(2)
 Retract the slats (Ref. TASK 27-80-00-866-005).

 (3)
 Retract the spoilers (Ref. TASK 27-60-00-866-002).

 Subtask 05-51-25-410-053
 B. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Close the NLG doors (Ref. TASK 32-22-00-410-001).

 (3)
 Close the MLG doors (Ref. TASK 32-12-00-410-001).

 1EFF : ALL 1 05-51-25Page 647 1 1 May 01/05R 1 1 1CES 1

 (4)
 Close all the access doors, and the access panels opened during the inspection procedure.

 (5)
 Remove the access platform(s).

 (6) Remove the warning notice(s). Subtask 05-51-25-860-054
 C. Put the aircraft back to its initial configuration.
 (1)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 (2)
 Remove the access platform(s).

 (3)
 Remove the warning notice(s).

 INSPECTION AFTER ENGINE FAILURE - INSPECTION/CHECK
__________________________________________________
 TASK 05-51-26-200-001
 INSPECTION AFTER ENGINE FAILURE
 1. Reason for the Job
__________________
 You must do this inspection after an engine failure:
 -
the engine is not balanced when one or more blades are not there,

 -
the engine is seized.
 You must remove the engines for these failures.

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific warning notices
 No specific access platform 0.62 m (2 ft.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
05-56-00-200-001 Inspection/Check of the Leveling and Measurement after Abnormal Operation of the Aircraft 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 28-10-00-910-002 Access to the Fuel Tanks and the Work Areas 28-25-00-650-001 Pressure Defuel 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
 Configuration before Maintenance Action 32-00-00-481-001 Installation of the Safety Devices on the Landing
 Gears 71-00-00-000-042 Removal of the Power Plant 71-00-00-400-042 Installation of the Power Plant 71-13-11-200-001 Visual Inspection of the Fan Cowl Doors 78-32-11-210-001 Detailed Visual Inspection of the Thrust Reverser

 3. Job Set-up
__________

 Subtask 05-51-26-481-050
 A. Safety Precautions
 (1)
 Make sure the the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-001).

 (2)
 Put the warning notices in position in the cockpit to tell persons not to operate the aircraft systems.

 Subtask 05-51-26-860-050
 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the hydraulics systems are depressurized (Ref. TASK 29-00-00-864-001).

 (2)
 Make sure that the electrical systems are de-energized (Ref. TASK 24-41-00-862-002).

 (3) Put the access platform in position. Subtask 05-51-26-020-050
 C. Removal of the Power Plant
 (1) Remove the power plant (Ref. TASK 71-00-00-000-042).

 4. Procedure
_________

 Subtask 05-51-26-210-050
R A. Inspection of the Engine Pylon
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----|
R |1. | | Engine Pylon | | | | | | | | | | | | | | | |  A.| | Examine the pylon panels, the doors |  X  | | | | | | | | and the auxiliary structure. Make | | | | | | | | | sure that there are no buckles, | | | | | | | | | cracks, or pulled or missing | | | | | | | | | fasteners. | | | | | | | | | | | | | | | |  B.| | Examine the main frame. Make sure that|  X  | | | | | | | | there are no distortion, cracks, | | | | | | | | | cracked or flaked paint, loose | | | | | | | | | rivets, or signs of shearing. | | | | | | | | | If you find damage: | | | | | | | | | (1) Remove or open the access doors | |  X  | | | | | | | and the inspection panels and | | | | | | | | | examine the panels and the | | | | | | | | | adjacent structure. Make sure that| | | | | | | | | there is no distorsion, wrinkles, | | | | | | | | | buckles, or tearing of plates at | | | | | | | | | the rivets. | | | | | | | | | (2) Examine the pylon main frame. Make| |  X  | | | | | | | sure that the parts that follow | | | | | | | | | are in the correct condition: | | | | | | | | | - the spars connected to the side | | | | | | | | | panels, | | | | | | | | | - the attachments between the | | | | | | | | | ribs, the side panels and the | | | | | | | | | upper and lower spars, | | | | | | | | | - the electrical cables, the | | | | | | | | | hydraulic pipes and the | | | | | | | | | components of the engine air | | | | | | | | | bleed system, | | | | | | | | | - the different components | | | | | | | | | mounted on the main frame, | | | | | | | | | - the fire protection systems | | | | | | | | | and specially the attachments of| | | | | |
　
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