-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
25-23-47-000-001 Removal of the Lining from the Emergency Exit Hatches 25-23-47-400-001 Installation of the Lining on the Emergency Exit
Hatches 52-10-00-010-001 Opening of the Passenger/Crew Door 52-10-00-410-001 Closing of the Passenger/Crew Door 52-21-00-200-001 Detailed Visual Inspection of the Emergency Exits,
Internal Structure and Load Transmitting Profile
LH/RH
52-21-11-000-001 Removal of the Emergency Exit Hatch
52-21-11-400-001 Installation of the Emergency Exit Hatch
52-21-11-820-002 Adjustment of the Hatch Control Handle
**ON A/C 001-049, 051-099, 101-149, 201-299,
52-21-11-991-003 Fig. 406
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
3. Job Set-up
__________
Subtask 52-21-11-860-054
A. Aircraft Maintenance Configuration
(1)
Make sure that the FWD or the AFT passenger/crew door is opened (Ref. TASK 52-10-00-010-001).
(2)
Make sure that the applicable emergency exit hatch is removed (Ref. TASK 52-21-11-000-001).
(3)
Make sure that the lining is removed from the applicable emergegecy exit hatch (Ref. TASK 25-23-47-000-001).
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4. Procedure
_________
Subtask 52-21-11-910-050
A. Preparation for Installation
(1)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(2)
Make sure that the mating areas of the bearing brackets (2) and the hatch structure are clean and in the correct condition.
(3)
Apply COMMON GREASE (Material No. 04-004) to the bolts (1), (6), (7), (12),(31), (41) and (42).
(4)
Apply SEALANTS (Material No. 09-018) to the mating area of the hatch control handle (14) and the bearing brackets (2).
(5)
Make sure that the bonding areas of the bolts (6) and (42) are correctly prepared (Ref. TASK 20-28-00-912-004).
Subtask 52-21-11-420-050
B. Installation of the Hatch Locking Mechanism
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 406/TASK 52-21-11-991-003) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(1) Install the hatch control handle (14) as follows:
(a) Put the hatch control handle (14) with the plate (30) in position.
NOTE : Make sure that the handle seal (38) touches the frame
____
panel (37).
(b) Install the bolts (31), the washers (32) and nuts (33). NOTE : Make sure that the push plate (39) is installed
____ symmetrically in the opening of the hatch skin.
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(c)
Make sure that the push plate (39) is in line with the outer skin of the hatch structure.
(d)
To adjust the offset, change the position of the washers (32) between the hatch control handle (14) and the hatch structure.
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