B. Consumable Materials
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REFERENCE DESIGNATION
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No specific corrosion-resistant steel lockwire 0.8 mm (0.032 in) dia
R Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) Material No. 05-052 SELF-ADHES.PVC DISKS FOR HOISTING POINT BLANKING (Ref. 20-31-00) Material No. 11-008 (USE 11-008A) (Ref. 20-31-00)
C. Expendable Parts
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FIG.ITEM |DESIGNATION |IPC-CSN
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59 cotter pins 55-31-04 02 -190 72 cotter pins 55-31-04 03 -190 85 cotter pins 27-21-04 21 -120
D. Referenced Information
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REFERENCE DESIGNATION
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20-21-12-911-001 Tightening Torques for Pipes Unions (not for OXYGEN unions)
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)-
23-11-00-710-001 Operational Test of the HF System 27-21-00-720-002 Functional Test of the Rudder Mechanical Control 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
29-00-00-910-002 Safety Procedures of the Hydraulic System
34-55-00-710-001 Operational Test of the VOR/MKR
53-45-11-400-001 Installation of the Dorsal Fin 321AL
53-55-11-400-001 Installation of the Fairings 323AL/323AR
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
53-55-12-400-001 Installation of the Rudder Fairings 325AL and 325AR
55-33-13-410-002 Closing/Installation of the Trailing Edge Access-Panels 325EL, 325ER, 325DL, 325DR, 325CL, 325CR, 325BL and 325BR
55-43-19-400-001 Installation of the Rudder Fillet Fairing 55-31-11-991-005 Fig. 401 55-31-11-991-001 Fig. 402 55-31-11-991-002 Fig. 403 55-31-11-991-003 Fig. 404 55-31-11-991-006 Fig. 405
3. Job Set-up
__________
Subtask 55-31-11-860-052
A. Aircraft Maintenance Configuration
(1)
Make sure that the warning notices are in position to tell persons not to operate the flight controls.
(2)
Make sure that the access platform is in position.
(3)
Make sure that the Green, Blue and Yellow hydraulic system is drpressurized(Ref. TASK 29-00-00-864-001) (Ref. TASK 29-00-00-910-002).
(4)
Make sure that the rigging pins are installed.
1EFF : ALL 1 55-31-11Page 417 1 1 Aug 01/02R 1 1 1CES 1
Subtask 55-31-11-865-053
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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R **ON A/C 001-049, 101-105, 151-199,
49VU COM/HF1 1RE1 HA14
**ON A/C ALL
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03
R **ON A/C 051-099, 106-149, 201-299, 301-399,
49VU COM HF1 1RE1 HA14
**ON A/C ALL
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU COM NAV/VOR/2 2RS2 K08 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
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