(Ref. Fig. 401/TASK 27-54-45-991-001) R **ON A/C 062-099, 104-149, 151-199, 204-299, 301-399, 401-499,
 (Ref. Fig. 401A/TASK 27-54-45-991-001-A)
 **ON A/C ALL

 Subtask 27-54-45-941-077
 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 landing-gear doors.

 (3)
 Make sure that the warning notice is in position to tell persons not to operate the flap controls.

 Subtask 27-54-45-860-063
 B. 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 fully retracted (Ref. TASK 27-50-00-866-009).

 (2)
 Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER is on the flap/slat control lever on panel 114VU.

 (3)
 Make sure that the MLG are open (Ref. TASK 32-12-00-010-001).

 (4)
 Make sure that the GROUND LOCK SLEEVE is on the applicable MLG door actuator.

 (5)
 Make sure that the access platform is in the applicable position.

 (6)
 Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is installed on the flap torque shaft (Ref. TASK 27-50-00-400-003), outboard of the removed component.

 Subtask 27-54-45-865-059
 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
_________
 (Ref. Fig. 402/TASK 27-54-45-991-002, 403/TASK 27-54-45-991-005)
 CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
 EDGE:

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.

 -MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
 1EFF : ALL 1 27-54-45Page 412 1 1 May 01/00R 1 1 1CES 1

 Subtask 27-54-45-420-063
 A. Preparation for Installation
 CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT.

_______
 GREASE AND ASSEMBLY PASTE DO NOT MIX.

 (1)
 Clean the parts:

 (a) Use a clean MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026) to clean:
 -
the nuts (4), (8) and (101)

 -
the washers (103)

 -
the bolts (3) and (9)

 -
the flanges of the universal joints (1) and (7)

 -
the flanges of the shaft (2).

 (2)
 Dry the parts. WARNING : USE A PROTECTIVE EYE SHIELD/GOGGLES WHEN YOU USE COMPRESSED

_______ AIR. DEBRIS AND/OR HIGH PRESSURE AIR CAN DAMAGE YOUR EYES.
 WARNING : DO NOT PUT COMPRESSED GAS IN CONTACT WITH YOUR SKIN. THE
_______ GAS CAN GO THROUGH THE SKIN AND MAKE BUBBLES IN THE BLOOD. THIS CONDITION CAN KILL YOU.
 (a) Use compressed air to dry the cleaned areas.
 (3)
 Do an inspection of the component interface and/or the adjacent area.

 (4)
 Do one of the steps that follow:
 CAUTION : DO NOT APPLY MORE THAN ONE TYPE OF LUBRICANT.

_______
 GREASE AND ASSEMBLY PASTE DO NOT MIX.

 (a)
 Apply a thin layer of COMMON GREASE (Material No. 04-024) to the torque shaft splines.

 - or

 (b)
 Apply a thin layer of COMMON GREASE (Material No. 04-018) to the torque shaft splines.

 1EFF : ALL 1 27-54-45Page 413 1 1 May 01/00R 1 1 1CES 1

 Subtask 27-54-45-420-050
 B. Installation of the Torque Shaft 6202CM(6052CM)
 (1)
 Put the retaining ring (5) temporarily in position on the shaft of the universal joint (7).

 (2)
 Install the universal joint (7) in the end of the right-angle gear-box 6203CM(6253CM).

 (3)
 Install the pin (6) and the retaining ring (5).

 (4)
 Install the universal joint (1) and align its flange with the flange of the universal joint (7).
　
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