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 adjustable access platform No specific warning notices No specific access platform 1.6 m (5 ft. 3 in.) 98D27203001000 1 TOOL - RUDDER NEUTRAL ADJUSTMENT 98D27207516000 1 RIGGING PIN SET 98D27207546000 1 PIN - RIGGING 98D27303000001 1 LOAD APPLICATION TOOL - ELEVATOR, AILERON, RUDDER
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific lockwire - corrosion resistant steel dia. 0.8 mm
 (0.03 in.) RR C. Referenced Information

 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
11-00-00-960-001 24-41-00-861-002
24-41-00-862-002
27-24-00-710-001 29-10-00-863-003
29-10-00-864-003 29-23-00-863-001
29-23-00-864-001 29-24-00-863-001 29-24-00-864-001 55-33-13-010-001 55-33-13-410-001 27-24-00-991-003 27-24-00-991-004 27-24-00-991-005
3. Job Set-up
__________ Subtask 27-24-00-861-054
Replacement of the Reference TriangleEnergize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerOperational Test of the Rudder Hydraulic ActuationPressurize the Blue Hydraulic System with a Ground Power SupplyDepressurize the Blue Hydraulic SystemPressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric PumpDepressurize the Green and Yellow Hydraulic Systems after Operation of the PTUPressurize the Yellow Hydraulic System with the Electric PumpDepressurize the Yellow Hydraulic SystemOpening of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BRClosing of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BRFig. 501Fig. 502Fig. 503
 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002). Subtask 27-24-00-010-055
 B. Get Access
 (1)
 Put the access platform in position at the access door 822.

 (2)
 Open the access door 822.

 (3)
 At the battery power center 105VU:

 -loosen the two screws and remove the protective cover.

 Subtask 27-24-00-865-050
 C. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
 Subtask 27-24-00-860-059
 D. Aircraft Maintenance Configuration
 (1)
 Pressurize the aircraft hydraulic systems (Ref. TASK 29-24-00-863-001) (Ref. TASK 29-23-00-863-001) (Ref. TASK 29-10-00-863-003).

 (2)
 On the overhead panel 23VU, make sure that:

 -the FLT CTL/FAC1, FLT CTL/ELAC1 and FLT CTL/SEC1 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).

 (3)
 On the overhead panel 24VU, make sure that:

 -the FLT CTL/FAC2, FLT CTL/ELAC2, FLT CTL/SEC2 and FLT CTL/SEC3 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).

 (4)
 On the center pedestal, on the panel 110VU, make sure that the RUD TRIM indicator shows 0.

 (5)
 Put the warning notices in the cockpit to tell persons not to operate the flight controls.

 (6)
 Depressurize the aircraft hydraulic systems (Ref. TASK 29-10-00-864-003) (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001).

 1EFF : ALL 1 27-24-00Page 511 1 1 Aug 01/04R 1 1 1CES 1
　
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