**ON A/C ALL
R  Post SB 25-1225 For A/C 001-049,051-061,101-103,201-203, Subtask 25-13-14-020-053-A
 B. Removal of the Actuator on the Foot Rest Assembly
 (1)
 Put the foot rest assembly (10) on a bench, with the foot rest on the top and in the stowed position.

 (2)
 Remove the cotter pin (4) (on the actuator rod side) and discard it.

 (3)
 Remove the nut (3) and the washer (2).

 (4)
 Lightly compress the actuator (5) and disengage the actuator rod from the hinge pin (1).

 (5)
 Remove the cotter pin (9) (on actuator body side) and discard it.

 (6)
 Remove the nut (8) and the washer (7).

 (7)
 Disengage the hinge pin (6).

 (8)
 Remove the actuator.

 EFF : ALL

25-13-14Page 411

 **ON A/C ALL
 TASK 25-13-14-400-003
 Installation of the Actuator on the Foot Rest Assembly
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. 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 25-13-14-400-001 Installation of the Foot Rest and Sliding Table Assembly
R  **ON A/C 001-049, 051-061, 101-103, 201-203,
 25-13-14-991-003 Fig. 403
 **ON A/C ALL

R  Post SB 25-1225 For A/C 001-049,051-061,101-103,201-203, 25-13-14-991-003-A Fig. 403A
 EFF : ALL

25-13-14Page 412

 **ON A/C ALL
 3. Job Set-up
__________
 Subtask 25-13-14-861-052

 A. Aircraft Maintenance Configuration
 (1) Energize the ground service network
 (Ref. TASK 24-42-00-861-001)

 4. Procedure
_________ R **ON A/C 001-049, 051-061, 101-103, 201-203,
 (Ref. Fig. 403/TASK 25-13-14-991-003) **ON A/C ALL R Post SB 25-1225 For A/C 001-049,051-061,101-103,201-203, (Ref. Fig. 403A/TASK 25-13-14-991-003-A) R **ON A/C 001-049, 051-061, 101-103, 201-203,
 Subtask 25-13-14-420-052
 A. Installation of the Actuator on the Foot Rest Assembly CAUTION : MAKE SURE THAT THE RING DOES NOT EXPAND TOO MUCH WHEN YOU
_______ INSTALL IT. THERE IS A RISK OF RING FAILURE IF THE RING EXPANDS TOO MUCH.
 (1)
 Install the foot rest assembly (5) on a bench, with the foot rest on the top and in the stowed position.

 (2)
 Engage the actuator (3) (on actuator body side) in the clevis, engage the pin (4).

 (3)
 Install a new retaining ring (1).

 (4)
 Compress the actuator (3) (3 mm approximately) and engage the actuator rod in its pin (2).

 EFF : ALL

25-13-14Page 413

 (5) Install a new retaining ring (1).
 **ON A/C ALL

R  Post SB 25-1225 For A/C 001-049,051-061,101-103,201-203, Subtask 25-13-14-420-052-A
 A. Installation of the Actuator on the Foot Rest Assembly
 (1)
 Install the foot rest assembly (10) on a bench, with the foot rest on the top and in the stowed position.

 (2)
 Engage the actuator (5) (on actuator body side) in the clevis, engage the hinge pin (6).

 (3)
 Install the washer (7), the nut (8) and tighten it.

 (4)
 Install a new cotter pin (9).

 (5)
 Compress the actuator (5) (3 mm approximately) and engage the actuator rod in its hinge pin (1).

 (6)
 Install the washer (2), the nut (3) and tighten it.

 (7) Install a new cotter pin (4).
 **ON A/C ALL

 Subtask 25-13-14-420-053
 B. Installation of the Foot Rest and Sliding Table Assembly (Ref. TASK 25-13-14-400-001)
 5. Close-up
________
 Subtask 25-13-14-942-052

 A. Removal of Equipement
 (1) Make sure that the work area is clean and clear of tools and other items
 EFF : ALL

25-13-14Page 414

 Subtask 25-13-14-861-053
 B. Aircraft Maintenance Configuration (Ref. TASK 24-42-00-862-001)
 EFF : ALL

25-13-14Page 415

R  TASK 25-13-14-000-005 
R  Removal of the Captain and First-Officer Retractable Foot-Rests 
　
中國航空網(wǎng) m.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(shè)備1(123)