(2)
Push the FLT CTL/FAC 2 pushbutton switch on the overhead panel 24VU and the OFF legend goes off.
Subtask 27-21-49-710-050
F. Do an operational test of the rudder servo controls (Ref. TASK 27-24-00-710-002).
Subtask 27-21-49-820-050
G. Adjust the spring rod (3) if necessary: (Ref. TASK 27-24-51-400-001).
5. Close-up
________ Subtask 27-21-49-860-055
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)
Apply a layer of SPECIAL MATERIALS (Material No. 05-027) to the adjacent structure.
Rigging Pin Locations
Figure 402/TASK 27-21-49-991-002
1EFF : ALL 1 27-21-49 Page 412
1 1 Feb 01/98
1 1
1CES 1
(3) Make sure that the drain holes in the adjacent structure are not
blocked.
R Subtask 27-21-49-410-050-A
R B. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Close the access panel 325CR and install the access panel 325DR
R (Ref. TASK 55-33-13-410-002).
R (3) Remove the warning notice(s).
R (4) Remove the access platform(s).
SPRING ROD - INSPECTION/CHECK
_____________________________
TASK 27-21-49-200-001
Check of the Actuating Spring Rod
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______ FALL CAN INJURE OR KILL YOU.
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 digital calliper No specific 1 ACCESS PLATFORM 6M (20 FT) No specific 1 WARNING NOTICE No specific 1 TIE WRAP No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft) 98D27207545000 1 PIN - RIGGING 98D27207546000 1 PIN - RIGGING
B. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
11 cotter pin 27-21-04 08 -050 15 cotter pin 27-21-04 22 -100
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
27-21-49-000-001 Removal of the Spring Rod
27-21-49-400-001 Installation of the Spring Rod
27-24-00-710-002 Operational Test of the Rudder Servocontrols with Individual Hydraulic System
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
29-10-00-864-003 Depressurize the Blue Hydraulic System
55-33-13-010-002 Opening/Removal of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
55-33-13-410-002 Closing/Installation of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
27-21-49-991-003 Fig. 601
3. Job Set-up__________
Subtask 27-21-49-865-054
A. 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
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