R No specific warning notice(s)
R No specific access platform 5.87 m (19 ft. 3 in.)
R 97A27003000000 1 GAGE ASSY - PUSH-PULL
R 97A27003000001 1 GAGE ASSY - PUSH-PULL
R 97A27902016000 1 SPRING SCALE ASSY
R 98D27207516000 1 RIGGING PIN SET
R 98D27207546000 1 PIN - RIGGING
R 98D27303000001 1 LOAD APPLICATION TOOL - ELEVATOR, AILERON, RUDDER
R 98D27303003001 1 CHECK TOOL - AILERON, ELEVATOR, RUDDER
R 98D27303022000 1 CHECK TOOL (ORAP) - AILERON, ELEVATOR, RUDDER
R B. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 24-41-00-861-002 R R 24-41-00-862-002 R R 29-10-00-863-003 R R 29-10-00-864-003 R 29-23-00-863-001 R R R 29-23-00-864-001 R R 29-24-00-863-001 R R 29-24-00-864-001 R 27-24-00-991-001-A R 27-24-00-991-010
R 3. Job Set-up
__________
R Subtask 27-24-00-861-056 Energize the Aircraft Electrical Circuits from the External Power De-energize the Aircraft Electrical Circuits Supplied from the External Power Pressurize the Blue Hydraulic System with a Ground Power Supply Depressurize the Blue Hydraulic System Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU Pressurize the Yellow Hydraulic System with the Electric Pump Depressurize the Yellow Hydraulic System Fig. 601 Fig. 602
R A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
R Subtask 27-24-00-010-059
R B. Get Access
R (1) Put the access platform at zone 325.
R (2) Open the access doors 325BL, 325BR, 325CL, 325CR, 325DL, 325DR,
R 325EL, 325ER.
R Subtask 27-24-00-860-065
R C. Aircraft maintenance configuration
R (1) Pressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-863-
R 001) (Ref. TASK 29-24-00-863-001) (Ref. TASK 29-10-00-863-003).
R (2) On the HYD section of the maintenance panel 50VU :
R - release the LEAK MEASUREMENT VALVES/B and LEAK MEASUREMENT VALVES/Y
R pushbutton switches (the OFF legends of these pushbutton switches
R come on).
R (3) On the center pedestal, on the panel 110VU, make sure that the RUD
R TRIM indicator shows 0.
R Subtask 27-24-00-941-054
R D. Safety Precautions
R (1) Put warning notice(s) on the pedals (CAPT and F/O) to tell persons
R not to operate them.
R (2) Put warning notice(s) on the panel 110VU to tell persons not to use
R the rudder trim.
R Subtask 27-24-00-480-054
R E. Installation of the Tools
R (Ref. Fig. 601/TASK 27-24-00-991-001-A, 602/TASK 27-24-00-991-010)
R (1) Install the PIN - RIGGING (98D27207546000) (2) or RIGGING PIN SET
R (98D27207516000) pin (98D27207516090) on the input lever of the lower
R servocontrol (1).
R (2) Install the LOAD APPLICATION TOOL - ELEVATOR, AILERON, RUDDER
R (98D27303000001) as follows:
R - on the trailing edge of the rudder
R - in line with the middle servo control.
R (3) Install the CHECK TOOL - AILERON, ELEVATOR, RUDDER (98D27303003001)
R or CHECK TOOL (ORAP) - AILERON, ELEVATOR, RUDDER (98D27303022000) on
R the trailing edge of the rudder.
R NOTE : Clean and make the tail-cone upper surface moist before you____
R attach the tool.
Servocontrol - Location of Rigging Point Figure 601/TASK 27-24-00-991-001-A
1EFF : 1 1R 1CES ALL 1 11 1 27-24-00 Page 609 May 01/05
Installation of the Check Tool Figure 602/TASK 27-24-00-991-010
1EFF : 1 1R 1CES ALL 1 11 1 27-24-00 Page 610 May 01/05
R 4. Procedure_________
R Subtask 27-24-00-220-054
R A. Check for too much Play (Green servo control pressurized)
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