-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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)-
27-50-00-000-002 Removal of the Inboard and Outboard Flap
Hoisting-Sling
27-50-00-400-002 Installation of the Inboard and Outboard Flap
Hoisting-Sling
27-50-00-866-008 Extension of the Flaps on the Ground
27-50-00-866-009 Retraction of the Flaps on the Ground
27-50-00-866-011 Manual Extension of the Flaps
27-50-00-866-012 Manual Retraction of the Flaps
27-51-00-820-003 To Do a Check of the Flap Rigged Position (With the
Sharks Fin)
27-51-00-820-008 Adjustment of the Flap Rigged Position With the
Sharks Fin Tool (A318/319/320)
27-51-44-400-001 Installation of the Interconnecting Strut
27-54-00-710-001 Operational Test of the Flap System
27-54-61-000-002 Removal of the Flap Kink-Seals
27-54-61-400-006 Installation of the Flap Kink-Seals
27-60-00-866-002 Extension-Retraction of the Spoilers for Maintenance
27-64-00-710-001 Operational Test of the Spoiler Hydraulic Actuation
32-12-00-410-001 Close the Main Gear Doors after Access
53-35-11-000-001 Removal of the Wing-to-Fuselage Fairings
54-55-00-000-001 Removal of the Aft Movable Fairing
54-55-00-400-001 Installation of the Aft Movable Fairing
57-55-11-010-001 To Lower the Flap Track No. 2 Movable Fairing for
Access
57-55-11-410-001 To Lift the Flap Track No. 2 Movable Fairing after
Access
ISB 27-1066
ISB 27-1108
**ON A/C 001-001, 051-052, 27-54-61-991-001 Fig. 401
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 429 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, Post SB 27-1117 For A/C 001-001,051-052, 27-54-61-991-001-A Fig. 401A **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-54-61-991-012 Fig. 402 **ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
R 27-54-61-991-005 Fig. 403 **ON A/C 106-149, 159-199, 211-299, 401-499,
R 27-54-61-991-005-B Fig. 403A **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-54-61-991-006 Fig. 404 27-54-61-991-013 Fig. 405 **ON A/C 001-049, 051-061, 101-103, 201-203,
R 27-54-61-991-007 Fig. 406 **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
R 27-54-61-991-007-A Fig. 406A **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-54-61-991-008 Fig. 408
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 430 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
3. Job Set-up
__________ Subtask 27-54-61-941-060
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice(s) is on the panel 400VU to tell persons not to operate the landing gear.
(3)
Make sure that the warning notice is in position to tell persons not to operate the flight controls.
Subtask 27-54-61-865-051
B. 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
Subtask 27-54-61-860-058
C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
Make sure that the flaps are in the position 3 (Ref. TASK 27-50-00-866-011).
(2)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is on the applicable torque shaft.
(3)
Make sure that the access platform is in position below the applicable inboard flap.
(4)
Make sure that the number 1 spoiler is fully extended (Ref. TASK 27-60-00-866-002).
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