B. Referenced Information

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied
 from the External Power
 27-50-00-866-008  Extension of the Flaps on the Ground
 27-50-00-866-009  Retraction of the Flaps on the Ground
 27-54-00-200-001  Detailed Visual Inspection of the Transmission
 Assembly (Including Part of the Transmission in Zone
 140)
 27-54-00-710-001  Operational Test of the Flap System
 27-54-46-200-001  Detailed Visual Inspection of the Flap Tracks and
 Rollers (as far as is possible)
 27-60-00-866-002  Extension-Retraction of the Spoilers for Maintenance
 27-64-00-710-001  Operational Test of the Spoiler Hydraulic Actuation
 27-80-00-866-004  Extending the Slats on the Ground
 27-80-00-866-005  Retracting the Slats on the Ground
 27-84-00-200-001  Detailed Visual Inspection of the Slat Transmission
 System
 27-84-00-210-001  Detailed Visual Inspection of the Slat Track Rollers,
 the Pinions and the Curved Rack Gears (As Far As
 Visible)
 27-84-00-710-001  Operational Test of the Slat System
 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
 32-12-00-010-001  Open the Main Gear Doors for Access
 32-12-00-410-001  Close the Main Gear Doors after Access
 57-26-00-200-001  Detailed Visual Inspection of Outer Wing Flap Track 2
 Aft Attachment Fittings on Wing Bottom Skin at Rear
 False Spar, and Flap Track 3 and 4 ....
 57-26-00-200-006  Detailed Visual Inspection of Outer Wing Flap Track
 Beams 2, 3, 4 Fwd Spigot Pins, Bolts and Fittings
 05-51-13-991-001  Fig. 601
 05-51-13-991-002  Fig. 602
 05-51-13-991-005  Fig. 603
 05-51-13-991-006  Fig. 604
 05-51-13-991-004  Fig. 605
 05-51-13-991-003  Fig. 606

 1EFF : ALL 1 05-51-13Page 602 1 1 May 01/02R 1 1 1CES 1

 3. Job Set-up
__________ Subtask 05-51-13-869-051
 A. Not Applicable Subtask 05-51-13-481-050
 B. Safety Precautions
 (1) Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-001).
 Subtask 05-51-13-010-050
 C. Get Access
 (1) Open the main doors of the main gear and install the safety devices (Ref. TASK 32-12-00-010-001).
 Subtask 05-51-13-866-050
 D. Extension of the Flight Control Surfaces
 (1)
 Fully extend the flaps (Ref. TASK 27-50-00-866-008).

 (2)
 Fully extend the slats (Ref. TASK 27-80-00-866-004).

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

 (4)
 Put a warning notice in the cockpit to tell persons not to operate the landing gear or the flight controls.

 Subtask 05-51-13-860-050
 E. Aircraft Maintenance Configuration
 (1)
 Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-001).

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

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 Subtask 05-51-13-010-051
 F. Get Access
 (1) Put the access platform in position.
 4. Procedure
_________
 Subtask 05-51-13-869-050
 A. General
 NOTE : All the inspections are visual unless the text gives other
____ instructions. Operators can refer to the Non-destructive Testing Manual (NTM) and use the non-destructive procedures.
 Subtask 05-51-13-210-051
 B. Inspection of the Wings
 -------------------------------------------------------------------------------|ITEM|INSP| INSPECTION TASKS |PHASE|PHASE|PHASE|INSP|REF.| | |CODE| |  1  |  2  |  3  |SIGN|FIG.| |----|----|---------------------------------------|-----|-----|-----|----|----| |1. | | Inspection of the wing leading edge | | | | | | | | | | | | | | | |  A.| | Examine the upper and lower skin |  X  | | | | | | | | panels of the leading edge for | | | | | | | | | distortion, cracks, pulled or torn | | | | | | | | | fasteners and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access to the other side of | |  X  | | | | | | | the damaged area. | | | | | | | | | (2) Examine internally the related | |  X  | | | | | | | area for distortion and damage. | | | | | | | | | | | | | | | |2. | | Inspection of the wing trailing edge | | | | | | | | | | | | | | | |  A.| | Examine the upper and lower skin |  X  | | | | | | | | panels of the wing trailing edge for | | | | | | | | | distortion, cracks, pulled or torn | | | | | | | | | fasteners, skin/honeycomb-core | | | | | | | | | delamination and damaged paintwork. | | | | | | | | | If you find damage: | | | | | | | | | (1) Get access to the other side of | |  X  | | | | | | | the damaged area. | | | | | | | | | (2) Examine internally the related | |  X  | | | |
　
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