-
maximum 2.0 mm (0.0787 in.) above wing surface (out of wind).
(2)
Measure the step tolerances of the pressure-relief panel ends across the line of flight. These must be as follows:
(a) For the panel ends:
-
maximum 1.2 mm (0.0472 in.) above or below the adjacent panel end (DIM X)
-
maximum 1.2 mm (0.0472 in.) above or below the adjacent wing surface (DIM Y).
(3)
Measure the clearance between the D-nose skin and the leading edges of the pressure-relief panels. The clearance must be between 0.5 mm (0.0196 in.) and 3.5 mm (0.1377 in.).
(4)
Measure the clearance at the inboard and outboard edges of the pressure-relief panels. The clearance must be between 0.5 mm (0.0196 in.) and 5.5 mm (0.2165 in.).
R (5) Measure the clearance at the trailing edges of the pressure-relief
R panels between:
R - the wing-skin and the edges of the panels (that are parallel to the
R panel leading edges), the clearance must be between 0.5 mm (0.0196
R in.) and 5.5 mm (0.2165 in.)
R - the wing-skin and the edges of the panel cut-outs (that are not
R parallel to the panel leading edges), the clearances must be
R between 0.5 mm (0.0196 in.) and 7.0 mm (0.2755 in.).
R **ON A/C ALL
R 5. Close-up________
R Subtask 57-41-37-865-074
R A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
R breaker(s):
R 5CV, 7CV.
R Subtask 57-41-37-942-060
R B. Removal of Equipment
R (1) Remove the warning notice(s).
R (2) Remove the safety barriers.
R (3) Remove the access platform(s).
R (4) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
TASK 57-41-37-000-003
Removal of the Access Panel 522AT(622AT)
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
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
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific safety barriers
No specific warning notice
No specific access platform 3.2 m (10 ft. 6 in.)
1EFF : ALL 1 57-41-37Page 412 1 1 Aug 01/04R 1 1 1CES 1
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-80-00-866-004 Extending the Slats on the Ground
**ON A/C 001-003, 051-052,
57-41-37-991-018 Fig. 401 R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
57-41-37-991-018-A Fig. 401A
**ON A/C ALL
3. Job Set-up
__________
Subtask 57-41-37-941-060
A. Safety Precautions
(1) Put the safety barriers in position.
Subtask 57-41-37-860-064
B. Aircraft Maintenance Configuration
(1)
Fully extend the slats (Ref. TASK 27-80-00-866-004).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control lever.
(3)
Put a warning notice in the cockpit to tell persons not to operate the slats.
(4)
Put the access platform in position below the applicable access panel 522AT(622AT).
Subtask 57-41-37-865-069
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
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