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THE FLIGHT CONTROLS

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THE FLIGHT CONTROL SURFACES

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THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
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REFERENCE  QTY DESIGNATION
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No specific  access platform 2.0 m (6 ft. 7 in.)
 B. Referenced Information
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REFERENCE  DESIGNATION
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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)-
53-35-13-000-002 Removal of the Quick-Release Access Panels from the Belly Fairing Structure 53-35-13-400-002 Installation of the Quick-Release Access Panels on the Belly Fairing Structure
R **ON A/C 001-049, 051-061, 101-103, 201-203,
 52-41-24-991-001  Fig. 401
 1EFF : ALL 1 52-41-24Page 407 1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
 52-41-24-991-001-A Fig. 401A
 **ON A/C 001-049, 051-061, 101-103, 201-203,

 52-41-24-991-002 Fig. 402 R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
 52-41-24-991-002-A Fig. 402A
 **ON A/C 301-399,

 52-41-24-991-002-B Fig. 402B
 **ON A/C ALL

 3. Job Set-up
__________
 Subtask 52-41-24-941-050

 A. Make sure that the access platform is in position below the access door of the Blue hydraulic system.
 4. Procedure
_________
 **ON A/C 001-049, 051-061, 101-103, 201-203,

 (Ref. Fig. 401/TASK 52-41-24-991-001) R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
 (Ref. Fig. 401A/TASK 52-41-24-991-001-A)
 1EFF : ALL 1 52-41-24Page 408 1 1 Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-061, 101-103, 201-203,

 Subtask 52-41-24-420-050
 A. Installation of the Access Door of the Blue Hydraulic System
 (1)
 Clean the component interface and/or the adjacent area.

 (2)
 Do an inspection of the component interface and/or the adjacent area.

 (3)
 Put the access door (2) in the installation position.

 (4)
 Install the screws (1), the washers (17) and the nuts (16).

 (5)
 Install the bonding strap (15) (Ref. TASK 20-28-00-912-004).

 (6)
 If it was necessary to remove the spring bolt assembly, install it as follows:

 (a)
 Make sure that all parts of the removed spring bolt assembly are clean and in the correct condition.

 (b)
 Make sure that the bearing flange assy (7) and the hinge (19) are clean and in the correct condition.

 (c)
 Install the spring bolt (13) with the pin (3) and the retaining ring (14) at the hinge (19).

 (d)
 Put the compression spring (12) and the guide (10) in position on the spring bolt (13).

 (e)
 Install the guide (10) with the washers (11), the pin (8) and the retaining ring (9) at the bearing flange assy (7).

 (7)
 If it was necessary to remove the hinges (18) and (19), install them as follows:

 (a)
 Make sure that the support fitting assemblies (6) are clean and in the correct condition.

 (b)
 Install the hinges (18) and (19) with the pins (4) and the retaining rings (5) at the support fitting assemblies (6).

 (c)
 Connect the spring bolt assembly with the pin (3) and the retaining ring (14).

R 1EFF : 001-049, 051-061, 101-103, 201-203, 1 52-41-24Page 409 1 1 May 01/05 1 1 1CES 1R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,

 Subtask 52-41-24-420-050-A
 A. Installation of the Access Door (197FB)
 (1)
 Clean the component interface and/or the adjacent area.

 (2)
 Do an inspection of the component interface and/or the adjacent area.

 (3)
 If removed, assemble the hinges (9) on the access panel and attach it with the srews (5) and the washers (4).
　
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