B. Consumable Materials
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REFERENCE DESIGNATION
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R Material No. 02-003 F NSA 307110 TYPE 4 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) Material No. 05-005 USA MIL-C-16173 GRADE II CORROSION PREVENTIVE (Ref. 20-31-00) Material No. 08-029 USA MIL-R-46082 TYPE I ADHESIVE (Ref. 20-31-00) Material No. 09-013 USA MIL-PRF-81733 TYPE I CLASS A CORROSION INHIBITING BRUSH CONSISTENCY (Ref. 20-31-00) Material No. 16-003 F ASNB70720 COATING (OBSOLETE USE 16-021) (Ref. 20-31-00)
C. Expendable Parts
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FIG.ITEM |DESIGNATION |IPC-CSN
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cotter pins 27-26-04 02 -050
D. Referenced Information
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REFERENCE DESIGNATION
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22-63-00-710-001 Operational Test of the Yaw Damper Function 22-96-00-710-001 Operational Test of the AFS 22-97-00-710-001 Operational Test of the LAND CAT III Capability 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action
29-00-00-910-002 Safety Procedures of the Hydraulic System
29-14-00-614-001 Depressurization of the Hydraulic Reservoirs
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REFERENCE DESIGNATION
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29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through the Ground Connector
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
27-26-51-991-001 Fig. 401
3. Job Set-up
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(Ref. Fig. 401/TASK 27-26-51-991-001)
Subtask 27-26-51-860-054-A
A. Aircraft Maintenance Configuration
WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
(1)
Obey the hydraulic safety procedures (Ref. TASK 29-00-00-910-002).
(2)
Make sure that the adjustable access platform is in position at zone
325.
R (3) Make sure that the access panel 325BL (for 3CC1) or 325BR (for 3CC2) R is open (Ref. TASK 55-33-13-010-002).
(4)
Make sure that the rudder pedals are in the neutral position.
(5)
Make sure that the RUD TRIM indicator on the center pedestal, on the panel 110VU shows 0.
(6)
Make sure that the warning notices are in position in the cockpit to tell persons not to operate the flight controls.
(7)
Make sure that the hydraulic systems are depressurized and put them in the maintenance configuration. (Ref. TASK 29-00-00-864-001).
(8)
Make sure that the reservoirs of the Green and Yellow hydraulic systems are depressurized (Ref. TASK 29-14-00-614-001).
(2)
Inspection of the attachment components.
R R (9) Make sure that the drainage container is in position below the hydraulic pipes of the actuator.
R R (10) Make sure that the aircraft electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
R R R R R R (11) Make sure that the warning notices are in position to tell persons not to pressurize the Green, the Yellow and the Blue hydraulic systems: - in the cockpit on the hydraulic section 40VU of the overhead panel, - on the ground service panels of the Green, Yellow and Blue hydraulic systems.
R R R (12) Make sure that the PIN - RIGGING 98D27207516330, part of the RIGGING PIN SET (98D27207516000), or the PIN - RIGGING (98D27207549000) is in position in the yaw damper bellcrank.
Subtask 27-26-51-865-052
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
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PANEL DESIGNATION IDENT. LOCATION
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49VU AUTO FLT/FAC1/28VDC 49VU AUTO FLT/FAC1/26VAC 121VU AUTO FLT/FAC2/28VDC 121VU AUTO FLT/FAC2/26VAC 5CC1 14CC1 5CC2 14CC2 B04B03M19M18
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