(f)
Remove the rigging pin (29) from the output bellcrank of the centering spring-rod (15).
(2) Do the operational test of the rudder mechanical control (Ref. TASK 27-24-00-710-001).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-21-00Page 525 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Rudder Mechanical Control Figure 505/TASK 27-21-00-991-003
1EFF : 1 1R 1CES ALL 1 11 1 27-21-00 Page 526 Aug 01/04
R **ON A/C 301-399,
R Subtask 27-21-00-710-054-A
R E. Test
R (Ref. Fig. 505/TASK 27-21-00-991-003)
R
R (Ref. Fig. 502A/TASK 27-21-00-991-004-A)
R
R (Ref. Fig. 503/TASK 27-21-00-991-005)
R
R (Ref. Fig. 504/TASK 27-21-00-991-012)
R (1) Preparation for the Test.
R
R (a) Remove the three rigging pins (51):
R 1 From the connection relay of the CAPT rudder pedals (60)._
R 2 From the connection relay of the F/O rudder pedals (52)._
R 3 From the tension regulator (57)._
R (b) Remove the rigging pin (42) from the cable quadrant (24).
R (c) Remove the rigging pin (39) from the output bellcrank of the
R servocontrol (21).
R (d) Remove the rigging pins (34) and (35) from the input levers of
R the travel limitation unit (27).
R (e) Remove the rigging pin (40) from the mixer (41) of the artificial
R feel unit.
R (f) Remove the rigging pin (29) from the output bellcrank of the
R centering spring-rod (15).
R (2) Do the operational test of the rudder mechanical control (Ref. TASK
R 27-24-00-710-001).
R 1EFF : 301-399, 1 27-21-00Page 527 1 1 Aug 01/04 1 1 1CES 1R **ON A/C ALL
5. Close-up
________
Subtask 27-21-00-942-068
A. Make sure that the work area is clean and clear of tool(s) and other items.
Subtask 27-21-00-410-059
B. Close Access
(1)
Close the access doors 811, 312AR, 325BL, 325BR, 325CR, 325CL, 325DL, 325DR, 325ER, 325EL.
(2)
Install the access panel 211GF (Ref. TASK 53-12-11-400-001).
(3)
Install the protective cover on the battery power center 105VU.
(4)
Tighten the two screws.
(5)
Close the access door 822.
(6) Remove the access platform(s).
Subtask 27-21-00-860-053
C. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
TASK 27-21-00-720-002 Functional Test of the Rudder Mechanical Control 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. WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______ CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
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 access platform 5.87 m (19 ft. 3 in.)
TR60 1 RIGMASTER SYSTEM
98A27308005000 1 PROTRACTOR-CONTROL SURFACE DEFLECTION
1EFF : ALL 1 27-21-00Page 529 1 1 Aug 01/04R 1 1 1CES 1
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 29-10-00-864-003 Depressurize the Blue Hydraulic System 29-23-00-863-001 Pressurize the Green Hydraulic System from the Yellow
Hydraulic System through the PTU with the Electric Pump 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
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