-
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
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REFERENCE QTY DESIGNATION
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No specific blanking caps
No specific circuit breaker(s) safety clip(s)
R No specific adjustable access platform 6 m (19 ft. 8 in.)
R No specific 2 WARNING NOTICE 6137-013 1 PIN - LOCKING 6137-060 1 PIN - LOCKING 98D27207546000 1 PIN - RIGGING 98D27207547000 1 PIN - RIGGING 98D27207548000 1 PIN - RIGGING
B. Consumable Materials
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REFERENCE DESIGNATION
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Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. 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 27-21-00-840-001 Removal/Installation of the control rod on the rudder mechanical control 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground Power Supply 55-33-13-000-001 Removal of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
55-33-13-010-002 Opening/Removal of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
27-22-51-991-001 Fig. 401 27-22-51-991-004 Fig. 402 27-22-51-991-005 Fig. 403 27-22-51-991-003 Fig. 404 27-22-51-991-007 Fig. 405
3. Job Set-up
__________
(Ref. Fig. 401/TASK 27-22-51-991-001, 402/TASK 27-22-51-991-004)
Subtask 27-22-51-010-050-A
A. Get Access
(1)
Put the adjustable access platform in position.
(2)
Open the access door 312AR.
(3)
Open the access panel 325BL at the trailing edge of the vertical stabilizer (1) (Ref. TASK 55-33-13-010-002).
(4)
Remove the access panel 325BR (Ref. TASK 55-33-13-000-001).
1EFF : ALL 1 27-22-51Page 402 1 1 Aug 01/04R 1 1 1CES 1
Rudder Trim Actuator 10CC - Part Number 6137-3 Figure 401/TASK 27-22-51-991-001
1EFF : 1 1R 1CES ALL 1 11 1 27-22-51 Page 403 May 01/03
R Rigging Pin Locations for the Replacement of a Rudder Trim Actuator - Part R Number 6137-4/6137-5 Figure 402/TASK 27-22-51-991-004
Subtask 27-22-51-865-056
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18
Subtask 27-22-51-860-051
C. Aircraft Maintenance Configuration
R R NOTE : The subsequent worksteps are necessary if you remove a rudder trim____ actuator with the part number 6137-3. If you remove a rudder trim actuator with the part number 6137-4 or 6137-5, refer to the next subtask.
(1) Energize the aircraft electrical circuits. (Ref. TASK 24-41-00-861-002)
R (2) Pressurize the Blue hydraulic system
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL_______ SURFACES ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
R
R R (a) Pressurize the Blue hydraulic system with the electric pump. (Ref. TASK 29-10-00-863-003)
(3) Put the rudder pedals in the neutral position.
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