) so that the clearance is correct.
 -TORQUE the screws (40) to between 0.039 and 0.045 m.daN (3.45 and 3.98 lbf.in).

 (g)
 Apply SEALANTS (Material No. 09-018) at the mating surfaces of the push plate (39) and the flash panel (36).

 (h)
 Apply SEALANTS (Material No. 09-018) on the ends of the screws

 (40) and on the inner area of the flush panel (36).

 (i)
 Install the bolts (41) and (42), the washers (35) and the nuts (34).

 NOTE : The bolt (42) is a bonding point (Ref. TASK 20-28-00-912-
____
 004).

 (j)
 Adjust the overcenter position of the hatch control handle (14) (Ref. TASK 52-21-11-820-002).

 (k)
 Attach the connection rod (9) on the hatch control handle (14) with the bolt (12), the washers (13) and the nut (15).

 (l)
 Tighten the nut (15) and safety it with cotter pin (16).

 (2) Install the locking shaft unit (17) as follows:
 (a) Put the locking shaft unit (17) and the shim plate (44) in the installation position.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-21-11Page 427 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 (b)
 Attach the bearing brackets (2) of the locking shaft unit (17) with the bolts (1) and the nuts (3).

 (c)
 Put the bonding jumper in position to the bearing bracket (2) and install the bolt (6) and the nut (4) (Ref. TASK 20-28-00-912-004).

 (d)
 Install the connection rod (9) on the locking hook (18) with the bolt (7), the washers (8) and the nut (10).

 (e)
 Tighten the nut (10) and safety it with the new cotter pin (11).

 (f)
 Adjust the overcenter position of the hatch control handle (1) (Ref. TASK 52-21-11-820-002).

 Subtask 52-21-11-210-050
 C. Visual Inspection
 (1)
 Install the emergency exit hatch (Ref. TASK 52-21-11-400-001). NOTE : Do not remove the lockpin assembly on the inflation reservoir

____ at this stage and make sure that the latch pin remains in the disarmed position.

 (2)
 Make sure that the handle seal (38) of the flush panel (36) is in the correct position to prevent that the cabin pressure decreases.

 NOTE : If necessary, change the position of the hatch control handle
____ (14) so that the handle seal (38) and the push plate (39) are correctly installed.
 (3)
 Operate the hatch control handle (14) to make sure that the locking function is correct.

 (4)
 Make sure that the skin offset between the emergency exit hatch and the fuselage is correct (Ref. TASK 52-21-00-200-001).

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-21-11Page 428 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 5. Close-up
________ Subtask 52-21-11-410-053
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the lining on the applicable emergency exit hatch (Ref. TASK 25-23-47-400-001).

 (3)
 Close the FWD passenger/crew door (Ref. TASK 52-10-00-410-001).

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-21-11Page 429 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 TASK 52-21-11-000-003
 Removal of the Slide Release Mechanism

 1. Reason for the Job
__________________
 To replace a damaged component of the slide release mechanism or to change its installation position. NOTE : This change makes it possible to install an emergency exit hatch to
____
 the opposite or the adjacent position.

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
25-23-47-000-001 Removal of the Lining from the Emergency Exit Hatches 52-21-11-000-001 Removal of the Emergency Exit Hatch
 **ON A/C 001-049, 051-099, 101-149, 201-299,
 52-21-11-991-004 Fig. 407 R **ON A/C 151-199, 401-499,
　
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 DOORS 艙門3(35)