-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-000-003 27-50-00-400-003 27-50-00-866-008 27-50-00-866-009 27-51-00-820-003 27-54-00-710-001 27-54-49-000-004 27-54-49-400-004 27-60-00-866-002 57-55-11-000-001 57-55-11-000-004 57-55-11-400-001 Removal of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)Extension of the Flaps on the GroundRetraction of the Flaps on the GroundTo Do a Check of the Flap Rigged Position (With the Sharks Fin)Operational Test of the Flap SystemRemoval of the Flap Track 4 Actuator 6233CM(6283CM)Installation of the Flap Track 4 Actuator 6233CM(6283CM)Extension-Retraction of the Spoilers for MaintenanceRemoval of the Flap Track Fairings Nos. 2, 3 and 4Removal of the Flap Track Fairings Nos. 2, 3 and 4Installation of the Flap Track Fairings Nos. 2, 3 and 4
57-55-11-400-004 Installation of the Flap Track Fairings Nos. 2, 3 and 4
27-54-55-991-002 Fig. 403
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-210, 301-399, 27-54-55-991-003 Fig. 404 R **ON A/C 106-149, 211-299, 401-499, 27-54-55-991-003-A Fig. 404A
**ON A/C ALL
3. Job Set-up
__________
Subtask 27-54-55-941-072
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice(s) are in the cockpit to tell persons not to operate the flight controls.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-55-860-060
B. Aircraft Maintenance Configuration
(1)
Make sure that the flaps are fully extended (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the Nos. 2, 3, 4 and 5 spoilers are fully extended (Ref. TASK 27-60-00-866-002).
(3)
Make sure that the COLLAR-SAFETY, SPOILER is on the piston rod of the servo-control.
(4)
Make sure that the access platform is below the applicable zone 575 or 675.
(5)
Make sure that the applicable access panels have been removed 575BB(675BB), 575FB(675FB).
(6)
Make sure that the No. 3 and the No. 4 Flap-Track movable fairings have been removed (Ref. TASK 57-55-11-000-001).
(7)
Make sure that the Track 4 actuator has been removed (Ref. TASK 27-54-49-000-004).
(8)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control-lever.
(9)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is on the torque shaft adjacent to the Track 4 actuator (Ref. TASK 27-50-00-400-003).
**ON A/C 301-399,
Subtask 27-54-55-860-060-A
B. Aircraft Maintenance Configuration
(1)
Make sure that the flaps are fully extended (Ref. TASK 27-50-00-866-008).
(2)
Make sure that the Nos.2, 3, 4 and 5 spoilers are fully extended (Ref. TASK 27-60-00-866-002).
(3)
Make sure that the COLLAR-SAFETY, SPOILER is on the piston rod of the servo-control.
(4)
Make sure that the access platform is below the applicable zone 575 or 675.
(5)
Make sure that the applicable access panels have been removed 575BB(675BB), 575FB(675FB).
(6)
Make sure that the No. 3 and the No. 4 Flap-Track movable fairings have been removed (Ref. TASK 57-55-11-000-004).
(7)
Make sure that the Track 4 actuator has been removed (Ref. TASK 27-54-49-000-004).
(8)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER is installed on the flap/slat control-lever.
(9)
Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is on the torque shaft adjacent to the Track 4 actuator (Ref. TASK 27-50-00-400-003).
**ON A/C ALL
Subtask 27-54-55-865-057
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
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-210, 301-399,
(Ref. Fig. 404/TASK 27-54-55-991-003)
R **ON A/C 106-149, 211-299, 401-499,
(Ref. Fig. 404A/TASK 27-54-55-991-003-A)
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