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).
1EFF : ALL 1 05-51-13Page 603 1 1 May 01/02R 1 1 1CES 1
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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