Removal of the Torque Shaft 6032CM(6082CM) (for
corrective action)
Installation of the Torque Shaft 6032CM(6082CM) (for
corrective action)
Removal of the Torque Shaft 6034CM(6084CM) (for
corrective action)
Installation of the Torque Shaft 6034CM(6084CM) (for
corrective action)
Removal of the Torque Shaft 6046CM(6096CM) (for
corrective action)
Installation of the Torque Shaft 6046CM(6096CM) (for
corrective action)
Removal of the Steady Bearing FIN 6007CM(6057CM) (for
corrective action)
Installation of the Steady Bearing FIN 6007CM(6057CM)
(for corrective action)
FOR FIN 6017CM, 6067CM, 6019CM, 6069CM
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-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-84-44-000-002 27-84-44-400-002 FOR FIN 6021CM, 6071CM
27-84-44-000-003 27-84-44-400-003 FOR FIN 6023CM, 6073CM
27-84-44-000-004 27-84-44-400-004 FOR FIN 6025CM, 6075CM
27-84-44-000-005 27-84-44-400-005 FOR FIN 6031CM, 6081CM
27-84-44-000-006 27-84-44-400-006
3. Job Set-up
__________ Subtask 27-84-00-941-058
A. Safety Precautions
Removal of the Steady Bearings FIN
6017CM(6067CM)/6019CM(6069CM) (for corrective action)
Installation of the Steady Bearings FIN
6017CM(6067CM)/6019CM(6069CM) (for corrective action)
Removal of the Steady Bearing FIN 6021CM(6071CM) (for
corrective action)
Installation of the Steady Bearing FIN 6021CM(6071CM)
(for corrective action)
Removal of the Steady Bearing FIN 6023CM(6073CM) (for
corrective action)
Installation of the Steady Bearing FIN 6023CM(6073CM)
(for corrective action)
Removal of the Steady Bearing FIN 6025CM(6075CM) (for
corrective action)
Installation of the Steady Bearing FIN 6025CM(6075CM)
(for corrective action)
Removal of the Steady Bearing FIN 6031CM(6081CM) (for
corrective action)
Installation of the Steady Bearing FIN 6031CM(6081CM)
(for corrective action)
(1)
Put the safety barriers in position.
(2)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the slat/flap control lever.
(3)
Put a warning notice in position to tell persons not to operate the slat system.
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Subtask 27-84-00-860-054
B. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
Pressurize the Green Hydraulic system (Ref. TASK 29-10-00-863-001).
(3) Pressurize the Yellow Hydraulic system (Ref. TASK 29-10-00-863-002). Subtask 27-84-00-010-055
C. Get Access
(1)
Put an adjustable access platform in position below the applicable zone 521(621) and 522(622).
(2)
Open the applicable access panels:
-
for the left wing, open 191BB, 191BT, 191EB, 191KB, 521AB, 521CB, 521EB, 521GB, 521HB, 522AB, 522CB, 522EB, 522FB, 522JB, 522KB, 522LB, 522NB, 522QB, 522SB, 522UB
-
for the right wing, open 192BT, 192CT, 192EB, 192FB, 192KB, 621AB, 621CB, 621EB, 621GB, 621HB, 622AB, 622CB, 622EB, 622FB, 622JB, 622KB, 622LB, 622NB, 622QB, 622SB, 622UB.
4. Procedure
_________ Subtask 27-84-00-210-053
A. Operational Test of Wingtip Brakes/Pressure-Off Brakes, Followed by Check of Transmission Shafting Integrity and Inspection of Seal Witness Drains
(1)
Do an operational test of the wing-tip brake and the pressure-off brake (Ref. TASK 27-81-00-710-001).
(2)
Trouble-shoot system failures (Ref. TSM 27 PB 101).
(3)
Do a check of the integrity of the slat transmission system and inspection of the seal witness drains of the wing-tip brakes (Ref. TASK 27-84-00-210-002).
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(4) Replace the Defective Components of the Slat Transmission System.
(a) Replace the applicable torque shafts:
-
FOR 6002CM, 6004CM (Ref. TASK 27-84-45-000-001) and (Ref. TASK 27-84-45-400-002)
-
FOR 6006CM, 6056CM (Ref. TASK 27-84-45-000-002) and (Ref. TASK 27-84-45-400-003)
-
FOR 6008CM, 6058CM (Ref. TASK 27-84-45-000-003) and (Ref. TASK 27-84-45-400-004)
-
FOR 6010CM, 6060CM (Ref. TASK 27-84-45-000-004) and (Ref. TASK 27-84-45-400-005)
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