C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-869-002 Table of the Maximum Permitted Resistance Values
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)-
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
R 1EFF : ALL 1 27-54-49Page A415 1 1 May 01/04 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-000-003 Removal of the Lock-Torque Shaft - Flaps and Slats
(98D27504030001) 27-50-00-866-008 Extension of the Flaps on the Ground 27-51-18-000-001 Removal of the Asymmetry-Position Pick-Off Unit 29CV
(30CV) 27-51-18-400-001 Installation of the Asymmetry-Position Pick-Off Unit
29CV (30CV) 27-54-00-710-001 Operational Test of the Flap System 27-54-45-000-013 Removal of the Torque Shaft 6232CM(6282CM) 27-54-45-400-013 Installation of the Torque Shaft 6232CM(6282CM) 27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST
F/CTL Page 27-54-49-000-004 Removal of the Flap Track 4 Actuator 6233CM(6283CM) (for corrective action)
**ON A/C 001-049, 051-061, 101-105, 201-203,
27-54-49-991-004 Fig. 406
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
27-54-49-991-004-A Fig. 406A
**ON A/C ALL
3. Job Set-up
__________
**ON A/C 001-049, 051-061, 101-105, 201-203,
(Ref. Fig. 406/TASK 27-54-49-991-004)
R **ON A/C 062-099, 106-149, 151-199, 204-299, 301-399, 401-499,
(Ref. Fig. 406A/TASK 27-54-49-991-004-A)
**ON A/C ALL
Subtask 27-54-49-941-073
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in position to tell persons not to operate the flight controls.
Subtask 27-54-49-860-058
B. Aircraft Maintenance Configuration
R (1) Make sure that the flaps are fully extended (Ref. TASK 27-50-00-866-008).
(2)
Make sure the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is on the flap/slat control lever in the cockpit.
(3)
Make sure that the No. 4 and the No. 5 spoilers have been extended (Ref. TASK 27-60-00-866-002).
(4)
Make sure that a COLLAR-SAFETY, SPOILER is on the piston rod of each servo-control.
(5) Make sure that the trailing edge of the flap is on a support. R (6) Make sure that the clamp holds the carriage in position.
(7)
Make sure that the access platform is below the applicable access panel.
(8)
Make sure that the applicable access panels are removed:
-
for the left wing, panels 573BB, 575CB, 575EB, 575FB, 575GB
-
for the right wing, panels 673BB, 675CB, 675EB, 675FB, 675GB.
(9)
Make sure that the Asymmetry Position Pick-off Unit (APPU) (4) has been removed (Ref. TASK 27-51-18-000-001).
(10)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed on the applicable torque shafts.
(11)
Make sure that the torque shaft (2) and the universal joint (1) have been removed (Ref. TASK 27-54-45-000-013).
Subtask 27-54-49-865-064
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
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