D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-22-55-640-001 Lubrication of the Rudder Bearing No. 6
20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
23-61-41-000-001 Removal of the Static Discharger 23-61-41-400-001 Installation of the Static Discharger 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 27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 27-25-00-820-001 Adjustment of the Rudder Position Indicating 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action 51-75-13-916-002 Repair to a layer of Corrosion Preventive Compound 53-55-12-000-001 Removal of the Rudder Fairings 325AL and 325AR 53-55-12-400-001 Installation of the Rudder Fairings 325AL and 325AR 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
55-42-13-400-001 Installation of the Access Panel 326CT at the Rudder
Attach Fitting No. 7
27-21-41-991-001 Fig. 401
27-21-41-991-002 Fig. 402
27-21-41-991-003 Fig. 403
**ON A/C 001-003, 051-054,
27-21-41-991-004-B Fig. 404
R **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
27-21-41-991-004-A Fig. 404A
INTENTIONALLY BLANK
R 1 1
27-21-41Page 426
1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
**ON A/C ALL
27-21-41-991-005 Fig. 405 27-21-41-991-006 Fig. 406
3. Job Set-up
__________ Subtask 27-21-41-861-051
A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits. (Ref. TASK 24-41-00-861-002)
Subtask 27-21-41-865-054
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 27-21-41-860-053
C. Aircraft Maintenance Configuration
(1)
Make sure that the rudder pedals are in the neutral position.
(2)
Make sure that the hydraulic systems are depressurized and put them in the maintenance configuration. (Ref. TASK 29-00-00-864-001).
(3)
Make sure that the RUD TRIM indicator on the panel 110VU of the center pedestal shows zero.
(4)
Make sure that the FLT CTL/FAC 1 pushbutton switch on the overhead panel 23VU is released and the OFF legend is on.
(5)
Make sure that the FLT CTL/FAC 2 pushbutton switch on the overhead panel 24VU is released and the OFF legend is on.
(6)
Make sure that the warning notices are in position.
1EFF : ALL 1 27-21-41Page 427 1 1 Aug 01/01R 1 1 1CES 1
(7) Make sure that the access platform is in position.
(8) Make sure the access door 312AR is open.
Subtask 27-21-41-862-051
D. Aircraft Maintenance Configuration
(1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002)
Subtask 27-21-41-865-052
E. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU AUTO FLT/FAC1/28VDC 49VU AUTO FLT/FAC1/26VAC 121VU AUTO FLT/RUDDER/TRIM/IND 121VU AUTO FLT/FAC2/28VDC 121VU AUTO FLT/FAC2/26VAC 5CC1 14CC1 15CC 5CC2 14CC2 B04B03M20M19M18
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