(3)
Do the operational test of the alternate braking system (operational check of the pedals) (Ref. TASK 32-43-00-710-001).
5. Close-up
________ Subtask 27-21-44-942-053
A. Put the aircraft back to the serviceable condition.
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Remove the warning notice(s). Subtask 27-21-44-410-051
B. Close Access
(1)
Close the access door 811.
(2)
Remove the access platform(s).
REGULATOR - CABLE TENSION (103CM) - REMOVAL/INSTALLATION
________________________________________________________
TASK 27-21-45-000-001
R Removal of the Cable Tension Regulator Assy
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.
CAUTION : DO THIS PROCEDURE IN A HANGAR IF THERE ARE WIND GUSTS. WIND GUSTS CAN
_______ CAUSE DAMAGE TO THE LINKAGE WHEN THE RIGGING PINS ARE IN POSITION ON THE RUDDER CONTROL.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.5 m (4 ft. 11 in.)
No specific access platform 2.8 m (9 ft. 2 in.)
FE171901 1 TOOL - LOCKING
98A27901002000 1 PIN, RIGGING - RUDDER CONTROL
98D27207516000 1 RIGGING PIN SET
98D27207547000 1 PIN - RIGGING
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground
Power Supply
29-10-00-864-001 Depressurize the Green Hydraulic System
29-10-00-864-002 Depressurize the Yellow Hydraulic System
29-10-00-864-003 Depressurize the Blue Hydraulic System
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-21-45-991-001 Fig. 401
**ON A/C 301-399,
27-21-45-991-001-A Fig. 401A
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-21-45-991-002 Fig. 402
**ON A/C 301-399,
27-21-45-991-002-A Fig. 402A
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-21-45-991-003 Fig. 403
**ON A/C 301-399,
27-21-45-991-003-A Fig. 403A **ON A/C ALL
3. Job Set-up
__________
Subtask 27-21-45-010-052
A. Get Access
(1) Remove the panel 211GF at zone 211. R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 401/TASK 27-21-45-991-001)
**ON A/C 301-399,
(Ref. Fig. 401A/TASK 27-21-45-991-001-A)
**ON A/C ALL
(2)
Put the access platform in position at zone 121.
(3)
Open the access doors 811.
(4)
Put the access platform in position at zone 312.
(5) Open the access doors 312AR.
Subtask 27-21-45-860-050
B. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits
(Ref. TASK 24-41-00-861-002)
(2)
Pressurize the Blue hydraulic system (Ref. TASK 29-10-00-863-003).
(3)
On the overhead panel 23VU, make sure that the FLT CTL/FAC1 pushbutton switch is pushed.
(4)
On the overhead panel 24VU, make sure that the FLT CTL/FAC2 pushbutton switch is pushed (on these pushbuttons switches, the OFF and FAULT legends are off).
Component Location
Figure 401/TASK 27-21-45-991-001
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-21-45Page 404 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
R Component Location
R Figure 401A/TASK 27-21-45-991-001-A
R 1EFF : 301-399, 1 27-21-45 Page 405
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