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 : PRESSURIZE ONLY THE HYDRAULIC SYSTEM(S) THAT IS (ARE) NECESSARY FOR
_______ THE TASK. ISOLATE THE OTHER HYDRAULIC SYSTEM(S) BEFORE YOU SUPPLY HYDRAULIC POWER TO THE AIRCRAFT.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notices
No specific access platform 11.0 m (36 ft. 1 in.) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) 98D27207546000 1 PIN - RIGGING 98D27207547000 1 PIN - RIGGING
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
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R Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 05-027 USA MIL-L-81309 RUST INHIBITOR(FOR CORROSION USE 15-004) (Ref. 20-31-00) Material No. 08-029 USA MIL-R-46082 TYPE I ADHESIVE (Ref. 20-31-00) Material No. 11-002 USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00)
C. Expendable Parts
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FIG.ITEM |DESIGNATION |IPC-CSN
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20 cotter pins 27-21-04 12 -100 31 cotter pin 27-21-04 22 -100 40 cotter pin 27-21-04 21 -120 44 cotter pins 27-21-04 12 -100
D. Referenced Information
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REFERENCE DESIGNATION
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20-28-00-912-004 Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage R and in the Wings (this does not include the tanks)-24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 27-22-51-400-001 Installation of the Rudder Trim Actuator (10CC) 27-23-41-400-001 Installation of the Artificial Feel and Trim Unit 27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 27-26-41-400-001 Installation of the Centering Spring Rod for the
Actuator of the Yaw Damper Servo
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-26-51-400-001 Installation of the Yaw Damper Servo Actuator (3CC1) and (3CC2) 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action 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
27-21-47-991-001 Fig. 401 27-21-47-991-002 Fig. 402
3. Job Set-up
__________
(Ref. Fig. 401/TASK 27-21-47-991-001, 402/TASK 27-21-47-991-002)
Subtask 27-21-47-860-053-A
A. Aircraft Maintenance Configuration
(1)
Make sure that the access platform is in position at zone 325.
(2)
Make sure that the access panels 325BL, 325BR and 325CL are open (Ref. TASK 55-33-13-010-002).
(3)
Make sure that the rudder fairing 325AL is removed (Ref. TASK 53-55-12-000-001).
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